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UNITED STATES SECURITIES AND EXCHANGE COMMISSION

Washington, D.C. 20549

FORM 10-K

(Mark one)

þ ANNUAL REPORT PURSUANT TO SECTION 13 OR 15(d) OF THE SECURITIES EXCHANGE ACT OF 1934

 

     For the fiscal year ended December 31, 2011

OR

 

¨ TRANSITION REPORT PURSUANT TO SECTION 13 OR 15(d) OF THE SECURITIES EXCHANGE ACT OF 1934

 

     For the transition period from:                      to                     

Commission File No. 001-34299

DIGITALGLOBE, INC.

(Exact name of registrant as specified in its charter)

 

Delaware   31-1420852
(State or other jurisdiction of incorporation or organization)   (I.R.S. Employer Identification No.)

1601 Dry Creek Drive, Suite 260

Longmont, Colorado

  80503
(Address of principal executive office)   (Zip Code)

(303) 684-4000

(Registrant’s telephone number, including area code)

 

(Title of Each Class)

 

(Name of Each Exchange on Which Registered)

Common Stock, par value $0.001 per share

  New York Stock Exchange

Securities registered pursuant to Section 12(g) of the Act:

Not Applicable

Indicate by check mark if the registrant is a well-known seasoned issuer, as defined in Rule 405 of the Securities Act.    Yes   ¨     No   þ

Indicate by check mark if the registrant is not required to file reports pursuant to Section 13 or 15(d) of the Act.    Yes   ¨     No   þ

Indicate by check mark whether the registrant (1) has filed all reports required to be filed by Section 13 or 15(d) of the Securities Exchange Act of 1934 during the preceding 12 months (or for such shorter period that the registrant was required to file such reports) and (2) has been subject to such filing requirements for the past 90 days.    Yes   þ     No   ¨

Indicate by check mark whether the registrant has submitted electronically and posted on its corporate Web site, if any, every Interactive Data File required to be submitted and posted pursuant to Rule 405 of Regulation S-T (§232.405 of this chapter) during the preceding 12 months (or for such shorter period that the registrant was required to submit and post such files).    Yes   þ     No   ¨

Indicate by check mark if disclosure of delinquent filers pursuant to Item 405 of Regulation S-K is not contained herein, and will not be contained, to the best of the registrant’s knowledge, in definitive proxy or information statements incorporated by reference in Part III of this Form 10-K or any amendment to this Form 10-K.     ¨

Indicate by check mark whether the registrant is a large accelerated filer, an accelerated filer, or a smaller reporting company. (See definitions of “large accelerated filer”, “accelerated filer” and “smaller reporting company” in Rule 12b-2 of the Exchange Act).

 

Large accelerated filer     þ

   Accelerated filer     ¨    Non-accelerated filer     ¨    Smaller reporting company     ¨

Indicate by check mark whether the registrant is a shell company (as defined in Rule 12b-2 of the Act).    Yes   ¨     No   þ

State the aggregate market value of the voting and non-voting common equity held by non-affiliates computed by reference to the price at which the common equity was last sold, or the average bid and asked price of such common equity, as of the last business day of the registrant’s most recently completed second fiscal quarter: The aggregate market value of the registrant’s common stock held by non-affiliates, computed by reference to the closing sale price of $25.41 as reported by the New York Stock Exchange on June 30, 2011 was $986,447,226.

The number of shares of the registrant’s common stock, $0.001 par value, outstanding as of February 27, 2012 (latest practicable date) was 46,320,471.

Documents Incorporated by Reference: Portions of the registrant’s Definitive Proxy Statement for the 2012 Annual Meeting of Stockholders are incorporated by reference into Part III.

 

 

 

 

 

LOGO


Table of Contents

TABLE OF CONTENTS

 

     PAGE  

SPECIAL NOTE REGARDING FORWARD LOOKING STATEMENTS

     2   

TRADEMARKS

     2   
PART I   

ITEM 1.

  

BUSINESS

     3   

ITEM 1A.

  

RISK FACTORS

     11   

ITEM 1B.

  

UNRESOLVED STAFF COMMENTS

     21   

ITEM 2.

  

PROPERTIES

     22   

ITEM 3.

  

LEGAL PROCEEDINGS

     22   

ITEM 4.

  

MINE SAFETY DISCLOSURES

     22   
PART II   

ITEM 5.

   MARKET FOR REGISTRANT’S COMMON EQUITY, RELATED STOCKHOLDER MATTERS AND ISSUER PURCHASES OF EQUITY SECURITIES      23   

ITEM 6.

   SELECTED FINANCIAL DATA      25   

ITEM 7.

   MANAGEMENT’S DISCUSSION AND ANALYSIS OF FINANCIAL CONDITION AND RESULTS OF OPERATIONS      26   

ITEM 7A.

   QUANTITATIVE AND QUALITATIVE DISCLOSURES ABOUT MARKET RISK      46   

ITEM 8.

   FINANCIAL STATEMENTS AND SUPPLEMENTARY DATA      47   

ITEM 9.

   CHANGES IN AND DISAGREEMENTS WITH ACCOUNTANTS ON ACCOUNTING AND FINANCIAL DISCLOSURE      82   

ITEM 9A.

   CONTROLS AND PROCEDURES      82   

ITEM 9B.

   OTHER INFORMATION      84   
PART III   

ITEM 10.

   DIRECTORS, EXECUTIVE OFFICERS AND CORPORATE GOVERNANCE      85   

ITEM 11.

   EXECUTIVE COMPENSATION      85   

ITEM 12.

   SECURITY OWNERSHIP OF CERTAIN BENEFICIAL OWNERS AND MANAGEMENT AND RELATED STOCKHOLDER MATTERS      85   

ITEM 13.

   CERTAIN RELATIONSHIPS AND RELATED TRANSACTIONS, AND DIRECTOR INDEPENDENCE      85   

ITEM 14.

   PRINCIPAL ACCOUNTING FEES AND SERVICES      85   
PART IV   

ITEM 15.

   EXHIBITS AND FINANCIAL STATEMENT SCHEDULES      86   

 

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SPECIAL NOTE REGARDING FORWARD-LOOKING STATEMENTS

Certain statements contained herein and other of our reports, filings, and public announcements may contain or incorporate forward-looking statements within the meaning of the Private Securities Litigation Reform Act of 1995, as amended. Forward-looking statements relate to future events or our future financial performance. We generally identify forward-looking statements by terminology such as “may,” “will,” “should,” “expects,” “plans,” “anticipates,” “could,” “intends,” “target,” “projects,” “contemplates,” “believes,” “estimates,” “predicts,” “potential” or “continue” or the negative of these terms or other similar words, although not all forward-looking statements contain these words.

Any forward-looking statements are based upon our historical performance and on our current plans, estimates and expectations. The inclusion of this forward-looking information should not be regarded as a representation by us that the future plans, estimates or expectations will be achieved. Such forward-looking statements are subject to various risks and uncertainties and assumptions. A number of important factors could cause our actual results or performance to differ materially from those indicated by such forward looking statements, including: the loss, reduction or change in terms of any of our primary contracts; the availability of government funding for our products and services both domestically and internationally; changes in government and customer priorities and requirements (including cost-cutting initiatives, the potential deferral of awards, terminations or reduction of expenditures to respond to the priorities of congress and the administration, or budgetary cuts resulting from congressional committee recommendations or automatic sequestration under the Budget Control Act of 2011); the loss or impairment of our satellites; delays in the construction and launch of WorldView-3; delays in implementation of planned ground system and infrastructure enhancements; loss or damage to the content contained in our ImageLibrary; interruption or failure of our ground system and other infrastructure, decrease in demand for our imagery products and services; increased competition that may reduce our market share or cause us to lower our prices; our failure to obtain or maintain required regulatory approvals and licenses; changes in U.S. foreign law or regulation that may limit our ability to distribute our imagery products and services; the costs associated with being a public company; and other important factors, all as described more fully in our filings with the Securities and Exchange Commission, including our Annual Report on Form 10-K.

We undertake no obligation to update any forward-looking statement to reflect events or circumstances after the date on which the statement is made or to reflect the occurrence of unanticipated events. Readers are cautioned not to place undue reliance on any of these forward looking statements.

TRADEMARKS

DigitalGlobe, Digitalglobe.com , EarthService, GlobeXplorer, CitySphere, ImageBuilder, ImageConnect, PhotoMapper, Seconds On Orbit, SOO and WorldView Global Alliance are our trademarks. Other names used in this annual report are for informational purposes only and may be trademarks of their respective owners.

 

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PART I

 

ITEM 1.

BUSINESS

Overview

DigitalGlobe is a leading global provider of commercial high-resolution earth imagery products and information services. Sourced from our own advanced satellite constellation, our imagery solutions support a wide variety of uses within both domestic and international governments, including defense and intelligence, and civil agencies, location based services (LBS), and other verticals such as financial services, mining, telecommunications, and oil and gas exploration. We offer a range of products and services designed to enable customers to easily access and integrate our imagery into their workflow. We believe that our imagery archive, which we refer to as our ImageLibrary, is the largest, most up-to-date and comprehensive archive of high-resolution earth imagery commercially available, containing more than 2.0 billion square kilometers of imagery, with new imagery added every day. As of December 31, 2011, our collection capacity was approximately 900 million square kilometers of imagery per year or roughly six times the earth’s land surface area.

Products and Services

We offer earth imagery products and information services that are comprised of imagery from our three high-resolution satellite constellation as well as aerial imagery, satellite imagery and other information that we acquire from third party suppliers. We process and analyze our imagery according to our customers’ specifications and deliver our products using the distribution method that best suits their needs. Customers can purchase satellite or aerial images that are archived in our ImageLibrary, or they can place orders to task our satellites for a specific area of interest.

Customers specify how they want the imagery content that they are purchasing from us to be produced. We deliver our satellite imagery content at three processing levels: (i) basic imagery with the least amount of processing; (ii) standard imagery with radiometric and geometric correction; and (iii) ortho-rectified imagery with radiometric, geometric, and topographic correction. Radiometric correction enables images to appear uniformly illuminated with the appropriate level of brightness. Geometric correction allows a user to identify the latitudinal, longitudinal and altitudinal location of any point in an image. Topographic correction accounts for terrain and projects images onto the earth as they would be seen by the human eye. All of our purchased aerial imagery is delivered as ortho-rectified imagery.

We also use enhanced processing to produce mosaic and stereo imagery products. The mosaic process takes multiple imagery scenes, collected at different times and dates, and merges them into a single seamless imagery product. We use specialized collection and enhanced processing to produce stereo imagery products. Stereo imagery products consist of two images collected from two different viewpoints along the satellite orbit track that are produced as basic products, but can be viewed in stereo (3D) using specialized software. Stereo imagery products are used for the creation of digital elevation maps, for the more accurate creation of 3D maps and flight simulations.

We offer a range of on- and off-line distribution options designed to enable customers to easily access and integrate our imagery into their business operations and applications, including desktop software applications, web services that provide for direct on-line access to our ImageLibrary, File Transfer Protocol, or FTP, and physical media such as CD, DVD and hard drive. We offer an additional distribution option through our Direct Access Program, or DAP, that allows certain customers, approved by the U.S. government, to task and download data directly from our WorldView-1 and WorldView-2 satellites within their regional area of interest. DAP is designed to meet the enhanced information and operational security needs of a select and limited number of defense and intelligence customers and certain commercial customers.

We also offer analysis products and services to provide context and insight to imagery. Our analysis products and services focus on regular monitoring of events or areas of interest to end-users, providing

 

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situational awareness for crisis events to support first responders and on-going relief efforts, and providing deeper insight into implications of change, particularly in environmental and land use planning applications. Although a relatively small percentage of revenue today is generated from analysis services, we believe customers are increasingly looking for analysis, content and insight, in addition to the imagery we provide.

With the exception of our analysis center products and services, which we primarily sell directly, we sell our products and services through a combination of direct and indirect channels, a global network of resellers, strategic partners, direct enterprise sales and web services. During the year ended December 31, 2011, we generated 38.3% of our revenue through direct sales, and 61.7% of our revenue from our reseller and partner network.

Customers

We have two reportable segments: defense and intelligence, and commercial. Defense and intelligence revenue is sourced from domestic and international government defense and intelligence customers, including the majority of those in our DAP. Revenue in our commercial segment is sourced from customers in LBS, international civil government and from customers in other verticals. In 2011, we generated 77.0% of our revenue from defense and intelligence customers and 23.0% of our revenue from commercial customers.

Defense and Intelligence

Our single largest defense and intelligence customer is the U.S. government. The National Geospatial-Intelligence Agency (NGA) serves as the primary U.S. government procurement agency for geospatial information and purchases imagery products and services on behalf of various agencies within the U.S. government, including defense, intelligence and law enforcement agencies. NGA currently comprises 60.1% of our revenue.

The ClearView agreement, executed in 2002, with NGA originally provided for minimum annual purchase commitments over four years. In January 2007, the ClearView Agreement was merged into the NextView Agreement.

In January 2008, we amended the NextView agreement from an image-based ordering agreement to a Service Level Agreement (SLA). Under the SLA, we were obligated to make substantially all the image tasking capacity of our WorldView-1 satellite available to NGA, as well as to meet certain service requirements related to the operational performance of our WorldView-1 satellite and related ground systems. The terms of the SLA provided for payment of $12.5 million per month, subject to the right of NGA to holdback an allowance of up to $0.8 million of the total $12.5 million monthly fee if certain performance criteria were not met. The holdback amounts could be used by NGA to extend the SLA period or could be applied to any new agreement between the parties. In June 2009, we signed an extension to the SLA through March 31, 2010 with an option for NGA to extend at the same level and on the same terms through December 31, 2010. In February 2010, we modified the SLA to allow NGA the option to extend the SLA on the same terms for three months from April 1, 2010 to June 30, 2010 with six additional options, each for a one month period, with the last option expiring in December 31, 2010. NGA exercised two monthly options under the NextView SLA through August 31, 2010.

On August 6, 2010, we entered into the EnhancedView contract with NGA. The SLA portion of the EnhancedView contract had an effective date of September 1, 2010, commencing upon the expiration of the NextView SLA. The EnhancedView contract has a ten year term, inclusive of nine one-year options exercisable by NGA, and is subject to Congressional appropriations and annual federal budget approval and the right of NGA to terminate, modify or suspend the contract at any time. For a discussion of the risks associated with our government contracts, see Risk Factors in Part 1, Item 1A. On July 25, 2011, NGA provided us with an amendment to the EnhancedView contract exercising year two for the SLA for the period September 1, 2011 through August 31, 2012.

 

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The EnhancedView SLA portion of the award is sized at $2.8 billion over the term of the contract; $250.0 million annually, or $20.8 million per month, for the first four contract years, commencing September 1, 2010, with an increase to $300.0 million annually, or $25.0 million per month, for the remaining six years of the contract term. The award also provides for up to $750.0 million for value added products, infrastructure enhancements and other services, including the option for NGA to require us to lower the altitude of WorldView-2 to an altitude of 496 km at any time after September 1, 2013. We are required to meet certain service level requirements related to the operational performance of the satellites comprising the WorldView constellation and related ground systems. To support requirements under this agreement, we have begun the procurement and construction of our next satellite, WorldView-3, as well as certain other infrastructure improvements.

We recognize revenue for the $2.8 billion in services to be provided under the EnhancedView SLA using a proportional performance method based upon the percentage of capacity of our constellation made available to NGA compared to the total capacity to be provided over the life of the contract. We have agreed to increase the image taking capacity of the constellation through the installation of additional remote ground terminals, which communicate directly with our satellites, as well as the addition of a new satellite, WorldView-3. As capacity is added to our constellation, we recognize revenue in direct proportion to the amount of incremental capacity that is made available to NGA in the reporting period as a percentage of the total capacity estimated to be made available over the life of the EnhancedView contract. For the year ended December 31, 2010, we recognized approximately $50.2 million of revenue for imagery services under the EnhancedView SLA. From January 1, 2011 through August 31, 2011, we recognized approximately $12.5 million of revenue per month for imagery services under the EnhancedView SLA. As of September 1, 2011, we increased the capacity of the constellation made available to NGA and are now recognizing approximately $14.1 million per month under the EnhancedView SLA. For the year ended December 31, 2011, we recognized approximately $157.0 million of revenue and we recorded $94.6 million of deferred revenue related to the EnhancedView SLA contract.

Based on the EnhancedView contract, and assuming all option years under the agreement are exercised and fully funded, we will receive a consistent, monthly non-refundable cash payment of approximately $20.8 million from NGA during the first four years of the EnhancedView contract, with an increase to $25.0 million per month in years five through ten. Each month is subject to a holdback of up to 10% of the monthly cash payment, depending upon our performance against contractually defined criteria. If we have been certified as having performed all requirements in the agreement each month, no holdback will be applied to that month. If funds are held back, the Company retains the cash, however, those funds can be applied as a credit to future products and services or may be used to fund a pro-rated extension beyond the current contract period. For the performance period commencing upon the effective date of September 1, 2010 through December 31, 2010, we satisfied all performance criteria under the agreement, and therefore had no holdback for the period. During the year ended December 31, 2011, there was a $0.2 million of holdback, which occurred during the first quarter of 2011, all of which has been applied to other products and recognized as revenue as of December 31, 2011.

In addition to the U.S. government, our other defense and intelligence customers include U.S. and foreign defense contractors, and certain foreign government defense, intelligence, and national security agencies. Our defense and intelligence customers use our products for many purposes, including but not limited to mapping, monitoring, threat assessment, disaster response and training. We sell to our defense and intelligence customers directly and through resellers. In 2011, defense and intelligence customers accounted for $261.4 million or 77.0% of our total revenue, of which NGA was 60.1% of total 2011 revenue.

Direct Access Program

Customers in our Direct Access Program (DAP) are able to directly task and receive imagery from our WorldView-1 and WorldView-2 satellites within certain local geographic boundaries of interest. These customers have the ability to download imagery directly from our satellites as a result of purchasing from us the requisite hardware required to communicate with and process imagery from our satellites. DAP is designed to

 

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meet the enhanced information and operational security needs of a select and limited number of defense and intelligence customers and certain commercial customers. All of our DAP agreements are subject to approval by the U.S. government.

We have five customers signed to our DAP with one operational in 2009, three more operational in 2010, and one expected to become operational in the first half of 2012. In 2011, we generated $47.1 million in revenue from our four currently operational DAP customers, representing 13.9% of our total revenue.

For segment reporting purposes, we include DAP within our defense and intelligence segment.

Commercial

Our commercial business consists of customers concentrated in three principal industry sectors, which are international civil governments, providers of LBS and other industry verticals. International civil government customers buy our products and services for mapping, monitoring and planning activities for their populations. Providers of LBS, include internet portals, connected devices, and digital mapmakers, who use our imagery products and services to expand their products and services. Customers in other industry verticals are represented by financial services, oil and gas, telecommunications, utilities, environmental services and other industry verticals who use our imagery in a wide range of applications. We typically sell to the international civil government and other industry verticals customers through our global resellers and partners, and we primarily sell directly to providers of LBS.

Our commercial customers are located throughout the world. We sell to these customers directly and through resellers. Our commercial revenue is generated both through purchases of our products and services on an as-needed basis and through annual and multi-year contracts. In 2011, commercial revenue accounted for $78.1 million or 23.0% of our total revenue.

Satellite and Ground System Operations

Our business operations consist primarily of our satellite constellation, related satellite control ground stations, and our image processing facilities.

The following table summarizes the primary characteristics of the satellites in constellation in operation as of December 31, 2011:

 

    

QuickBird

 

WorldView-1

  

WorldView-2

Best Ground Resolution

   64-centimeters black and
white 2.56-meter multi-
spectral
  50-centimeters black and
white
   46-centimeters black and
white 1.84-meter multi-
spectral

Annual Collection Capacity

   77 million square
kilometers
  468 million square
kilometers
   369 million square
kilometers

Revisit Time

   2-3 days   1-2 days    1-2 days

Orbital Altitude

   469 kilometers(1)   496 kilometers    770 kilometers

Launch Date

   October 2001   September 2007    October 2009

Original Estimated Design Life(2)

   Q4 2006   Q4 2017    Q1 2018

Expected End of Operational Life(3)

   Q3 2013   Q2 2018    Q1 2021

Original Satellite Cost

   $174.4 million   $473.2 million    $463.2 million

Satellite Net Book Value

   $3.9 million   $287.1 million    $379.0 million

 

(1)

Following NOAA approval in first quarter of 2011 QuickBird was raised to an orbital attitude of 482 kilometers and is slowly deorbiting.

 

(2)

The original estimated design life is the minimum number of years, at a 75% probability, that a satellite is expected to operate based on our construction performance specifications.

 

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(3)

Following actual launch, we determine a satellite’s expected operational life utilizing a calculation that involves the probabilities of failure of the satellite’s components from design or manufacturing defects, environmental stresses or other causes. The expected operational life of these satellites is affected by a number of factors, including the quality of construction, the supply of fuel, the expected gradual environmental degradation of solar panels and other components, the projected levels of solar radiation, the durability of various satellite components and the orbits in which the satellite is placed. On an annual basis, we evaluate the estimated lives of our satellites.

Satellite Insurance

As of December 31, 2011, we maintain the following insurance coverage on our satellites:

 

Satellite

   Policy Period      Coverage  
            (in millions)  

QuickBird

     10/2011 — 10/2012       $ 11.0   

WorldView-1

     10/2011 — 10/2012         235.0   

WorldView-2

     10/2011 — 10/2012         182.0   

WorldView-2

     10/2009 — 10/2012         68.0   

The satellite insurance coverage will pay us in the event of a total loss of a satellite or will indemnify us for partial losses if the functional capacity of the satellite is significantly impaired due to anomalies with the satellite equipment or other events causing significant impairment.

We intend to continue this coverage to the extent it remains available at acceptable premiums. Satellite insurance premiums, corresponding to the launch and in-orbit commissioning period prior to the satellite reaching full operational capability (FOC), are capitalized in the original cost of the satellite and are amortized over the estimated useful life of the asset. The remainder of the insurance premiums that are not capitalized as part of the satellite are recorded as prepaid expenses and are amortized to expense ratably over the related policy periods and are included in selling, general and administrative costs.

Ground Station Centers and Image Processing Facilities

We have eight operational remote ground terminals (RGT) located throughout the world. We own and operate three ground terminals in Fairbanks, Alaska and Prudhoe Bay, Alaska, and Tromso, Norway, and we have a service contract with Kongsberg Satellite Services (KSAT) and ViaSat to utilize their ground stations in five other locations throughout the world. The KSAT and ViaSat RGT’s allow us to supplement the data downlink capabilities of our other three stations, to maximize the amount of imagery we are able to download, as well as to shorten the time between downloads to enable us to serve our customers with faster turnaround times for our imagery products and services. Each ground station center is strategically placed to maximize contact with our satellites on their orbital paths. QuickBird, WorldView-1 and WorldView-2 satellites currently each orbit the earth approximately 15 times per day, communicating with one or more of our ground station centers. We are under contract with KSAT to add an additional three RGT’s in 2012. Our image processing facility at our Longmont, Colorado headquarters houses the hardware and software systems and personnel required to operate and control our satellites as well as process, store and distribute our imagery. Operational control of our satellites, and all data processing, storing and distribution, is managed exclusively from our facility in Longmont, Colorado.

Intellectual Property

We rely on licenses of certain intellectual property to conduct our business operations. Specifically, we license certain proprietary rights from third parties, such as BAE Systems Mission Solutions, Inc., Ball Aerospace and Technologies Corp., Harris Technical Services Corporation, MacDonald Dettwiler and Associates

 

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Ltd., Orbit Logic, and the University of New Brunswick, to enable us to operate our satellites, ground station centers, collection systems and other various components of our systems. In addition, we actively pursue internal development of intellectual property, and as of December 31, 2011, we held three U.S. patents and had four U.S. patent applications pending. As of December 31, 2011, we also held several U.S. and foreign trademark registrations with additional U.S. and foreign trademark applications pending.

Regulation

Operations

The satellite operations portion of our business is highly regulated. The Department of Commerce (DoC), pursuant to the National and Commercial Space Programs Act of 2010 (successor legislation to the 1992 Land Remote Sensing Policy Act, as amended), has the primary regulatory authority over our industry. The DoC delegated responsibility for satellite remote sensing operations to the National Oceanic and Atmospheric Administration (NOAA). Each of our satellites is required to be individually licensed for operation by NOAA. We currently have licenses for our QuickBird, WorldView-1, WorldView-2 and WorldView-3 satellites, which we refer to as the NOAA licenses. Our NOAA licenses require us to obtain prior approval from NOAA for any significant and substantial foreign agreements, and generally require us to operate our satellite system in a manner that is consistent with U.S. national security and foreign policy objectives. Our NOAA license for WorldView-2 requires that all data be resampled to a ground resolution of 0.50 meter black and white and 2.0 meter multispectral before it may be commercially distributed to customers other than the U.S. government or entities specifically approved by the U.S. government. In addition, the NOAA licenses allow the U.S. government to suspend our imaging activities in certain cases, if deemed necessary, for national security reasons. Provided we comply with the NOAA licenses, the NOAA licenses are valid for the operational life of the licensed satellites.

The launch of our satellites and the communication links, both uplink and downlink, are regulated by the Federal Communications Commission (FCC). FCC licenses must be obtained for each individual satellite. The FCC is the governmental agency with primary authority in the United States over the commercial use of satellite frequency spectrum. We currently have the requisite licensing authority from the FCC to operate our QuickBird, WorldView-1 and WorldView-2 satellites. The FCC has also granted licenses to operate ground stations for QuickBird, WorldView-1 and WorldView-2 in the cities of Fairbanks and Prudhoe Bay, Alaska. The FCC’s rules and regulations and terms of our licenses require that we comply with various operating conditions and requirements. Failure to comply with these or other conditions or requirements could lead to sanctions, up to and including revocation, cancellation or non-renewal of our licenses. In addition to the FCC’s requirements, our satellites must undergo the frequency coordination and registration process of the International Telecommunications Union (ITU).

Sales

Satellite imagery does not require an export license in order to be sold internationally. Our ability to sell certain imagery products and value added services may be subject to sanctions or embargoes imposed by the U.S. government against particular entities or individuals, against other countries or by foreign government regulation.

Direct access to the satellites under our DAP program constitute significant and substantial foreign agreements under our NOAA license and require approval from NOAA under the terms of NOAA License. In addition, we or our suppliers must obtain an export license from the Department of State (DoS) for the export of certain equipment and related technology necessary to enable DAP access. The ground station equipment and related technology necessary to allow access to the satellites are controlled under the International Traffic in Arms Regulations (ITAR). The approval process for these sales takes approximately two to three months, and there is no obligation on the part of either NOAA or the DoS to approve any transaction. In addition to required U.S. government approvals, the export of equipment from Canada by our DAP equipment supplier, MacDonald

 

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Dettwiler & Associated Ltd., is subject to Canadian export license requirements. Our DAP customers may also be required to obtain additional approvals from the government of the country in which the ground station is to be operated.

Ownership

We are obligated under our NOAA licenses to monitor and report increases in foreign ownership of common stock of the Company and any agreement for ownership of 20% or greater is subject to NOAA approval. We are also required to report common stock foreign ownership levels to the Defense Security Service (DSS) and to comply with certain rules and regulations to mitigate foreign influence as part of maintaining our facility security clearances. Our facility security clearance allows us to perform work on U.S. government classified contracts. A transfer to foreign ownership also could trigger other requirements including filings with, and review by, the Committee on Foreign Investment in the United States pursuant to the Exon-Florio provision. Depending on the country of origin and identity of foreign owners, other restrictions and requirements may also arise.

Backlog

The following table represents our backlog as of December 31, 2011:

 

     Backlog to be recognized  
     2012      Life of Contracts  
     (in millions)  

EnhancedView SLA

   $ 186.3       $ 2,648.0   

DAP

     45.2         148.5   

Amortization of pre-FOC payments related to NextView

     25.5         162.7   

Other(1)

     49.9         136.7   
  

 

 

    

 

 

 

Total Backlog

   $ 306.9       $ 3,095.9   
  

 

 

    

 

 

 

 

(1)

Other consists of firm orders, minimum commitments under signed customer contracts, remaining amounts under pre-paid subscriptions, firm fixed price reimbursement and funded and unfunded task orders from U.S. and International defense and intelligence and commercial customers.

Backlog consists of all contractual commitments, including those under the anticipated ten year term of the EnhancedView contract, amounts committed under DAP agreements, firm orders, remaining pre-paid subscriptions and task orders from our government customers. Our backlog also includes amounts of obligated funding on indefinite delivery/indefinite quantity (IDIQ) contracts on which we participate for products and services that we believe we are qualified to provide.

The EnhancedView contract is structured as a ten year term, inclusive of nine annual renewal options that may be exercised by NGA. Although NGA may terminate the contract at any time and is not obligated to exercise any of the remaining eight option years, we include the full remaining term in backlog, because we believe it is NGA’s intention to exercise the remaining options, subject only to annual appropriation of funding and the federal budget process. For risks associated with our government contracts, see Item 1A, Risk Factors.

The pre-FOC balance will be recognized over the 10.5 years from the launch of WorldView-1. We recognize it ratably over the estimated satellite life, but the recognition of this revenue has no effect on our ability to generate additional revenue from the usage of our satellite and therefore should not be considered a reduction in our capacity to generate additional sales.

Although backlog reflects business that is considered to be firm, terminations, amendments or cancellations may occur which could result in a reduction in our total backlog. In addition, failure to receive task orders under

 

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IDIQ contracts could also result in a reduction in our total backlog. Any such terminations, amendments or cancellations of contractual commitments, or failure to receive task orders under IDIQ contracts may also negatively impact the timing of our realization of backlog.

Competition

We compete against various private companies, and foreign state-sponsored entities that provide satellite and aerial imagery and related products and services to the commercial market. Our major existing and potential competitors for high resolution satellite imagery include GeoEye, Astrium Geo-Information Services (formerly SPOT Image), ImageSat International N.Y. and RapidEye, plus numerous aggregators of imagery and imagery-related products and services, including Google and Microsoft. Most of these companies offer high-resolution imagery commercially from their archives of imagery in competition with our ImageLibrary. In addition, we compete against aerial providers of high-resolution imagery. Aerial imagery provides certain benefits over satellite-based imagery, most notably better resolution. We compete on the basis of:

 

   

the technical capabilities of our satellites, such as size of collection area, collection speed, revisit time, resolution, accuracy and spectral diversity;

 

   

satellite availability for tasked orders;

 

   

the size, comprehensiveness and relevance of our ImageLibrary;

 

   

distribution platform and tools that enable customers to easily access and integrate imagery;

 

   

timeliness and ready availability of imagery products and services that can be deployed quickly and cost-effectively; and

 

   

price.

For risks associated with competition, see Item 1A, Risk Factors.

Employees

As of December 31, 2011, we employed 708 full-time employees worldwide.

We currently do not have any collective bargaining agreements with our employees.

Company History

We were originally incorporated as EarthWatch, Incorporated on September 30, 1994 under the laws of the State of Colorado and reincorporated in the State of Delaware on August 21, 1995. We commenced development stage operations on March 31, 1995 with the contribution of the net assets of WorldView Imaging Corporation and certain assets of Ball Corporation. On August 22, 2002, we changed our name to DigitalGlobe, Inc. On January 4, 2007, we acquired GlobeXplorer, LLC, a producer and integrator of digital earth imagery and vector data, and AirPhotoUSA, LLC, an aerial imagery provider, for a total purchase price of $21.3 million.

Company Website

Our website can be accessed at www.digitalglobe.com . The website contains information about us and our operations. Through a link on the Investor Relations section of our website, copies of our filings with the SEC on Forms 8-K, 10-Q and 10-K can be viewed and downloaded free of charge as soon as reasonably practicable after the reports have been filed with the SEC. The information on our website is not incorporated by reference and is not a part of this Annual Report on Form 10-K.

 

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ITEM 1A.

RISK FACTORS

Risks

Our business is subject to many risks. The occurrence of any of the following risks could materially and adversely affect our business, financial condition, prospects, results of operations and cash flows. Additional risks and uncertainties not currently known to us or that we currently deem to be immaterial may also materially adversely affect our business, prospects, financial condition, results of operations and cash flows.

Risks Related To Our Business

The loss or reduction in scope of any one of our primary contracts will materially reduce our revenue. The majority of our revenue is currently derived from a single contract with a U.S. government agency that can be terminated at any time.

Approximately 77.2% of our revenue for the year ended December 31, 2011 was derived from our top five customers, including NGA, which accounted for approximately 60.1% of our revenue for the year ended December 31, 2011. These contracts may be terminated in the future, or may not be renewed or extended, and the loss of any one of these customers would materially reduce our revenue and could have a material adverse effect on our business financial condition and results of operations.

Our contracts with U.S. government agencies are subject to risks of termination or reduction in scope due to changes in U.S. government policies, priorities or funding level commitments to various agencies. Under the EnhancedView SLA, we are obligated to make a portion of the image tasking capacity of the WorldView constellation available to NGA, including specified priority access rights. To support requirements under the EnhancedView contract, we have begun the construction of our next satellite, WorldView-3, are investing in infrastructure to integrate certain of our operations more closely with NGA and are engaged in the expansion of our global network of regional ground terminals. As part of EnhancedView, we had previously agreed with NGA that we would lower the altitude of WorldView-2 from its current altitude of 770 km to an altitude of 680 km in September 2011. In August 2011 NGA notified us that it was waiving its right to have us lower WorldView-2 in September 2011. NGA continues to have the option to require us to lower the altitude of WorldView-2 to 496 km at any time after September 1, 2013, subject to receipt of all required regulatory approvals. The lowering of the orbital altitude would result in a decrease in the amount of square kilometers collected by WorldView-2. While we believe the decrease in collection capability would be offset by improved data capture capabilities on the ground resulting from the expansion of our ground terminal network, there can be no assurance that our current collection capability will be maintained. Our ability to service other customers could be negatively impacted if we are unable to maintain our current collection capacity. In addition, any inability on our part to meet the performance requirements of the EnhancedView contract could result in a breach of our contract with NGA. A breach of our contract with NGA or reduction in service to our other clients could have a material adverse effect on our business, financial condition and results of operations.

NGA may also terminate or suspend our contracts, including EnhancedView, at any time with or without cause. Although our NGA contracts generally involve fixed annual minimum commitments, such commitments are subject to annual Congressional appropriations and the federal budget process, and as a result, NGA may not continue to fund these contracts at current or anticipated levels. In addition, the sequestration process under the Budget Control Act of 2011 (PL 112-25) could have an adverse impact on the timing and amount of appropriations available for defense programs, including EnhancedView. Under the terms of the Budget Control Act, discretionary spending is capped, and any breach of the caps would result in automatic, across-the-board spending cuts, known as sequestration. The Budget Control Act assumed that spending cap recommendations would be recommended to Congress by the Joint Select Committee on Deficit Reduction. This Committee failed to come to agreement, and accordingly sequestration will be implemented beginning with the January 2013 budget in the event the law is not amended. Upon implementation, sequestration would be implemented by the Office of Management and Budget every January with the submission of the President’s budget over the next

 

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decade. This will result in reductions of approximately $600 billion in Department of Defense budgets over the Fiscal Year 2013-2021 period compared to currently projected budget levels. We cannot tell you how those cuts may affect the EnhancedView contract or other current or future business with the Department of Defense. Reductions in the current EnhancedView program or other current or future business with the Department of Defense resulting from sequestration could have a material adverse effect on our business, financial condition and results of operations

Any program delays encountered in implementing the infrastructure enhancements required to support the EnhancedView contract, or in the construction, launch and operational commissioning of our WorldView-3 satellite, may affect our ability to meet our obligations under the EnhancedView contract resulting in a reduction of a scope or termination of the contract, and may otherwise require us to increase our reliance on our existing satellites to meet our business needs, which could have a material adverse effect on our business, financial condition and results of operations.

Under the EnhancedView contract we are obligated to meet certain capacity and timeliness of delivery requirements. To meet these requirements, we are expanding our network of ground terminals around the world. We added five new ground terminals during 2011, and we expect to add three new ground terminals with all installations expected to be complete by September 2012. Any delay in bringing one or more ground terminals on-line may impact our ability to provide the capacity and meet delivery timelines required under the EnhancedView contract. In addition, delays may reduce the overall capacity available to service our non-NGA customers following any lowering of our WorldView-2 satellite.

To support requirements under the EnhancedView contract, we have contracted for and started manufacture of our WorldView-3 satellite. We currently expect to launch and commission WorldView-3 in the second half of 2014. The manufacturing, testing and launch of satellites, involves complex processes and technology and we rely on third party contractors for the manufacturing, testing and launch of our satellites, including WorldView-3. Many factors, including, but not limited to, availability of parts, subcontractor and supplier delays and anomalies discovered during testing, may result in significant delays to the WorldView-3 program. In addition, while we have contracted with Lockheed Martin Commercial Launch Services for the launch of WorldView-3 in mid-2014, launch windows and specific dates, once scheduled, are subject to change and may be materially delayed for reasons beyond our control, including intervening launch failures of other satellites, reduced availability of launch facilities and support crew, and preemption by certain government launches. After launch, the satellite must be calibrated and tested to confirm operational capability, a commissioning process that typically takes several months. The satellite may not pass the operational commissioning tests or may not otherwise operate as required. For example, satellites may experience technical difficulties communicating with the ground station center or collecting imagery in the same quality or volume that was intended. The failure to construct and launch WorldView-3 on time or to achieve operational commissioning on time or at all could affect our ability to meet our obligations under the EnhancedView contract and may otherwise limit the anticipated volume of imagery products and services available to meet our business needs, which could have a material adverse effect on our business, financial condition and results of operations.

Breach of our system security measures or loss of our secure facility clearance and accreditation could result in interruption, delay or suspension of our ability to provide our products and services, and could result in loss of current and future business, including our U.S. government contracts.

Breach of our system security could materially adversely affect our business. Our business involves the transmission and storage of large quantities of electronic data, including the imagery comprising our ImageLibrary. In addition, our business is becoming increasingly web-based, allowing our customers to access and take delivery of imagery from our ImageLibrary over the Internet. From time to time, we have experienced computer virus and other forms of third party attacks on our systems that, to date, have not had a material adverse effect on our business. We cannot assure you, however, that future attacks will not materially adversely affect our business.

 

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Despite the implementation and continued upgrading of security measures, our network infrastructure may be vulnerable to computer viruses, unauthorized third party access, or other problems caused by third parties, which could lead to interruptions, delays or suspension of our operations, loss of imagery from our ImageLibrary, as well as the loss or compromise of technical information or customer information. Inappropriate use of the Internet by third parties including attempting to gain unauthorized access to information or systems – commonly known as “cracking” or “hacking” – could also potentially jeopardize the overall security of our systems, and could deter certain customers from doing business with us. In addition, a security breach that involved classified or other sensitive government information, or certain controlled technical information, could subject us to civil or criminal penalties, and could result in loss of our secure facility clearance and other accreditations, loss of our government contracts, loss of access to classified information, loss of export privileges, or debarment as a government contractor.

Because the techniques used to obtain unauthorized access, or to otherwise infect or sabotage systems change frequently and often are not recognized until launched against a target, we may be unable to anticipate these techniques or to implement adequate preventative measures. We may also need to expend significant resources to protect against security breaches. The risk that these types of events could seriously harm our business is likely to increase as we expand the number of web based products and services we offer as well as increase the number of countries within which we do business.

Changes in U.S. government policy regarding use of commercial data providers, or material delay or cancellation of the planned U.S. government EnhancedView program may have a material adverse effect on our revenue and our ability to achieve our growth objectives.

Current U.S. government policy encourages the use by the U.S. government of commercial data providers to support U.S. national security objectives. We are considered by the U.S. government to be a commercial data provider. U.S. government policy is subject to change and any change in policy away from supporting the use of commercial data providers to meet U.S. government imagery needs could materially affect our revenue and our ability to achieve our growth objectives.

Management’s determination that material weaknesses exist in our internal control over financial reporting and our disclosure controls and procedures could have a material adverse impact on us.

We are required to maintain internal control over financial reporting to provide reasonable assurance regarding the reliability of financial reporting and the preparation of our consolidated financial statements for external purposes in accordance with generally accepted accounting principles. We are also required to maintain disclosure controls and procedures designed to ensure that information required to be disclosed in the reports we file or submit under the Exchange Act is recorded, processed, summarized and reported within the time periods specified in the rules and forms of the SEC. In Item 9A of this Annual Report on Form 10-K, management reports that material weaknesses exist in our internal control over financial reporting, principally that the Company did not maintain effective controls over the accuracy, completeness and presentation of the accounting for DAP contracts and also that the Company did not maintain a sufficient complement of personnel with appropriate level of accounting knowledge, experience and training. Management has also concluded that our disclosure controls and procedures were not effective at the reasonable assurance level as of December 31, 2011 because of the material weaknesses in internal controls over financial reporting that have been identified.

We are currently in the process of remediating the material weaknesses we have identified. If we are unable to remediate our current material weaknesses or if we have additional material weaknesses in the future and are not able to remedy such material weaknesses in a timely manner, we may be unable to provide our stockholders with the required financial information in a timely, and reliable manner which could subject us to stockholder litigation, regulatory enforcement actions or other adverse consequences. This could materially and adversely impact our business and financial condition, perceptions of us among investors and other constituencies, and the market value of our securities.

 

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Interruption or failure of our infrastructure could hurt our ability to effectively perform our daily operations and provide our products and services, which could damage our reputation and harm our operating results.

The availability of our products and services depends on the continuing operation of our satellite operations infrastructure, information technology and communications systems. Any downtime, damage to or failure of our systems could result in interruptions in our service, which could reduce our revenue and profits. Our systems are vulnerable to damage or interruption from floods, fires, power loss, telecommunications failures, computer viruses, computer denial of service attacks or other attempts to harm our systems. We do not currently maintain a back-up data center from which we can continue to collect, process and deliver imagery in the event of the loss of our primary capabilities. In the event we are unable to collect, process and deliver imagery from our primary facility in Longmont, Colorado, our daily operations and operating results would be materially and adversely affected. In addition, our ground station centers are vulnerable to damage or interruption from human error, intentional bad acts, earthquakes, hurricanes, floods, fires, war, terrorist attacks, power losses, hardware failures, systems failures, telecommunications failures and similar events. The occurrence of any of the foregoing could result in lengthy interruptions in our services and/or damage our reputation, which could have a material adverse effect on our financial condition and results of operations.

If our satellites fail to operate as intended, our ability to collect imagery and market our products and services successfully could be materially and adversely affected.

Our satellites employ advanced technologies and sensors that are exposed to severe environmental stresses in space that could affect our satellites’ performance. Hardware component problems in space could lead to deterioration in performance or loss of functionality of a satellite, with attendant costs and revenue losses. In addition, human operators may execute improper implementation commands that may negatively impact a satellite’s performance. Exposure of our satellites to an unanticipated catastrophic event, such as a meteor shower or a collision with space debris, could reduce the performance of, or completely destroy, the affected satellite.

We cannot assure you that our QuickBird, WorldView-1 and WorldView-2 satellites will continue to operate successfully in space throughout their expected operational lives. Even if a satellite is operated properly, technical flaws in that satellite’s sensors or other technical deficiencies could significantly hinder its performance, which could materially affect our ability to collect imagery and market our products and services successfully.

If we suffer a partial or total loss of a deployed satellite, we would need a significant amount of time and would incur substantial expense to replace that satellite. We may experience other problems with our satellites that may reduce their performance. During any period of time in which a satellite is not fully operational, we may lose most or all of the revenue that otherwise would have been derived from that satellite. In addition, we may not have on hand, or be able to obtain in a timely manner, the necessary funds to cover the cost of any necessary satellite replacement. Our inability to repair or replace a defective satellite or correct any other technical problem in a timely manner could result in a significant loss of revenue.

We are highly dependent upon our ImageLibrary and our failure or inability to protect and maintain the earth imagery content stored in our ImageLibrary could have a material adverse effect on our business, financial condition and results of operations.

Approximately 54.5% of our revenue is generated from our ImageLibrary, excluding EnhancedView SLA. Our operations depend upon our ability to maintain and protect our earth imagery content and our ImageLibrary against damage that may be caused by fire and other natural disasters, power failures, telecommunications failures, terrorist attacks, unauthorized intrusion, computer viruses, equipment malfunction or inadequacy, firewall breach or other events. The satellite imagery content we collect is downloaded directly to our Longmont, Colorado facility and then stored in our ImageLibrary for sale to customers. Our aerial imagery is collected and processed by our aerial suppliers and then delivered to us to be uploaded to our ImageLibrary. We back up our

 

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imagery and permanently store it with a third party data storage provider. Notwithstanding precautions we have taken to protect our ImageLibrary, there can be no assurance that a natural disaster or other event would not result in a prolonged interruption in our ability to provide access to or deliver imagery from our ImageLibrary to our clients. The temporary or permanent loss or disruption of access to our ImageLibrary could impair our ability to supply current and future customers with imagery content, have a negative impact on our revenue and cause harm to our reputation. Any impairment in our ability to supply our customers with imagery content could affect our ability to retain or attract customers, which would have a material adverse effect on our business, financial condition and results of operations.

The market may not accept our imagery products and services. You should not rely upon our historic growth rates as an indicator of future growth.

Our success depends on existing markets accepting our imagery products and services and our ability to develop new markets. Our business plan is based on the assumption that we will generate significant future revenue from sales of imagery products and services produced from our QuickBird, WorldView-1, WorldView-2 satellites, our planned WorldView-3 satellite and our other imagery content sources. The commercial sale of high-resolution earth imagery and related products and services is a relatively new industry. Consequently, it is difficult to predict the ultimate size of the market and the acceptance by the market of our products and services. Our business strategy and projections rely on a number of assumptions, some or all of which may be incorrect. Actual markets could vary materially from the potential markets that we have identified.

We cannot accurately predict whether our products and services will achieve significant market acceptance or whether there will be a market for our products and services on terms we find acceptable. Market acceptance of our commercial high-resolution earth imagery and related products and services depends on a number of factors, including the quality, scope, timeliness, sophistication, price, and the availability of substitute products and services. Lack of significant market acceptance of our offerings, or other products and services that utilize our products and services, delays in acceptance, failure of certain markets to develop or our need to make significant investments to achieve acceptance by the market would negatively affect our business, financial condition and results of operations.

We may not continue to grow in line with historical rates, or at all. If we are unable to achieve sustained growth, we may be unable to execute our business strategy, expand our business or fund other liquidity needs and our prospects, financial condition and results of operations could be materially and adversely affected.

We face competition that may cause us to have to reduce our prices or to lose market share.

Our products and services compete with satellite and aerial imagery and related products and services offered by a range of private and government providers. Our current or future competitors may have greater financial, personnel and other resources than we have. Our major existing competitors include GeoEye, Astrium Geo-Information Services, ImageSat International N.V., RapidEye, foreign governments including India, South Korea, Taiwan, and others that sell their data commercially, as well as numerous aggregators of imagery and imagery-related products and services, including Google and Microsoft. In addition, we compete against aerial providers of high-resolution imagery, whose offerings provide certain benefits over satellite-based imagery, including better resolution and accuracy. The value of our imagery may also be diluted by Earth imagery that is available free of charge.

The U.S. government and foreign governments also may develop, construct, launch and operate their own imagery satellites, which could reduce their need to rely on commercial suppliers. In addition, such governments could sell or provide free of charge Earth imagery from their satellites in the commercial market and thereby compete with our imagery products and services. These governments could also subsidize the development, launch and operation of imagery satellites by our current or future competitors.

In December 2011, Astrium Geo-Information Services successfully launched its high-resolution satellite, Pleiades-1, which is expected to begin commercial operations in the first half of 2012. Its twin satellite,

 

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Pleiades-2, is expected to be launch in 2013. In addition, two medium resolution satellites, SPOT 6 and SPOT 7, are currently under construction and expected to be launched in 2012 and 2014, respectively. Additionally, GeoEye continues to build its next high-resolution satellite, GeoEye-2, and expects to launch it in the first half of 2013, with commercial operations beginning in the second half of 2013.

Our competitors, including GeoEye and Astrium Geo-Information Services, or potential competitors with greater resources than ours could in the future offer satellite-based imagery or other products and services with more attractive features than our products and services. The emergence of new remote imaging technologies or the continued growth of low-cost imaging satellites, such as those built and sold by Surrey Satellite Technologies, Ltd, could negatively affect our marketing efforts. More importantly, if competitors develop and launch satellites or other imagery content sources with more advanced capabilities and technologies than ours, or offer services at lower prices than ours, our business and results of operations could be harmed. From time to time, we have experienced decreases in the average sales prices of some of our products and services. Due to competitive pricing pressures, new product introductions by us or our competitors, or other factors, the average selling price of our products and services may further decrease. If we are unable to offset decreases in our average selling prices by increasing our sales volumes or by adjusting our product mix, our revenue and operating margins may decline and our financial position may be harmed.

Changes in U.S. or foreign laws and regulations could have a material adverse effect on our operations and financial condition.

Our industry is highly regulated due to the sensitive nature of satellite technology. We cannot assure you that the laws and regulations governing our business and operations, including the distribution of satellite imagery, will not change in the future. Our business and operating results may be materially and adversely affected if we are required to alter our business operations to comply with such changes or if our ability to sell our products and services on a global basis is reduced or restricted due to increased U.S. or foreign government regulation.

Failure to obtain or maintain regulatory approvals could result in service interruptions or could impede us from executing our business plan.

Approvals.     Our business requires licenses from the DoC, through NOAA. Under our NOAA licenses, the U.S. government reserves the right to interrupt service or limit our ability to distribute satellite images when foreign policy or U.S. national security interests are affected. In addition, NOAA has the right to review and approve the terms of certain of our agreements with international customers, including our DAP customers. We currently have the necessary approvals for our existing international customers. However, such reviews in the future could delay or prohibit us from executing new international agreements. The inability to get approvals for DAP customers could materially affect our ability to establish and grow our DAP business. In addition, should we not get approvals in a timely manner our products and services may not be competitive.

Export Approvals.     The ground station equipment and related technology that is purchased by certain of our DAP customers is controlled under the ITAR. We, or our suppliers, must obtain export licenses from the DoS, and in some cases from foreign government agencies, in order to export ground station equipment and related technology to our DAP customers. Export licenses can take up to three months or longer to be processed and neither the DoS nor any corresponding foreign government agency are obligated to approve any license application. Our inability or the inability of our suppliers to get required export approvals for equipment and technology supporting DAP could materially affect our ability to establish and grow our DAP business.

FCC Approvals.     Our operation of satellites and ground station centers also requires licenses from the FCC. The FCC regulates the construction, launch and operation of our satellites, the use of satellite frequency spectrum and the licensing of our ground station centers located within the United States. We are also subject to the FCC’s rules and regulations and the terms of our licenses, which require us to comply with various operating conditions and requirements. The current licenses of our satellites expire in September of 2012 and those of our

 

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ground station centers expire in 2019 and 2021. While the FCC generally renews licenses routinely, there can be no assurance that our licenses will be renewed at their expiration dates on favorable terms or without adverse conditions. Failure to renew these licenses could have a material and adverse effect on our ability to generate revenue and conduct our business as currently expected. In addition, we must apply for and receive a license for our WorldView-3 satellite. Failure to receive the required FCC license for WorldView-3 could have a material adverse effect on our ability to meet our obligations under the EnhancedView contract.

International Registration and Approvals.     The use of satellite frequency spectrum internationally is subject to the rules and requirements of the ITU. Additionally, satellite operators must abide by the specific laws of the countries in which downlink services are provided from the satellite to ground station centers within such countries. The FCC has coordinated the operations for each of our satellites pursuant to the ITU requirements.

Coordination of our satellites with other satellite systems is required by the ITU to help prevent harmful frequency interference from or into existing or planned satellite operations. We do not expect significant issues relating to the coordination of our satellites due to the nature of satellite imaging operations.

Our foreign DAP customers are responsible for securing necessary licenses and operational authority to use the required spectrum in each country into which we will downlink high resolution commercial earth imagery. If such customers are not successful in obtaining the necessary approvals, we will not be able to distribute real-time imagery to those customers. Our inability to offer real-time access service in a significant number of foreign countries could negatively affect our business. In addition, regulatory provisions in countries where we wish to operate may impose unduly burdensome restrictions on our operations. Our business may also be adversely affected if the national authorities where we plan to operate adopt treaties, regulations or legislation unfavorable to foreign companies.

Global economic conditions may adversely impact our business, operating results or financial condition.

Disruption and volatility in global financial markets may lead to increased rates of default and bankruptcy, and may negatively impact consumer spending levels. These macroeconomic developments could adversely affect our business, operating results or financial condition. Current or potential customers, including foreign governments, may delay or decrease spending on our products and services as their business and/or budgets are impacted by economic conditions. The inability of current and potential customers to pay us for our products and services may adversely affect our earnings and cash flows.

We are dependent on foreign resellers for our international revenue. If these resellers fail to market or sell our products and services successfully, our business would be harmed.

In 2011, we generated $111.2 million in revenue, or 32.8% of our total revenue, from our foreign resellers and partners. We rely on our foreign regional resellers and partners to market and sell the majority of our products and services in the international market. We have intensified our efforts to further develop our operations in overseas markets. Our foreign resellers and partners may not have the skill or experience to develop regional commercial markets for our imagery products and services, or may have competing interests that negatively affect their sales of our products and services. If we fail to enter into reseller agreements on a timely basis or if our foreign resellers and partners fail to market and sell our imagery products and services successfully, these failures could negatively impact our business, financial condition and results of operations.

Our international business exposes us to risks relating to increased regulation and political or economic instability in foreign markets, which could adversely affect our revenue.

In 2011, approximately 32.8% of our revenue was derived from international sales, and we intend to continue to pursue international contracts. International operations are subject to certain risks, such as:

 

   

changes in domestic and foreign governmental regulations and licensing requirements;

 

   

deterioration of relations between the United States and a particular foreign country;

 

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increases in tariffs and taxes and other trade barriers;

 

   

changes in political and economic stability, including fluctuations in the value of foreign currencies, which may make payment in U.S. dollars, as provided for under some of our existing contracts, more expensive for foreign customers; and

 

   

affects of austerity programs or similar significant budget reduction programs; and

 

   

difficulties in obtaining or enforcing judgments in foreign jurisdictions.

These risks are beyond our control and could have a material and adverse effect on our business.

We depend on third parties to provide us with aerial imagery. If we are unable to obtain aerial imagery at sufficient resolution, quality, or on commercially reasonable terms, our ability to supplement our content library may be harmed, which could have a material adverse effect on our business, financial condition and results of operations.

We do not own planes or other similar aircraft and therefore depend on a network of aerial imagery suppliers to provide us with aerial imagery to include in our ImageLibrary. The imagery must meet certain quality specifications, including resolution requirements, to allow it to be used by us in products and services we sell to our customers. Aerial imagery is collected and processed by our aerial suppliers and then delivered to us to be uploaded into our ImageLibrary. If our aerial imagery suppliers are unable to meet quality specifications or delivery time lines, the comprehensiveness and currency of our ImageLibrary could be diminished or become compromised. In addition, any inability to reach mutually acceptable commercial arrangements with our current aerial suppliers, or find new aerial providers to supply us with aerial imagery on commercially reasonable terms, could result in our inability to maintain or expand our customer base or to bring to market certain products, which could have a material adverse effect on our business, financial condition and results of operations.

We depend upon our ability to attract, train and retain employees. Our inability to do so, or the loss of key personnel, would seriously harm our business.

Because of the specialized nature of our business, we rely heavily on our ability to attract and retain qualified scientific, technical, sales, marketing and managerial personnel. The loss of one or more of our senior executive officers could result in the loss of knowledge, experience and technical expertise within the satellite imagery sector, which would be detrimental to us if we cannot recruit suitable replacements in a timely manner. The competition for qualified personnel in the commercial high-resolution earth imagery industry is intense. Due to this intense competition, we may be unable to continue to attract and retain the qualified personnel necessary for the development of our business or to recruit suitable replacement personnel. The loss of the services of any member of our senior management or the inability to hire or retain experienced management personnel could adversely affect our ability to execute our business plan and harm our operating results.

Satellites have limited operational lives and are expensive to replace. Loss of, or damage to, a satellite may require us to seek additional financing from outside sources, which we may be unable to obtain on favorable terms, if at all.

We determine a satellite’s useful life, or its expected operational life, using a complex calculation involving the probabilities of failure of the satellite’s components from design or manufacturing defects, environmental stresses, estimated remaining fuel or other causes. The expected ends of the operational lives of our currently in-orbit satellites are as follows:

 

Satellite

   Expected End of
Operational Life
 

QuickBird

     Q3 2013   

WorldView-1

     Q2 2018   

WorldView-2

     Q1 2021   

 

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The expected operational lives of these satellites are affected by a number of factors, including the quality of construction, the supply of fuel, the expected gradual environmental degradation of solar panels, the durability of various satellite components and the orbits in which the satellites are placed. The failure of satellite components could cause damage to or loss of the use of a satellite before the end of its expected operational life. Electrostatic storms or collisions with other objects could also damage our satellites. We cannot assure you that each satellite will remain in operation until the end of its expected operational life. Furthermore, we expect the performance of each satellite to decline gradually near the end of its expected operational life. We can offer no assurance that QuickBird, WorldView-1 or WorldView-2 will maintain their prescribed orbits or remain operational.

We anticipate using funds generated from operations to fund the construction and launch of any future satellites, including WorldView-3. If we do not generate sufficient funds from operations, we may need to obtain additional financing from outside sources to deploy any future satellites, including WorldView-3. If we do not generate sufficient funds from operations and cannot obtain financing, we will not be able to deploy any future satellites, including WorldView-3, or be able to replace any of our operating satellites at the end of their operational lives. We cannot assure you that we will be able to generate sufficient funds from operations or raise additional capital on favorable terms or on a timely basis, if at all, to develop or deploy additional high-resolution satellites.

Limited insurance coverage and availability may prevent us from obtaining insurance to cover all risks of loss.

As of December 31, 2011, we maintain the following insurance coverage on our satellite constellations:

 

Satellite

   Policy Period      Coverage
(in
millions)
 

QuickBird

     10/2011 — 10/2012       $ 11.0   

WorldView-1

     10/2011 — 10/2012         235.0   

WorldView-2

     10/2011 — 10/2012         182.0   

WorldView-2

     10/2009 — 10/2012         68.0   

We intend to continue this coverage to the extent it remains available at acceptable premiums. It is anticipated that the insurance proceeds received in connection with a partial or total loss of QuickBird, WorldView-1 or WorldView-2 may not be sufficient to cover the replacement cost, if we choose to do so, of an equivalent high-resolution satellite. In addition, this insurance will not protect us against all losses to our satellites due to specified exclusions, deductibles and material change limitations, and it may be difficult to insure against certain risks, including a partial deterioration in satellite performance.

The price and availability of insurance have fluctuated significantly since we began offering commercial services in 2001. Although we have historically been able to obtain adequate insurance coverage for our in-orbit satellites, we cannot guarantee that we will be able to do so in the future. Although we intend to maintain insurance for all of our operating satellites, any determination we make as to whether to obtain insurance coverage will depend on a variety of factors, including the availability of insurance in the market, the cost of available insurance, and the redundancy of our operating satellites. Insurance market conditions or factors outside our control at the time we are in the market for the required insurance, such as failure of a satellite using similar components, could cause premiums to be significantly higher than current estimates and could reduce amounts of available coverage. Higher premiums on insurance policies will increase our costs and consequently reduce our operating income by the amount of such increased premiums. If the terms of in-orbit insurance policies become less favorable than those currently available, there may be limits on the amount of coverage that we can obtain or we may not be able to obtain insurance at all. Even if obtained, our in-orbit operations insurance will not cover any loss in revenue incurred as a result of a partial or total satellite loss.

 

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We have a substantial amount of indebtedness, which may adversely affect our cash flow and our ability to operate our business, including our ability to incur additional indebtedness.

As of December 31, 2011, our total indebtedness was $500.0 million. Our balance, $486.6 million which is net of discounts of $13.4 million, represented 50.2% of our total capitalization. Our indebtedness increases the possibility that we may be unable to generate sufficient cash to pay, when due, the principal, interest or other amounts due with respect to our indebtedness. We established a $500 million, seven-year senior term loan facility and a $100 million, five-year senior secured revolving credit facility, the terms of which are set forth in a Credit and Guaranty Agreement dated as of October 12, 2011 among the Company, the guarantors party thereto, the lenders named therein and J.P. Morgan Chase Bank, N.A., as administrative agent and as collateral agent. As of today, we have not drawn any amounts under the revolving Credit Facility. Our indebtedness could have several consequences, including:

 

   

increasing our vulnerability to adverse economic, industry or competitive developments;

 

   

requiring a substantial portion of cash flow from operations to be dedicated to the payment of principal and interest on our indebtedness, therefore reducing our ability to use our cash flow to fund our operations, capital expenditures and future business opportunities;

 

   

restricting us from making strategic acquisitions;

 

   

limiting our ability to obtain additional financing for working capital, capital expenditures, product development, debt service requirements, acquisitions and general corporate or other purposes; and

 

   

limiting our flexibility in planning for, or reacting to, changes in our business or the industry in which we operate, placing us at a competitive disadvantage compared to our competitors who are less highly leveraged and who, therefore, may be able to take advantage of opportunities that our leverage prevents us from exploiting.

The credit agreement governing our senior secured credit facilities contains a number of restrictions and covenants that, among other things, limit our ability to incur additional indebtedness, make investments, pay dividends or make distributions to our stockholders, grant liens on our assets, sell assets, enter into a new or different line of business, enter into transactions with our affiliates, merge or consolidate with other entities or transfer all or substantially all of our assets, and enter into sale and leaseback transactions.

Our ability to comply with these restrictions and covenants in the future is uncertain and will be affected by the levels of cash flow from our operations and events or circumstances beyond our control. Our failure to comply with any of the restrictions and covenants under our senior secured credit facilities could cause all of our existing indebtedness to be immediately due and payable. If our indebtedness is accelerated, we may not be able to repay our indebtedness or borrow sufficient funds to refinance it. If our indebtedness is in default for any reason, our business, financial condition and results of operations could be materially and adversely affected.

We expect that the price of our common stock will fluctuate substantially.

The market price of our common stock has been, and is likely to continue to be, volatile. Factors that could contribute to the volatility of our stock include:

 

   

termination or expiration of one or more of our key contracts, or a change in scope or purchasing levels under one or more of our contracts, including the EnhancedView contract, our DAP contracts, or other large contracts;

 

   

unfounded rumors and leaks of information, or formal announcements regarding federal budget cuts, including, but not limited to, reduction in budgets affecting the Department of Defense;

 

   

failure of our satellites to operate as designed;

 

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loss or damage to any of our satellites;

 

   

changes in U.S. or foreign governmental regulations or in the status of our regulatory approvals, clearances or future applications;

 

   

our announcements or our competitors’ announcements regarding new products or services, enhancements, significant contracts, acquisitions or strategic investments;

 

   

changes in the availability of insurance;

 

   

changes in earnings estimates or recommendations by securities analysts, if any, who cover our common stock;

 

   

fluctuations in our quarterly financial results or the quarterly financial results of companies perceived to be similar to us;

 

   

success of competitive products and services;

 

   

changes in our capital structure, such as future issuances of securities, sales of large blocks of common stock by our stockholders or the incurrence of additional debt;

 

   

investors’ general perception of us, including any perception of misuse of sensitive information;

 

   

changes in general global economic and market conditions;

 

   

changes in industry conditions; and

 

   

changes in regulatory and other dynamics.

In addition, in recent years, the stock market has experienced significant price and volume fluctuations that have particularly affected the market prices of equity securities of many companies in the technology sector, which have often been unrelated to their operating performance or prospects for future operations. These broad fluctuations may adversely impact the market price of our common stock. Future market movements may materially and adversely affect the market price of our common stock.

Provisions in our amended and restated certificate of incorporation and by-laws and Delaware law might discourage, delay or prevent a change of control of our company or changes in our management and, therefore, depress the trading price of our common stock.

Provisions of our amended and restated certificate of incorporation and by-laws and Delaware law may discourage, delay or prevent a merger, acquisition or other change in control that stockholders may consider favorable. These provisions may also prevent or frustrate attempts by our stockholders to replace or remove our management. These provisions include: the existence of a classified board of directors; limitations on the removal of directors; advance notice requirements for stockholder proposals and director nominations; the inability of stockholders to act by written consent or to call special meetings; the ability of our board of directors to make, alter or repeal our by-laws; and provisions that permit the redemption of stock from foreign stockholders where necessary, in the judgment of our board of directors, to protect our licenses and registrations.

We do not currently intend to pay dividends on our common stock.

We have never declared or paid any cash dividends on our common stock and do not anticipate paying cash dividends on our common stock. We anticipate that we will retain all of our future earnings, if any, for use in the development and expansion of our business and for general corporate purposes. Any determination to pay dividends on our common stock in the future will be at the discretion of our board of directors.

 

ITEM 1B.

UNRESOLVED STAFF COMMENTS

None.

 

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ITEM 2.

PROPERTIES

We currently lease approximately 233,903 square feet of office and operations space in two locations in Longmont, Colorado. This space includes our principal executive offices. The rent varies in amounts per year through the expiration of the lease in August 2015.

We believe that our existing facilities are adequate for our current needs.

 

ITEM 3.

LEGAL PROCEEDINGS

From time to time, we are a party to various litigation matters incidental to the conduct of our business. We are not presently party to any legal proceedings the resolution of which, we believe, would have a material adverse effect on our business, operating results, financial condition or cash flows.

 

ITEM 4.

MINE SAFETY DISCLOSURES

Not applicable.

 

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PART II

 

ITEM 5. MARKET FOR REGISTRANT’S COMMON EQUITY, RELATED STOCKHOLDER MATTERS AND ISSUER PURCHASES OF EQUITY SECURITIES

Our common stock has been listed on the NYSE and traded under the symbol “DGI” since our initial public offering (IPO) in May 2009. The following table sets forth, for the periods indicated, the high, low and last sale prices in dollars on the NYSE for our common stock.

 

     High      Low      Last Sale  

2011

        

Fourth Quarter

   $ 22.08       $ 13.59       $ 17.11   

Third Quarter

     27.42         18.00         19.43   

Second Quarter

     29.39         23.31         25.41   

First Quarter

     32.82         28.00         28.03   

2010

        

Fourth Quarter

   $ 32.95       $ 28.71       $ 31.71   

Third Quarter

     32.46         25.13         30.40   

Second Quarter

     28.80         24.66         26.30   

First Quarter

     28.23         21.69         27.95   

2009

        

Fourth Quarter

   $ 26.02       $ 21.08       $ 24.20   

Third Quarter

     22.84         17.10         22.37   

Second Quarter (since May 14, 2009 IPO)

     25.00         16.95         19.20   

At February 27, 2012, there were approximately 302 record holders of our common stock. This figure does not reflect beneficial ownership of shares held in nominee/street name.

Securities Authorized for Issuance Under Equity Compensation Plans

The following table provides certain information with respect to our equity compensation plans in effect as of December 31, 2011:

 

Plan Category

   Number of securities to
be issued upon exercise
of outstanding options
and rights (a)
     Weighted-average
exercise price of
outstanding
options and
rights (b)(1)
     Number of securities
remaining available
for issuance under
equity compensation
plans (excluding
securities reflected
in column (a)) (c)
 

Equity compensation plans approved by security holders

        

2007 Employee Stock Option Plan

     3,210,062       $ 24.47         953,668   
  

 

 

    

 

 

    

 

 

 

1999 Equity Incentive Plan(2)

     286,138       $ 12.50           
  

 

 

    

 

 

    

 

 

 

All plans approved by security holders

                       
  

 

 

    

 

 

    

 

 

 

Equity compensation plans not approved by security holders

                       
  

 

 

    

 

 

    

 

 

 

Total

     3,496,200                 953,668   
  

 

 

    

 

 

    

 

 

 

 

(1)

Does not take into account 371,777 restricted stock awards and restricted stock units granted to directors and officers under our 2007 Employee Stock Option Plan and 1999 Equity Incentive Plan.

 

(2)

We no longer grant equity awards under this plan although stock options remain outstanding under such plan.

 

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The graph below compares the percentage change in our cumulative total shareholder return on its common stock with the cumulative total return of the S&P Composite 500 Stock Index, GeoEye Inc., and the Russell 2000 for the period from the IPO date, May 14, 2009 through December 31, 2011. It assumes $100 was invested on May 14, 2009 and that dividends have been reinvested.

LOGO

 

Total Return Analysis    5/14/2009      12/31/2009      12/31/2010      12/31/2011  

DigitalGlobe, Inc.

   $ 100.00       $ 127.37       $ 166.89       $ 90.05   

GeoEye

     100.00         112.83         171.55         89.92   

Russell 2000

     100.00         131.28         166.53         159.58   

S&P 500

     100.00         126.75         145.84         148.92   

Dividends

We have never declared or paid any cash dividends on our common stock and do not anticipate paying cash dividends on our common stock. We anticipate that we will retain all of our future earnings, if any, for use in the development and expansion of our business and for general corporate purposes. Any determination to pay dividends in the future will be at the discretion of our board of directors and will be dependent on then-existing conditions, including our financial condition and results of operations, contractual restrictions, including restrictive covenants contained in our financing facilities, capital requirements and other factors.

Use of Proceeds

On May 13, 2009, our registration statement (File No. 333-150235) was declared effective for our IPO, pursuant to which we sold 1,366,256 shares of our common stock.

As a result of the offering, we received net proceeds of approximately $19.0 million, after deducting underwriting fees of $1.8 million and additional offering-related expenses of approximately $3.3 million, for total expenses to us of approximately $5.1 million. No offering expenses were paid directly or indirectly to any of our directors or officers (or their associates). A portion of the underwriting fee was paid to Morgan Stanley & Co., Incorporated, an affiliate owning 10% or more of our equity securities. During 2011, we have used the net proceeds from the IPO of $19.0 million to pay for development of our WorldView-3 satellite.

 

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ITEM 6.

SELECTED FINANCIAL DATA

The selected consolidated financial information set forth below for each of the years ended December 31, 2007, 2008, 2009, 2010 and 2011 has been derived from our audited consolidated financial statements. The information below should be read in conjunction with “Management’s Discussion and Analysis of Financial Condition and Results of Operations” and the consolidated financial statements and notes thereto in Item 8 of this report.

Summary Financial Data

 

     Year Ended December 31,  

(in millions, except per share data)

   2007      2008      2009      2010(1)
Revised
     2011  

Revenue

   $ 151.7       $ 275.2       $ 281.9       $ 322.5       $ 339.5   

Income (loss) before income taxes

     37.9         91.9         78.4         6.8         (46.0

Net income (loss)

     95.8         53.8         47.4         2.5         (28.1

Earnings (loss) per share:

              

Basic

   $ 2.21       $ 1.24       $ 1.07       $ 0.05       $ (0.61

Diluted

   $ 2.18       $ 1.22       $ 1.06       $ 0.05       $ (0.61

Total assets

     907.5         980.2         1,140.5         1,268.1         1,451.6   

Long-term debt

     230.0         274.6         343.5         346.1         481.6   

Stockholders’ equity

     344.6         402.3         479.5         498.9         487.4   

Adjusted EBITDA(2)

   $ 80.0       $ 149.3       $ 143.9       $ 180.3       $ 226.6   

 

(1)

The Company revised its 2010 financial information, see Note 3 to the Consolidated Financial Statements for more detail.

 

(2)

Adjusted EBITDA is defined as net income or loss adjusted for depreciation and amortization, net interest income or expense, income tax expense (benefit), loss on disposal of assets, restructuring, loss on early extinguishment of debt, loss on derivative instrument, non-cash stock compensation expense, EnhancedView deferred revenue and EnhancedView outstanding invoices not yet paid by NGA and amortization of pre-FOC payments related to NextView. EnhancedView outstanding invoices not yet paid by NGA represent an irrevocable right to be paid in cash by NGA.

Adjusted EBITDA is not a recognized term under generally accepted accounting principles, or GAAP, in the United States and may not be defined similarly by other companies. Adjusted EBITDA should not be considered an alternative to net income, as an indication of financial performance, or as an alternative to cash flow from operations as a measure of liquidity. There are limitations to using non-GAAP financial measures, including the difficulty associated with comparing companies in different industries that use similar performance measures whose calculations may differ from ours.

Adjusted EBITDA is a key measure used in internal operating reports by management and the board of directors to evaluate the performance of our operations and is also used by analysts, investment banks and lenders for the same purpose. Adjusted EBITDA has also been a key driver of the company-wide bonus incentive plan. Adjusted EBITDA is a measure of our current period operating performance, excluding charges for capital, depreciation related to prior period capital expenditures and items which are generally non-core in nature, and including EnhancedView deferred revenue and EnhancedView outstanding invoices not yet paid by NGA and excluding the amortization of pre-FOC payments related to our NextView contract. EnhancedView outstanding invoices not yet paid by NGA represent an irrevocable right to be paid in cash by NGA.

We believe that the elimination of material non-cash, non-operating items enables a more consistent measurement of period to period performance of our operations. In addition, we believe that elimination of these items in combination with the addition of the nonrefundable EnhancedView deferred revenue and EnhancedView outstanding invoices not yet paid by NGA as well as the elimination of amortization of pre-FOC payments

 

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related to NextView, facilitate comparison of our operating performance to companies in our industry. We believe this Adjusted EBITDA measure is particularly important in a capital intensive industry such as ours, in which our current period depreciation is not a good indication of our current or future period capital expenditures. The cost to construct and launch a satellite and build the related ground infrastructure may vary greatly from one satellite to another, depending on the satellite’s size, type and capabilities. For example, our QuickBird satellite, which we are currently depreciating, cost significantly less than our WorldView-1 and WorldView-2 satellites. Current depreciation expense is not indicative of the revenue generating potential of the satellite.

Adjusted EBITDA excludes interest income, interest expense, income taxes and loss on early extinguishment of debt because these items are associated with our capitalization and tax structures. Adjusted EBITDA also excludes depreciation and amortization expense because these non-cash expenses reflect the impact of prior capital expenditure decisions which are not indicative of future capital expenditure requirements. Adjusted EBITDA excludes non-cash stock compensation expense, because these items are non-cash expenses and loss on derivative instrument and disposal of assets because these are not related to our primary operations.

We use Adjusted EBITDA in conjunction with traditional GAAP operating performance measures as part of our overall assessment of our performance and we do not place undue reliance on this measure as our only measure of operating performance. Adjusted EBITDA should not be considered a substitute for other measures of financial performance reported in accordance with GAAP.

Reconciliation of Net Income (loss) to Adjusted EBITDA:

 

     Year Ended December 31,  

(in millions, except per share data)

   2007     2008     2009     2010(1)
Revised
    2011  

Net income (loss)

   $ 95.8      $ 53.8      $ 47.4      $ 2.5      $ (28.1

Depreciation and amortization

     46.8        75.7        74.4        118.9        117.1   

Interest (income) expense, net

     (4.1     3.0        (0.1     40.4        21.7   

Loss on derivative instrument

                   1.8                 

Loss from early extinguishment of debt

                   7.7               51.8   

Income tax expense (benefit)

     (57.9     38.1        31.0        4.3        (17.9

Non-cash stock compensation expense

     2.6        4.2        7.2        6.6        14.4   

EnhancedView deferred revenue

                          24.8        86.4   

EnhancedView outstanding invoices not yet paid by NGA

                          8.3        6.7   

Amortization of pre-FOC payment related to NextView

     (3.2     (25.5     (25.5     (25.5     (25.5
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Adjusted EBITDA

   $ 80.0      $ 149.3      $ 143.9      $ 180.3      $ 226.6   
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

 

(1)

The Company revised its 2010 financial information, see Note 3 to the Consolidated Financial Statements for more detail.

 

ITEM 7. MANAGEMENT’S DISCUSSION AND ANALYSIS OF FINANCIAL CONDITION AND RESULTS OF OPERATIONS

Overview

We are a leading global provider of commercial high-resolution earth imagery products and services. Our products and services support a wide variety of uses, including defense, intelligence and homeland security applications, mapping and analysis, environmental monitoring, oil and gas exploration, and infrastructure management. Our principal customers are governments, including U.S. and foreign defense and intelligence, and civil agencies and providers of location-based services (LBS). Additionally we serve a wide variety of companies in other vertical markets, such as energy, telecommunications, utility, forestry, mining, environmental and agricultural industries. The imagery that forms the foundation of our products and services is collected daily via our three high-resolution imaging satellites and managed in our content archive, which we refer to as our

 

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ImageLibrary. We believe our ImageLibrary is the largest, most up-to-date and comprehensive archive of high-resolution earth imagery commercially available, containing more than 2.0 billion square kilometers of imagery, with new imagery added every day. As of December 31, 2011, our collection capacity was approximately 910 million square kilometers of imagery per year or roughly six times the earth’s land surface area and offers intraday revisit around the globe.

Revision of Previously Issued Financial Statements

In connection with the preparation of the Company’s consolidated financial statements for the year ended December 31, 2011, errors were identified primarily relating to the year ended December 31, 2010 and the first three quarters of the year ended December 31, 2011. These errors were primarily related to the Company’s accounting for the Direct Access Program (“DAP”), as described below. The Company has assessed the impact of these errors on each period involved, in accordance with the SEC’s Staff Accounting Bulletin No. 99, and has determined that the impact of the errors was not material, both individually and in the aggregate, to all previously issued financial statements. While the Company has also determined that the cumulative effect of correcting the errors in the fourth quarter of the year ended December 31, 2011 would not be material to the 2011 consolidated financial statements, the Company has elected to revise its previously issued financial statements to facilitate comparisons among periods. As part of its revision, the Company has determined to reverse immaterial out-of-period adjustments that were previously recorded in the Company’s 2011 quarterly periods and to reflect those adjustments as corrections to the periods in which the errors originated.

The following is a description of the nature and the amount of the errors relating to the year ended December 31, 2010 (see Note 16 of the Notes to the Consolidated Financial Statements for the impact on the 2010 and 2011 quarterly financial information):

 

   

In three of the Company’s four current DAP customer contracts, the up-front payments contractually negotiated for the Facility were less than the actual third-party costs to manufacture the Facility. As each of the three Facilities was brought into service, it was the Company’s accounting policy to amortize both the deferred revenue and deferred contracts costs over the estimated customer relationship periods, which periods are consistent with the estimated remaining useful life of the satellite being accessed. However, the Company has concluded that this accounting policy was in error and that it should have been recognizing the deferred contract costs in excess of the deferred revenues (for each individual customer) over the related initial contract period. The impact of this error is an increase in cost of revenue of $1.5 million.

 

   

Certain costs for two DAP customers were previously netted against the related revenue. However, the Company concluded that this was an error as the Company acts as the principal in these arrangements. The cost and revenue should have been recorded on a gross basis, with the effect being an increase in both revenue and cost of revenue of $1.1 million.

 

   

The Company incorrectly capitalized interest related to the construction of its direct access facilities and other discrete projects. The impact of this error is an increase to interest expense of $0.8 million.

 

   

The Company previously recognized maintenance revenue for one DAP customer over a one-year period. However, the Company concluded that this was an error and that the revenue should have been recognized over the customer relationship period. The impact of this error is to reduce revenue by $0.5 million.

 

   

The Company incorrectly calculated certain DAP access minutes. The impact of this error is to reduce revenue by $0.3 million.

 

   

The Company has also corrected other immaterial errors including (i) over- or under-capitalization of certain internal and external costs, (ii) the accounting for stock compensation, including under capitalization of stock compensation for certain assets under construction, (iii) the effects of properly reconciling certain accrued liability accounts, and (iv) the classification of payments received for a sales type lease from operating to investing cash flows.

 

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Products and Services

We offer earth imagery products and services that are comprised of imagery from our three high-resolution satellite constellation as well as aerial and satellite imagery that we acquire from third party suppliers. We process our imagery to varying levels according to our customers’ specifications and deliver our products using the distribution methods that best suit our customers’ needs. Customers can purchase satellite or aerial images that are archived in our ImageLibrary, or by placing custom orders, which require tasking of our satellites, for a specific area of interest, or as a bundle of imagery and data for a region or type of location, such as cities, ports and harbors or airports. For example, our Global Basemap product features comprehensive color imagery of the Earth’s surface that is refreshed on a routine basis and is delivered to customers according to geographic need.

Our ImageLibrary currently houses what we believe to be the most comprehensive, up-to-date, high-resolution archive of commercial earth imagery in the world. It is a collection of substantially all imagery acquired by our QuickBird, WorldView-1 and WorldView-2 satellites, whether tasked for a specific customer or collected on a speculative basis, as well as aerial imagery and other satellite imagery we have purchased to supplement our satellite imagery. We collect and store hundreds of thousands of high-resolution imagery scenes covering over 2.0 billion square kilometers in the ImageLibrary. Approximately 54.5% of our revenue, excluding the NGA SLA, is generated from purchases from our ImageLibrary.

Customers specify how they want the imagery content that they are purchasing from us to be produced. We deliver our satellite imagery content at three processing levels: (i) basic imagery with the least amount of processing; (ii) standard imagery with radiometric and geometric correction; and (iii) ortho-rectified imagery with radiometric, geometric, and topographic correction. Radiometric correction enables images to appear uniformly illuminated with the right level of brightness. Geometric correction allows a user to identify the latitudinal, longitudinal and altitudinal location of any point in an image. Topographic correction accounts for terrain and projects images onto the earth as they would be seen by the human eye. All of our aerial imagery is delivered as ortho-rectified imagery.

We also use enhanced processing to produce mosaic and stereo imagery products. The mosaic process takes multiple imagery scenes, collected at different times and dates, and merges them into a single seamless imagery product. We use specialized collection and enhanced processing to produce stereo imagery products. Stereo imagery products consist of two images collected from two different viewpoints along the satellite orbit track that are produced as basic products, but can be viewed in stereo (3D) using specialized software. Stereo imagery products are used for the creation of digital elevation maps, for the more accurate creation of 3D maps and flight simulations.

We offer a range of on- and off-line distribution options designed to enable customers to easily access and integrate our imagery into their business operations and applications. Delivery options include desktop software applications, web services that provide for direct on-line access to our ImageLibrary, File Transfer Protocol (FTP), and physical media such as CD, DVD, and hard drive.

We offer an additional distribution option through our Direct Access Program (DAP) that allows certain customers, approved by the U.S. government, to task and download data directly from our WorldView-1 and WorldView-2 satellites within their regional area of interest. DAP is designed to meet the enhanced information and operational security needs of a select and limited number of defense and intelligence customers and certain commercial customers. To date, we have signed five customer contracts for our DAP, four of whom have been operational since the second half of 2010. The fifth customer is currently expected to come online in the first half of 2012.

We sell our products and services through a combination of direct and indirect channels, a global network of resellers, strategic partners, direct enterprise sales and web services. We generated 38.3% of our revenue through direct sales and 61.7% of our revenue from our reseller and partner network.

 

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Significant Customer

In September 2003, we entered into the NextView agreement with the National Geospatial-Intelligence Agency (NGA) under which we agreed to provide a minimum of $531.0 million of imagery products and services from our WorldView-1 satellite. Of this amount, $266.0 million was received between September 2003 and November 2007, the date WorldView-1 became operational, and was used to offset the construction costs of the satellite. The remaining $265.0 million commitment was to be received upon the delivery of imagery once WorldView-1 achieved full operational capability (FOC). In January 2008, we amended the NextView agreement from image-based ordering to a service level agreement (SLA) and increased the amount we received under the NextView agreement from $265.0 million to $311.0 million (NextView SLA). On June 25, 2009, the NextView SLA agreement was further amended to extend the term from July 31, 2009 through March 31, 2010 in consideration for payment of an additional $100.0 million, payable at $12.5 million per month during the extended term. On February 9, 2010 the NextView agreement was amended to provide NGA with an option to extend the agreement for three months on the same terms from April 1, 2010 to June 30, 2010 and six additional options each for a one month period with the last option term expiring on December 31, 2010. On March 11, 2010, NGA exercised the option to extend through June 30, 2010. On June 8, 2010, NGA exercised its first monthly option to extend through July 31, 2010, and on July 13, 2010 exercised its second monthly option to extend through August 31, 2010. The NextView SLA expired August 31, 2010.

On August 6, 2010, we entered into the EnhancedView contract with NGA. The SLA portion of the EnhancedView contract, (EnhancedView SLA) has an effective date of September 1, 2010, commencing upon the expiration of the NextView SLA. The EnhancedView contract has a ten year term, inclusive of nine one-year options exercisable by NGA, and is subject to Congressional appropriations and the federal budget process, and the right of NGA to terminate or suspend the contract at any time.

For a discussion of the risk associated with our government contracts, see Risk Factors in Part 1, Item 1A.

The EnhancedView SLA portion of the award is sized at $2.8 billion over the term of the contract assuming NGA exercises all of its options and we perform as specified; $250.0 million annually, or $20.8 million per month, for the first four contract years, commencing September 1, 2010, with an increase to $300.0 million annually, or $25.0 million per month, for the remaining six years of the contract term. The award also provides for up to $750.0 million for value added products, infrastructure enhancements and other services, including the option for NGA to require us to lower the altitude of WorldView-2 to an altitude of 496 km at any time after September 1, 2013. We will be required to meet certain service level requirements related to the operational performance of the satellites comprising the WorldView constellation and related ground systems. To support requirements under this agreement, we have begun the procurement and construction of our next satellite, WorldView-3, as well as certain other infrastructure improvements.

We recognize revenue for the $2.8 billion in services to be provided under the EnhancedView SLA using a proportional performance method based upon the estimated capacity of our constellation made available to NGA compared to the total capacity to be provided over the life of the contract. The contract requires us to increase capacity of the constellation through the installation of additional remote ground terminals, which communicate directly with our satellites, as well as the addition of an entirely new satellite, WorldView-3. Our WorldView-3 satellite is expected to be ready for launch in mid 2014. As capacity is added to our constellation, we recognize revenue in direct proportion to the amount of incremental capacity that is made available to NGA. Commencing in September 2010, we recognized approximately $12.5 million of revenue monthly through August 31, 2011, under the EnhancedView SLA. As of September 1, 2011, we increased the capacity of the constellation made available to NGA and are now recognizing approximately $14.1 million per month under the EnhancedView SLA. For the year ended December 31, 2011, we recognized approximately $157.0 million of revenue and recorded $94.6 million of deferred revenue related to the EnhancedView SLA contract. As of December 31, 2011, there was $119.4 million in total deferred revenue from the inception of the EnhancedView SLA. Given the significant amount of constellation capacity expected to be generated by WorldView-3 satellite and the increasing percentage of capacity that NGA will acquire from us once WorldView-3 satellite becomes operational, we anticipate a material increase in revenue once WorldView-3 satellite reaches FOC.

 

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Under the EnhancedView SLA, and assuming all option years under the agreement are exercised and funded, we will receive a consistent, monthly non-refundable cash payment of approximately $20.8 million from NGA during the first four years of the EnhancedView contract, with an increase to $25.0 million per month in years five through ten. Each month is subject to a holdback, up to 10% of the monthly payment scheduled, depending upon our performance against pre-defined criteria. If we have been certified as having performed all requirements in the agreement each month, no holdback will be applied to that month. If funds are held back, we retain the cash, however, those funds can be applied to future products and services or will fund a pro-rated extension beyond the current contract period. Accordingly, all amounts held back will cause us to defer recognition of a corresponding revenue amount until such additional products or services have been provided. From September 1, 2010 to December 31, 2010, we satisfied all performance criteria under the agreement, and therefore had no holdback applied for the period. During the year ended December 31, 2011, there was $0.2 million of holdback, which occurred during the first quarter of 2011, all of which has been applied to other products and recognized as revenue as of December 31, 2011.

Revenue

Our principal source of revenue is the licensing of our earth imagery products and services to end users and resellers and partners.

We conduct our business through two segments: (i) defense and intelligence; and (ii) commercial. We have organized our business into these two segments because we believe that customers in these two groups are functionally similar in terms of their areas of focus and purchasing habits. Our imagery products and services are comprised of imagery that we process to varying levels according to the customer’s specifications. We deliver our products and services using the distribution method that best suits our customers’ needs. Customers can purchase satellite or aerial images that are archived in our ImageLibrary. Customers can also order imagery content by placing custom orders, which require tasking of our satellites, for a specific area of interest, or as a bundle of imagery and data for a region or type of location, such as cities, ports and harbors or airports.

 

     Year ended December 31,  
   2009     2010
Revised
    2011  
     ($ in millions)  

Revenue

      

Defense and intelligence

   $ 231.0      $ 252.4      $ 261.4   

Commercial

     50.9        70.1        78.1   
  

 

 

   

 

 

   

 

 

 

Total Revenue

   $ 281.9      $ 322.5      $ 339.5   
  

 

 

   

 

 

   

 

 

 

Revenue as a percent of total

      

Defense and intelligence

     81.9     78.3     77.0

Commercial

     18.1        21.7        23.0   
  

 

 

   

 

 

   

 

 

 

Total Revenue

     100.0     100.0     100.0
  

 

 

   

 

 

   

 

 

 

Total U.S. and foreign sales were as follows:

 

     Year ended December 31,  
     2009      2010
Revised
     2011  
     (in millions)  

Revenue

        

U.S.

   $ 232.7       $ 227.8       $ 228.3   

Foreign

     49.2         94.7         111.2   
  

 

 

    

 

 

    

 

 

 

Total Revenue

   $ 281.9       $ 322.5       $ 339.5   
  

 

 

    

 

 

    

 

 

 

 

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Defense and Intelligence Revenue

Our defense and intelligence segment consists of customers who are principally defense and intelligence agencies of U.S. or foreign governments. The U.S. government, through NGA, purchases our imagery products and services on behalf of various entities within the U.S. government, including the military commands and other government agencies. We also sell to other U.S. defense and intelligence customers including defense and intelligence contractors who provide an additional outlet for our imagery by providing value-added services with our imagery to deliver a final end product to a customer.

Our defense and intelligence customers focus on image quality, including resolution, frequency of area revisit and coverage, as well as ensuring availability of a certain amount of our capacity as they integrate our products and services into their operational planning. Our customers in this segment typically operate under contracts with purchase commitments, through which we receive monthly or quarterly payments in exchange for delivering specific orders to the customer. Our revenue from our defense and intelligence customers has historically been largely from tasking orders, with a smaller portion from sales of imagery from our ImageLibrary. We believe this trend will continue. We sell to our defense and intelligence customers both directly and through resellers.

Only one DAP customer had been commissioned in 2009. By the second half of 2010, we commissioned four of our current DAP customers’ ground terminals and began generating revenue from providing satellite access time to these customers. These four DAP customers generated revenue for the entire year of 2011. The fifth DAP customer is currently expected to come online in the first half of 2012.

We earn revenue from sales of the DAP facility hardware and software, as well as service fees to access our satellite constellation. The revenues to access our satellite constellation are recognized over time based on minutes of actual usage. The revenues and costs associated with the sales of a DAP facility are deferred until we commission into operation the ground terminal and can provide contractually specified access to our operational satellites. The revenues and costs are then recognized ratably over the customer relationship period, which is based on the estimated useful life of the satellite being accessed, except when deferred contract costs are in excess of deferred revenues, in which case the excess costs are recognized over the initial contract period. If more than one satellite is used, the satellite with the longest remaining useful life is used as the basis for the amortization.

 

     Year ended December 31,  
   2009     2010
Revised
    2011  
     (in millions)  

Defense and intelligence revenue

      

U.S. and Canada revenue

      

NGA SLA

   $ 150.6      $ 150.3      $ 157.0   

Other revenue and value added services

     38.2        29.7        23.4   

Amortization of pre-FOC payments related to NextView

     25.5        25.5        25.5   
  

 

 

   

 

 

   

 

 

 

Total U.S. and Canada revenue

   $ 214.3      $ 205.5      $ 205.9   
  

 

 

   

 

 

   

 

 

 

International revenue, excluding Canada

   $ 16.1      $ 12.2      $ 8.4   

DAP revenue

     0.6        34.7        47.1   
  

 

 

   

 

 

   

 

 

 

Total international revenue, excluding Canada

   $ 16.7      $ 46.9      $ 55.5   
  

 

 

   

 

 

   

 

 

 

Total defense and intelligence revenue

   $ 231.0      $ 252.4      $ 261.4   
  

 

 

   

 

 

   

 

 

 

Revenue as a Percent of Total

      

U.S. and Canada

     92.8     81.4     78.8

International, excluding Canada

     7.2     18.6     21.2
  

 

 

   

 

 

   

 

 

 
     100.0     100.0     100.0

Reseller and Direct Sales

      

Direct Sales

     96.7     98.2     98.4

Resellers

     3.3     1.8     1.6
  

 

 

   

 

 

   

 

 

 
     100.0     100.0     100.0

 

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Commercial Revenue

Our commercial segment consists of both traditional and location based services customers. Our traditional customers are primarily civil government agencies, and energy, telecommunications, utility and agricultural companies who, like our defense and intelligence customers, use our content for mapping, monitoring, analysis and planning activities. Providers of LBS, include internet portals, connected devices, and digital mapmakers, who use our imagery products and services to expand their products and services. Customers in other industry verticals are represented by financial services, oil and gas, telecommunications, utilities, environmental services and other industry verticals who use our imagery in a wide range of applications.

Our commercial customers are located throughout the world. They purchase our products and services on an as-needed basis, or through multi-year contracts, depending on the solution that best suits their application. We sell to these customers directly and through resellers.

For the twelve months ended December 31, 2011, we generated approximately 21.9% of our commercial revenue from paid tasking and 78.1% from our ImageLibrary.

For the years ended December 31, 2009, 2010 and 2011, our top five commercial customers accounted for 56.1%, 46.3% and 43.5% of our commercial revenue. We believe that we will have additional growth opportunities internationally especially in countries with rapidly developing economies, such as Brazil, China and Russia, and, as a result, we expect that long-term sales growth in our commercial segment will be higher outside of the United States.

 

     Year ended December 31,  
   2009     2010
Revised
    2011  
    

(in millions)

 

Commercial Revenue

      

Americas

   $ 23.6      $ 32.5      $ 32.9   

International

     27.3        37.6        45.2   
  

 

 

   

 

 

   

 

 

 

Total commercial revenue

   $ 50.9      $ 70.1      $ 78.1   
  

 

 

   

 

 

   

 

 

 

Revenue as a Percent of Total

      

Americas revenue

     46.4     46.4     42.1

International revenue

     53.6     53.6     57.9

Reseller and Direct Sales

      

Direct sales

     43.4     42.4     38.3

Resellers

     56.6     57.6     61.7

Expenses

Most of our revenue is generated by the sale of products and services comprised of imagery from our QuickBird, WorldView-1 and WorldView-2 satellites. Given that most of the costs of a satellite are related to the pre-operation capital expenditures required to build and launch a satellite, there is no significant direct relationship between our cost of revenue and changes in our revenue. Our cost of revenue consists primarily of the cost of personnel, as well as the cost of operations directly associated with operating our satellites, retrieving information from the satellites, and processing the data retrieved. Costs of acquiring aerial imagery from third-parties are capitalized and amortized on an accelerated basis as a cost of revenue.

Our selling, general and administrative expenses consist primarily of labor, benefits, travel, rent, insurance, utilities, telecommunications and related overhead costs, third-party consultant payments, sales commissions and marketing expenses. Our total selling, general and administrative expenses have been increasing in recent years, and we expect the increase in costs to continue, as we expand our sales and administrative resources to enable our revenue growth and increase capacity for product sales and distribution.

 

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The increase in selling, general and administrative expenses may be offset in future years by the capitalization of labor costs incurred in the development of new assets, especially during the construction of a new satellite. With the initiation of WorldView-3 satellite and other capital investments related to the EnhancedView program, we anticipate we will be capitalizing increasing amounts of direct labor costs that are associated with the development of these programs.

Depreciation and amortization consist primarily of depreciation of our satellites and other operating assets. On January 4, 2010, when the WorldView-2 satellite reached FOC, we began depreciating this asset at a rate of approximately $10.5 million each quarter.

Our interest charges consist primarily of interest payments on borrowings used to finance satellite construction and are capitalized as a cost of our satellite construction. During 2009, all interest incurred was capitalized to our WorldView-2 satellite and other assets under construction. With the successful commissioning of WorldView-2, the total capitalized interest amount was significantly smaller in 2010, increasing our interest expense. During 2011, with the increase in capital projects, including WorldView-3 our capitalized interest expense has increased, decreasing our interest expense.

Based on our capitalization policies, we expect our future interest expense to decrease due to capitalization of these costs to the construction of our WorldView-3 satellite and other infrastructure, until the anticipated commissioning of WorldView-3 in 2014. The costs of our satellites include capitalized interest costs incurred during the construction and development period of the satellite. In addition, capitalized costs of our satellites and related ground systems include internal direct labor costs incurred in their construction.

Results of Operations

For the Year Ended December 31, 2011 Compared to Year Ended December 31, 2010

The following tables summarize our historical results of operations for the year ended December 31, 2011 compared to the year ended December 31, 2010, and our expenses as a percentage of revenue for the periods indicated:

 

     Year Ended
December 31,
    Change  
     2010
Revised
    2011     $     Percent  
     ($ in millions)  

Historical results of operations:

        

Defense and intelligence revenue

   $ 252.4      $ 261.4      $ 9.0        3.6

Commercial revenue

     70.1        78.1        8.0        11.4   
  

 

 

   

 

 

   

 

 

   

 

 

 

Total revenue

     322.5        339.5        17.0        5.3   

Cost of revenue excluding depreciation and amortization

     44.2        64.9        20.7        46.8   

Selling, general and administrative

     112.2        130.2        18.0        16.1   

Depreciation and amortization

     118.9        117.1        (1.8     (1.5
  

 

 

   

 

 

   

 

 

   

 

 

 

Income from operations

     47.2        27.3        (19.9     (42.2

Loss from early extinguishment of debt

            (51.8     (51.8       

Other income (expense), net

            0.2        0.2          

Interest income (expense), net

     (40.4     (21.7     (18.7     (46.3
  

 

 

   

 

 

   

 

 

   

 

 

 

Income (loss) before income taxes

     6.8        (46.0     (52.8     (776.5

Income tax (expense) benefit

     (4.3     17.9        22.2        516.2   
  

 

 

   

 

 

   

 

 

   

 

 

 

Net income (loss)

   $ 2.5      $ (28.1   $ (30.6     (1,224.0 )% 
  

 

 

   

 

 

   

 

 

   

 

 

 

 

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Table of Contents

 

     Year Ended
December 31,
 
   2010
Revised
    2011  

Expenses as a percentage of revenue:

    

Total revenue

     100.0     100.0

Cost of revenue excluding depreciation and amortization

     13.7        19.1   

Selling, general and administrative

     34.8        38.4   

Depreciation and amortization

     36.9        34.5   
  

 

 

   

 

 

 

Income from operations

     14.6        8.0   

Loss from early extinguishment of debt

            (15.3

Other income (expense), net

            0.1   

Interest income (expense), net

     (12.5     (6.4
  

 

 

   

 

 

 

Income (loss) before income taxes

     2.1        (13.6

Income tax (expense) benefit

     (1.3     5.3   
  

 

 

   

 

 

 

Net income (loss)

     0.8     (8.3 )% 
  

 

 

   

 

 

 

Revenue increased $17.0 million or 5.3% from $322.5 million for the year ended December 31, 2010 to $339.5 million for the year ended December 31, 2011.

There was an increase of $9.0 million or 3.6%, in defense and intelligence revenue during the year ended December 31, 2011, to $261.4 million from $252.4 million for the year ended December 31, 2010. This increase was the result of a $12.4 million increase in direct access program revenue and $6.7 million of additional revenue recognized under the NGA SLA due to increased capacity made available to NGA per the EnhancedView contract, offset by a $6.3 million decrease in value added services from the U.S. Government due to a decrease in funding available, as well as a $3.8 million decrease in International revenue. The increase of $8.0 million in commercial revenue to $78.1 million for the year ended December 31, 2011 from $70.1 million for the year ended December 31, 2010, was due to a $0.4 million increase in revenue from location-based services customers in the Americas and a $7.6 million increase in international sales, primarily in Europe.

Cost of revenue increased $20.7 million or 46.8%, during the year ended December 31, 2011 to $64.9 million from $44.2 million for the year ended December 31, 2010. This increase is attributed to (i) a $10.1 million increase in costs related to ground system operations due to the addition of four remote ground terminals brought into service during the year per the EnhancedView contract, (ii) a $5.6 million increase in labor related costs due to headcount growth and (iii) a $1.1 million increase in deferred contract costs amortization as all four direct access facilities were operational for the full year ended December 31, 2011.

Selling, general and administrative costs increased $18.0 million or 16.1%, for the year ended December 31, 2011, to $130.2 million from $112.2 million for the year ended December 31, 2010. This increase was attributable to (i) a $11.1 million increase in labor related costs, of which $5.1 million was a one-time, non-cash stock compensation expense related to the departure of the prior CEO, (ii) a $4.6 million increase in bad debt expense, primarily for two delinquent customers in Asia, (iii) a $4.3 million increase in consulting services, and (iv) a $1.7 million increase in general software and maintenance fees. These increases were offset by a $4.7 million decrease in costs to insure our satellite constellation, primarily due to reduced insurance premiums for WorldView-2 as the satellite was in the second year of operation and benefitted from lower on-orbit insurance.

Depreciation and amortization decreased by $1.8 million for the year ended December 31, 2011, to $117.1 million from $118.9 million for the year ended December 31, 2010. This decrease is primarily related to extending the life of the QuickBird satellite during the second quarter of 2011. Future changes in depreciation and amortization could be affected by commissioning of a new satellite, change in useful life of an existing satellite, or introduction of significant new capital assets.

 

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Interest expense, net of capitalized interest, decreased by $18.7 million for the year ended December 31, 2011 to $21.7 million from $40.4 million during the year ended December 31, 2010. This decrease is attributed to approximately 45% of our interest being capitalized to capital projects during the year ended December 31, 2011 as compared to 6% in 2010. This increase is attributable to the construction in progress of our WorldView-3 satellite, which began during the third quarter of 2010 and is currently expected to continue until anticipated launch and commission of WorldView-3 in 2014. We anticipate that an increasing percentage of our interest will be capitalized until the WorldView-3 satellite is launched.

The benefit from income taxes in 2011, is primarily due to loss on extinguishment of debt of $51.8 million. For the year ended December 31, 2011, we had an effective overall tax rate of 38.9%. The effective tax rate differed from the statutory federal rate of 35.0% primarily due to state taxes and the effects of non-deductible stock based compensation.

For the Year Ended December 31, 2010 Compared to Year Ended December 31, 2009

The following tables summarize our historical results of operations for the year ended December 31, 2010 compared to the year ended December 31, 2009 and our expenses as a percentage of revenue for the periods indicated:

 

     Year Ended
December 31,
    Change  
     2009     2010
Revised
    $     Percent  
     ($ in millions)  

Historical results of operations:

        

Defense and intelligence revenue

   $ 231.0      $ 252.4      $ 21.4        9.3

Commercial revenue

     50.9        70.1        19.2        37.7   
  

 

 

   

 

 

   

 

 

   

 

 

 

Total revenue

     281.9        322.5        40.6        14.4   

Cost of revenue excluding depreciation and amortization

     31.1        44.2        13.1        42.1   

Selling, general and administrative

     88.6        112.2        23.6        26.6   

Depreciation and amortization

     74.4        118.9        44.5        59.8   
  

 

 

   

 

 

   

 

 

   

 

 

 

Income from operations

     87.8        47.2        (40.6     (46.2

Loss from early extinguishment of debt

     (7.7            7.7        100.0   

Loss on derivative instruments

     (1.8            1.8        100.0   

Interest income (expense), net

     0.1        (40.4     (40.5     *   
  

 

 

   

 

 

   

 

 

   

 

 

 

Income before income taxes

     78.4        6.8        (71.6     (91.3

Income tax expense

     (31.0     (4.3     26.7        86.1   
  

 

 

   

 

 

   

 

 

   

 

 

 

Net income

   $ 47.4      $ 2.5      $ (44.9     (94.7 )% 
  

 

 

   

 

 

   

 

 

   

 

 

 

 

*

not meaningful

 

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Table of Contents

 

     Year Ended
December 31,
 
   2009     2010  
           Revised  

Expenses as a percentage of revenue:

    

Total revenue

     100.0     100.0

Cost of revenue excluding depreciation and amortization

     11.0        13.7   

Selling, general and administrative

     31.4        34.8   

Depreciation and amortization

     26.4        36.9   
  

 

 

   

 

 

 

Income from operations

     31.2        14.6   

Loss from early extinguishment of debt

     (2.7       

Loss on derivative instruments

     (0.6       

Interest income (expense), net

            (12.5
  

 

 

   

 

 

 

Income before income taxes

     27.9        2.1   

Income tax expense

     (11.0     (1.3
  

 

 

   

 

 

 

Net income

     16.9     0.8
  

 

 

   

 

 

 

Total revenue increased $40.6 million, or 14.4%, to $322.5 million in 2010 as compared to $281.9 million in 2009. The $21.4 million, or 9.3%, increase in defense and intelligence revenue was due primarily to DAP customers, who received access time to WorldView-1 and/or WorldView-2 through direct access facilities in the second half of 2010 that were not operational in 2009. The $19.2 million, or 37.7%, increase in commercial revenue was driven by growth from consumer customers in Europe and the Americas and reseller business worldwide.

The $13.1 million increase in cost of revenue is primarily attributable to $8.0 million of amortization of deferred contract costs arising from the construction, implementation and maintenance of the DAP facilities and a $3.9 million increase in subcontracting costs. The cost of revenue increase also includes a $2.7 million increase in labor related costs, primarily driven by headcount growth as well as the cost of employee labor which had previously been capitalized as part of the WorldView-2 development, but which has now been reallocated to other operating functions within the Company. These increases were offset by a $1.5 million decrease in amortization of the purchased aerial imagery library.

The $23.6 million increase in selling, general and administrative costs is attributable to a $10.5 million increase in labor-related costs, primarily driven by headcount growth as well as expensing of employee labor cost that previously had been capitalized as a part of WorldView-2 development. Other increases in selling, general and administrative costs include an increase of $6.6 million from costs related to insuring WorldView-2, an increase of $5.9 million in consulting costs, a $1.9 million increase in bonus expense due to increased headcount and a $1.7 million increase in legal and accounting services. These increases were offset by a $1.0 million decrease in stock compensation expense, a $1.0 million decrease in bad debt expense and a $1.1 million decrease in third party commission expense.

Depreciation and amortization increased by $44.5 million, or 59.8%, as compared to 2009, primarily due to the commissioning of WorldView-2 on January 4, 2010. The WorldView-2 satellite is being depreciated over 11 years and the incremental depreciation is approximately $10.5 million per quarter.

Interest expense, net was $40.4 million, an increase from 2009 due to the commissioning of the WorldView-2 satellite on January 4, 2010, which resulted in the expensing of substantially all of the interest on our debt during 2010. Approximately six percent of our interest was capitalized on capital projects during 2010. During the third quarter of 2010, we started the construction of the WorldView-3 satellite, thus we expect our capital expenditures to increase in future reporting periods, resulting in more of our interest being capitalized.

The decrease in income tax is primarily due to a decrease in pre-tax income. For the year ended December 31, 2010, we had an effective overall tax rate of 63.2%. The effective tax rate differed from the

 

36


Table of Contents

statutory federal rate of 35.0% primarily due to state taxes and the effects of non-deductible stock-based compensation.

Balance Sheet Measures

Total assets increased $183.5 million, or 14.5%, from $1,268.1 million at December 31, 2010 to $1,451.6 million at December 31, 2011. Total assets increased primarily as a result of an increase in property and equipment of $141.2 million, from $878.6 million at December 31, 2010 to $1,019.8 million at December 31, 2011. The increase in property and equipment results from an increase in WorldView-3 satellite construction and other infrastructure projects. The increase in aerial image library costs from $1.9 million at December 31, 2010 to $13.0 million at December 31, 2011, is due to receipt of imagery acquired from a third party provider. Cash and cash equivalents increased $19.2 million due to additional debt borrowings offset by increases in operating costs and increased capital expenditures related to World-View 3.

Total liabilities increased $195.0 million, from $769.2 million at December 31, 2010 to $964.2 million at December 31, 2011. This increase was due to a net $72.6 million increase in long term deferred revenue from $246.7 million at December 31, 2010 to $319.3 at December 31, 2011 primarily due to payments received from NGA under the EnhancedView SLA, offset by the recognition of the pre-FOC payments received under the NextView agreement. The Company entered into a new debt facility on October 12, 2011, increasing our long term debt $135.5 million, from $346.1 million at December 31, 2010 to $481.6 million at December 31, 2011. Total accounts payable, other accrued liabilities and long-term accrued liabilities increased by $7.7 million from $50.9 million at December 31, 2010 to $58.6 million at December 31, 2011. The increase is primarily related to the timing of accruals for milestone payments on capital projects. Accrued interest decreased $6.0 million from $6.2 million at December 31, 2010 to $0.2 million at December 31, 2011, due to the timing of interest payments under the new credit facility entered into in October of 2011.

Liquidity and Capital Resources

We believe that the combination of funds currently available to us and funds expected to be generated from operations will be adequate to finance our operations and development activities for the next twelve months. Our NextView agreement with NGA was replaced by the EnhancedView agreement which was signed during August 2010. We cannot assure you that the U.S. government will continue to purchase earth imagery or other services from us at similar levels or similar terms. All of our contracts with the U.S. government agencies are subject to risks of termination or reduction in scope due to changes in U.S. government policies and priorities, or reduced Congressional funding level commitments. Pursuant to the contract terms, U.S. government agencies can terminate, modify or suspend our contracts at any time with or without cause. The U.S. government accounted for approximately 60.1% of our consolidated revenue for the year ended December 31, 2011. If the U.S. government were not to renew or extend our contract at similar levels or similar terms, we believe we would be able to maintain operations at a reduced level with existing cash and cash equivalents for the next twelve months.

In summary, our cash flows were:

 

     2009     2010
Revised
    2011  
     (in millions)  

Net cash provided by operating activities

   $ 143.3      $ 153.3      $ 142.8   

Net cash used in investing activities

     (191.1     (80.9     (259.5

Net cash provided by financing activities

   $ 84.0      $ 9.9      $ 135.9   

Cash provided by operating activities decreased from $153.3 million in the year ended December 31, 2010 to $142.8 million in the year ended December 31, 2011. The $10.5 million decrease in operating activities is primarily due to a decrease in net income due to the loss on extinguishment of debt offset by the increase in EnhancedView deferred revenue as a result of payments received from NGA during the year, and increased non-cash stock compensation expense primarily due to the departure of the prior CEO.

 

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Cash used in investing activities increased from $80.9 million in the year ended December 31, 2010 to $259.5 million in the year ended December 31, 2011. The $178.6 million increase was primarily due to an increase in capital expenditures related to the construction of the WorldView-3 satellite and related infrastructure.

As disclosed in the contractual obligations table, we have $406.9 million that is contractually due to third party vendors. These contractual obligations are primarily related to the procurement and construction of our WorldView-3 satellite, including launch vehicle and related ground systems.

Cash provided by financing activities increased from $9.9 million in the year ended December 31, 2010 to $135.9 million in the year ended December 31, 2011. The $126.0 increase was primarily due to the new credit facility entered into on October 12, 2011 offset by the early extinguishment and repayment of the senior secured notes.

Senior Secured Credit Facility

On October 12, 2011, we entered into a $500 million, seven-year senior secured term loan facility and a $100 million, five-year senior secured revolving credit facility, the terms of which are set forth in a Credit and Guaranty Agreement dated as of October 12, 2011 among the Company, the guarantors party thereto, the lenders named therein and J.P. Morgan Chase Bank, N.A., as administrative agent and as collateral agent (the “Credit Agreement”). We have borrowed the full amount of the term loan facility to fund our cash tender offer (“Tender Offer”) to purchase all of our senior secured notes and add liquidity for general corporate purposes. We received net cash proceeds from the term loan facility of approximately $66.0 million following the payment of approximately $410.9 million for the tender of the senior secured notes, $11.8 million in underwriter and other related fees and expenses incurred in connection with the Credit Agreement, and net of the term loan issuance discount of $12.5 million. The Company paid $1.2 million in fees related to the tender offer. We recorded a loss on extinguishment of debt of $51.8 million, during the fourth quarter of 2011. As a result of the Tender Offer, 100% of all Senior Secured Notes were tendered and retired by the Company on October 12, 2011. We will use the remaining cash proceeds for general corporate purposes, which may include acquisitions and share repurchases. As of the date of this filing, the revolving credit facility remains undrawn.

The obligations of the Company under the credit facility are guaranteed by certain of the Company’s domestic subsidiaries and are secured by substantially all of the assets of the Company and the guarantors, subject to certain exceptions. The Credit Agreement contains affirmative and negative covenants that we believe are usual and customary for a senior secured credit agreement. The negative covenants include, among other things, limitations on asset sales, mergers and acquisitions, indebtedness, liens, dividends, investments and transactions with our affiliates. The Credit Agreement also requires us to comply with a maximum leverage ratio and minimum interest coverage ratio.

Borrowings under the Credit Agreement will bear interest, at our option, at a rate equal to either an adjusted LIBOR rate or a base rate, in each case plus the applicable margin. The applicable margin for borrowings under the term loan facility is 4.50% for adjusted LIBOR loans or 3.50% for base rate loans. The applicable margin for borrowings under the revolving credit facility may change depending on our leverage ratio, up to a maximum of 4.50%. The term loan facility currently bears interest based upon the LIBOR-based rate. We will also pay a commitment fee of between 37.5 to 50.0 basis points, payable quarterly, on the average daily unused amount of the revolving credit facility based on our leverage ratio.

Senior Secured Notes

On April 28, 2009, we issued $355.0 million principal amount of our senior secured notes. Net proceeds of $341.8 million were used to repay our senior credit facility and senior subordinated notes in full and pay fees and expenses associated with the transaction. The senior secured notes were scheduled to mature on May 1, 2014. The senior secured notes were guaranteed by certain of the Company’s domestic subsidiaries and secured by nearly all of our assets, including the shares of capital stock of our subsidiaries, and the QuickBird, WorldView-1

 

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and WorldView-2 satellites in operation. The senior secured notes bore interest at the rate of 10.5% per annum. Interest was payable semi-annually on May 1 and November 1 of each year.

Off-Balance Sheet Arrangements, Contractual Obligations, Guaranty and Indemnification Obligations

Off-Balance Sheet Arrangements

We had no off-balance sheet arrangements as of December 31, 2011.

Contractual Obligations

We have various contractual obligations impacting our liquidity. The following represents our contractual obligations as of December 31, 2011:

 

     Payments Due by Period  
       Total      Less
Than

1 year
     1-3
Years
     3-5
Years
     More
Than

5 Years
 
     (in millions)  

Operating leases

   $ 14.0       $ 3.6       $ 5.9       $ 1.7       $ 2.8   

Senior secured facility excluding interest payments

     500.0         5.0         10.0         10.0         475.0   

Interest payments for senior secured facility

     191.8         29.2         57.3         56.3         49.0   

Contractual obligations

     406.9         153.9         205.7         31.1         16.2   
  

 

 

    

 

 

    

 

 

    

 

 

    

 

 

 

Total

   $ 1,112.7       $ 191.7       $ 278.9       $ 99.1       $ 543.0   
  

 

 

    

 

 

    

 

 

    

 

 

    

 

 

 

Our senior secured facility requires quarterly principle payments in the amount $1.25 million starting March 31, 2012 through September 30, 2018. The remaining balance of $466.3 million is due October 12, 2018. Interest expense is due at least monthly or as agreed upon with the lender. Contractual obligations are remaining amounts due on long term contracts primarily relating to the procurement and construction of our WorldView-3 satellite, including the launch vehicle, and operational commitments related to our ground systems. Our operating leases are primarily for office space in the United States. We generally believe leasing office space is more cost-effective than purchasing real estate, for our existing operating locations. The Company has $5.4 million of uncertain tax positions and does not anticipate a material change within the next 12 months.

Guaranty and Indemnification Obligations

We enter into agreements in the ordinary course of business with resellers and others. Most of these agreements require us to indemnify the other party against third-party claims alleging that one of our products infringes or misappropriates a patent, copyright, trademark, trade secret or other intellectual property right. Certain of these agreements require us to indemnify the other party against claims relating to property damage, personal injury or acts or omissions by us, our employees, agents or representatives. In addition, from time to time we have made guarantees regarding the performance of our systems to our customers.

 

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Non-GAAP Disclosures

Reconciliation of Net Income to Adjusted EBITDA

 

     For the Year Ended December 31,  
       2007     2008     2009     2010(1)
Revised
    2011  
     (in millions)  

Net income (loss)

   $ 95.8      $ 53.8      $ 47.4      $ 2.5      $ (28.1

Depreciation and amortization

     46.8        75.7        74.4        118.9        117.1   

Interest (income) expense, net

     (4.1     3.0        (0.1     40.4        21.7   

Loss on derivative instrument

                   1.8                 

Loss from early extinguishment of debt

                   7.7               51.8   

Income tax expense (benefit)

     (57.9     38.1        31.0        4.3        (17.9

Non-cash stock compensation expense

     2.6        4.2        7.2        6.6        14.4   

EnhancedView deferred revenue

                          24.8        86.4   

EnhancedView outstanding invoices not yet paid by NGA

                          8.3        6.7   

Amortization of pre-FOC payment related to NextView

     (3.2     (25.5     (25.5     (25.5     (25.5
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Adjusted EBITDA

   $ 80.0      $ 149.3      $ 143.9      $ 180.3      $ 226.6   
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

 

     For the Quarters Ended(1)  
     2010     2011  
     Mar 31
Revised
    Jun 30
Revised
    Sep 30
Revised
    Dec 31
Revised
    Mar 31
Revised
    Jun 30
Revised
    Sep 30
Revised
    Dec 31  
     (in millions)  

Net income (loss)

   $ 1.5      $ 0.3      $ 0.1      $ 0.6      $ (1.3   $ (0.9   $ 1.1      $ (27.0

Depreciation and amortization

     29.2        31.1        29.1        29.5        29.2        29.2        29.1        29.6   

Interest (income) expense, net

     10.0        10.7        10.5        9.2        7.9        5.7        4.1        4.0   

Loss from early extinguishment of debt

                                                      51.8   

Income tax expense (benefit)

     1.6        0.4        0.8        1.5        (1.5     (1.1     (1.7     (13.6

Non-cash stock compensation expense

     1.4        1.5        1.5        2.2        2.1        7.4        2.3        2.6   

EnhancedView deferred revenue

                          16.5        16.5        16.5        16.5        13.6   

EnhancedView outstanding invoices not yet paid by NGA

                   8.3        8.3        8.3        8.3        6.7        6.7   

Amortization of pre-FOC payment related to NextView

     (6.4     (6.4     (6.4     (6.3     (6.4     (6.4     (6.4     (6.3
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Adjusted EBITDA

   $ 37.3      $ 37.6      $ 43.9      $ 61.5      $ 54.8      $ 58.7      $ 51.7      $ 61.4   
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

 

(1)

The Company revised its 2010 financial information as well as the first three quarters of 2011, see Note 3 to the Consolidated Financial Statements for more detail.

Non-GAAP Financial Measures

Adjusted EBITDA is not a recognized term under generally accepted accounting principles, or GAAP, in the United States and may not be defined similarly by other companies. Adjusted EBITDA should not be considered an alternative to net income, as an indication of financial performance, or as an alternative to cash flow from operations as a measure of liquidity. There are limitations to using non-GAAP financial measures, including the

 

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difficulty associated with comparing companies in different industries that use similar performance measures whose calculations may differ from ours.

Adjusted EBITDA is a key measure used in internal operating reports by management and the board of directors to evaluate the performance of our operations and is also used by analysts, investment banks and lenders for the same purpose. Adjusted EBITDA has also been a key driver of the company-wide bonus incentive plan. Adjusted EBITDA is a measure of our current period operating performance, excluding charges for capital, depreciation related to prior period capital expenditures and items which are generally non-core in nature, and including EnhancedView deferred revenue and EnhancedView outstanding invoices not yet paid by NGA and excluding the amortization of pre-FOC payments related to our NextView contract. EnhancedView outstanding invoices not yet paid by NGA represent an irrevocable right to be paid in cash by NGA.

We believe that the elimination of material non-cash, non-operating items enables a more consistent measurement of period to period performance of our operations. In addition, we believe that elimination of these items in combination with the addition of the nonrefundable EnhancedView deferred revenue and EnhancedView outstanding invoices not yet paid by NGA as well as the elimination of amortization of pre-FOC payments related to NextView, facilitate comparison of our operating performance to companies in our industry. We believe this Adjusted EBITDA measure is particularly important in a capital intensive industry such as ours, in which our current period depreciation is not a good indication of our current or future period capital expenditures. The cost to construct and launch a satellite and build the related ground infrastructure may vary greatly from one satellite to another, depending on the satellite’s size, type and capabilities. For example, our QuickBird satellite, which we are currently depreciating, cost significantly less than our WorldView-1 and WorldView-2 satellites. Current depreciation expense is not indicative of the revenue generating potential of the satellite.

Adjusted EBITDA excludes interest income, interest expense, income taxes and loss on early extinguishment of debt because these items are associated with our capitalization and tax structures. Adjusted EBITDA also excludes depreciation and amortization expense because these non-cash expenses reflect the impact of prior capital expenditure decisions which are not indicative of future capital expenditure requirements. Adjusted EBITDA excludes non-cash stock compensation expense, because these items are non-cash expenses and loss on derivative instrument and disposal of assets because these are not related to our primary operations.

We use Adjusted EBITDA in conjunction with traditional GAAP operating performance measures as part of our overall assessment of our performance and we do not place undue reliance on this measure as our only measure of operating performance. Adjusted EBITDA should not be considered a substitute for other measures of financial performance reported in accordance with GAAP.

Critical Accounting Policies

Revenue Recognition

Our principal source of revenue is the licensing of earth imagery products and services for end users and resellers. Revenue is recognized when the following criteria have been met: persuasive evidence of an arrangement exists, delivery has occurred or services have been rendered, the fee is fixed or determinable and the collection of funds is reasonably assured. Our revenue is generated from: (i) sales of or royalties arising from licenses of imagery; and (ii) subscription services and other service arrangements.

Sales of Licenses.     Revenue from sales of imagery licenses is recognized when the images are physically delivered to the customer or, in the case of electronic delivery, when the customer is able to directly download the image from our system. In certain customer arrangements, we must satisfy certain acceptance provisions. For these arrangements, revenue is recognized upon acceptance by these customers. Revenue is recognized net of contractually agreed discounts.

Royalties.     Revenue from royalties is based on agreements or licenses with third parties that allow the third party to incorporate our product into their value added product for commercial distribution. Revenue from these

 

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royalty arrangements is recorded in the period earned or on a systematic basis over the term of the license agreement. For those royalties that are due to third parties based on our revenue sharing arrangements, we report royalty revenue on a net basis.

Subscriptions.     We sell online subscriptions to our products. These arrangements allow customers access to our products via the internet for a set period of time and a fixed fee. The subscription revenue is recorded as deferred revenue and recognized ratably over the subscription period. In addition, we have other arrangements in which customers pay for their subscription to one of our web-based products by paying for a predetermined amount of access (for example, each time users click on an image of their home). In the case of prepayment, each time a product is accessed, a portion of the customer’s prepayment is earned. These prepayments are recorded as deferred revenue when received and the revenue is recognized based on the number of times the product is accessed. Revenue is recognized net of contractually agreed discounts.

Service Level Agreements (SLA).     We recognize service level agreement revenue net of any allowances resulting from failure to meet certain stated monthly performance metrics. Net revenue is either recognized ratably over time for a defined and fixed level of service, or based on proportional performance when the level of service changes based on certain criteria stated in the agreement.

Multiple Deliverable Arrangements .    We enter into revenue arrangements that may consist of multiple deliverables of our product and service offerings based on the needs of our customers. These arrangements may include products delivered at the onset of the agreement, as well as products or services that are delivered over multiple reporting periods.

In October 2009, the FASB issued ASU 2009-13, “Multiple-Deliverable Revenue Arrangements” and ASU 2009-14, “Certain Revenue Arrangements That Include Software Elements.” We concurrently adopted ASU 2009-13 and ASU 2009-14 prospectively on January 1, 2011. ASU 2009-13 changes the requirements for establishing separate units of accounting in a multiple deliverable arrangement and requires the allocation of arrangement consideration to each deliverable based on the relative selling price. The selling price for each deliverable is based on vendor-specific objective evidence (VSOE) if available, third-party evidence (TPE) if VSOE is not available, or best estimate selling price (BESP) if neither VSOE nor TPE is available. ASU 2009-14 excludes software that is contained in a tangible product from the scope of software revenue guidance if the software is essential to the tangible product’s functionality.

We have generally been unable to establish VSOE for any of our products due to our infrequently selling each deliverable separately or only having a limited sales history, such as in the case of new or emerging products. As of December 31, 2011, we have been unable to establish TPE for any of our offerings due to the unique nature of our products and services and the limited number of competitors. As we are unable to establish price on the basis of VSOE or TPE, we use BESP to determine the allocation of arrangement consideration. The objective of BESP is to determine the price at which we would transact a sale if the product or service were sold on a standalone basis. We determine BESP for a product or service by considering multiple factors, including but not limited to market conditions, competitive landscape, internal costs, gross margin objectives, product technology lifecycles, pricing practices and our go-to-market strategy.

The adoption of ASU 2009-13 and ASU 2009-14 was not material to our financial results for the year ended December 31, 2011. We are not able to reasonably estimate the effect of adopting these standards on future periods as the impact will vary based on the nature and volume of new or materially modified multiple element arrangements transacted in any given period.

While multiple deliverable arrangements occur throughout our business, the EnhancedView contract with NGA and the DAP make up the majority of our multiple deliverable arrangement activity. EnhancedView and four of our DAP agreements were entered into prior to the January 1, 2011 adoption of ASU 2009-13 and ASU 2009-14 and none have been subsequently materially modified. As we adopted the new guidance on a prospective basis, the agreements will continue to be accounted for under the pre-adoption guidance unless they are materially modified. The following is a description of the accounting for these arrangements.

 

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EnhancedView.     The EnhancedView contract contains multiple deliverables, including an SLA, infrastructure enhancements, and other services. We determined that these deliverables do not qualify as separate units of accounting due to a lack of standalone value for the delivered elements and a lack of objective reliable evidence of fair value for any of the undelivered elements in the arrangement. We recognize revenue on a single unit of accounting using a proportional performance method based on the estimated capacity of our constellation made available to NGA compared to the total estimated capacity to be provided over the life of the contract.

Direct Access Program.     Revenue under the direct access program includes construction of the direct access facility and an arrangement to allow the customer access to the satellite to task and download imagery. In these arrangements the facility is delivered upon completion and customer acceptance, and the maintenance and access services occur over several subsequent reporting periods. These arrangements have generally been treated as a single unit of accounting due to a lack of standalone value for the delivered elements and a lack of objective reliable evidence of fair value for any of the undelivered items. Accordingly, all funds received are initially recorded as deferred revenue. As the direct access facilities are brought into service, the deferred revenue is amortized ratably over the estimated customer relationship period, which is consistent with the estimated remaining useful life of the satellite being used.

Asset Valuation and Estimated Useful Lives of Satellites

Asset valuation includes assessing the recorded value of certain assets, including accounts receivable, goodwill, capitalized contract and related satellite costs and other intangible assets. We use a variety of factors to assess valuation, depending upon the asset. Accounts receivable are evaluated based upon the creditworthiness of our customers, historical experience, the age of the receivable and current market and economic conditions. Should current market and economic conditions deteriorate or if our other assumptions are not met, our actual bad debt expense could exceed our estimate.

We capitalize interest, an allocated portion of launch insurance premiums, contract costs and internal direct labor costs incurred. Once a satellite is operational, we depreciate the asset over the expected operational life. Changes in the estimates of the operational life of the asset are reflected in subsequent periods as adjustments to future depreciation expenses.

Following each launch, and at least annually thereafter, we review the expected operational life of our satellites. We determine a satellite’s expected operational life using a complex calculation involving the probabilities of failure of the satellite’s components from design or manufacturing defects, environmental stresses or other causes. The expected operational lives of our satellites are affected by a number of factors, including the quality of construction, the supply of fuel, the expected gradual environmental degradation of solar panels and other components, levels of solar radiation, the durability of various satellite components and the orbits in which the satellites are placed.

Income Taxes

The current provision for income taxes represents actual or estimated amounts payable or refundable on tax returns filed each year. Deferred tax assets and liabilities are recognized for the estimated future tax effects attributable to the temporary differences between the financial statement carrying amounts of existing assets and liabilities and their respective tax bases, as well as operating loss and tax credit carryforwards. The effect on deferred tax assets and liabilities of a change in enacted tax laws is recognized as an adjustment to the tax provision or benefit in the period of enactment. The overall change in deferred tax assets and liabilities during the period is equal to the deferred tax expense or benefit for the period. The carrying value of deferred tax assets may be reduced by a valuation allowance if, based upon the judgmental assessment of available evidence, it is deemed more likely than not that some or all of the deferred tax assets will not be realizable.

As of December 31, 2011, there are no income tax positions for which we currently believe that the unrecognized tax benefits will significantly increase or decrease during the next twelve months. Tax years still open for examination by federal and major state agencies as of December 31, 2011 are 1996 through 2011.

 

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Federal and state agencies may disallow research tax carryforwards, net operating loss carryforwards and other carryforwards previously claimed.

As of December 31, 2011, we had federal and state net operating loss carryforwards of $264.5 million and $245.9 million, respectively, available to offset future federal and state taxable income. If not used, the net operating loss carryforwards will expire at various times during the period from 2019 to 2031. The Internal Revenue Code places certain limitations on the annual amount of net operating loss carryforwards, which can be utilized, if certain changes in the Company’s ownership occur. Included in the Company’s federal net operating loss carryforward is $16.4 million that is subject to a $2.0 million annual IRC 382 limitation, which is expected to be fully utilized in future periods.

Property and Equipment

Property and equipment are recorded at cost. The cost of our satellites and related ground systems include capitalized interest costs incurred during their construction and development period, as well as, capitalized costs for internal direct labor costs incurred in the construction and development. Ground systems are placed into service when they are ready for their intended use. While under construction, the costs of our satellites are capitalized during the construction phase, assuming the eventual successful launch and in-orbit operation of the satellite. If a satellite were to fail during launch or while in-orbit, the resulting loss would be charged to expense in the period in which such loss were to occur. The amount of any such loss would be reduced to the extent of insurance proceeds received as a result of the launch or in-orbit failure.

We capitalize certain costs incurred to develop software for internal use. We expense the costs of developing computer software until the software has reached the application development stage and capitalize all costs incurred from that time until the software is ready for its intended use, at which time amortization of the capitalized costs begins. Determination of when the software has reached the application development stage is based upon completion of conceptual designs, evaluation of alternative designs and performance requirements. Costs of major enhancements to internal use software are capitalized while routine maintenance of existing software is charged to expense as incurred. The determination of when the software is in the application development stage and the ongoing assessment of the recoverability of capitalized computer software development costs requires considerable judgment by management with respect to certain factors, including, but not limited to, estimated economic life and changes in software and hardware technology.

Internal use capitalized software costs are amortized over their expected useful life, which is generally three to five years. Software costs that are directly related to a satellite are capitalized with the satellite and amortized over the satellite’s useful life. Amortization expense related to capitalized software costs, exclusive of software costs amortized as part of the cost of our satellites, was $7.5 million, $11.0 million and $10.7 million, for the years ended December 31, 2009, 2010, and 2011, respectively.

Depreciation is computed using the straight-line method over the estimated useful lives of the respective assets, such as three to seven years for computer equipment and five to eleven years for most other assets, including the satellite and ground stations. Leasehold improvements and assets used pursuant to capital-lease obligations are amortized on a straight-line basis over the shorter of their useful lives or lease terms; such amortization is included in depreciation expense. Upon sale or retirement, the cost and related accumulated depreciation are eliminated from the respective accounts and the resulting gain or loss is included in operations. Repairs and maintenance are expensed as incurred.

Accounting for Stock Options

We apply the fair value recognition provisions of stock-based compensation expense and measure stock compensation at the grant date based on the fair value of the award and recognize it as expense over the requisite service period, which is generally the vesting period. In order to determine the fair value of our common stock on the date of grant for purposes of calculating the fair value of our stock option grants, we utilize the most recent publicly traded stock price on the grant date.

 

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We established a peer group of comparable publicly traded companies. Annually, we review the companies that comprise the peer group and that from time to time have changed the composition of the peer group, based on changes to our business or the business of the comparable companies and other factors outside of our control, such as mergers and consolidations.

At each stock option grant date, we utilized the peer group data to calculate our expected volatility. Expected volatility was based on comparable companies’ four-year history for options granted prior to 2009, and five-year history for options granted after 2009. Expected term and forfeiture rate were based on existing employee exercise patterns and our historical pre-vested forfeiture experience. The risk-free rate was based on an average of the yields of the Treasury note with a maturity corresponding to the expected term of the option assumed at the grant date.

Changes to the underlying assumptions, including increased forfeiture rates, may have a significant impact on the underlying value of the stock options, which could have a material impact on our financial statements.

New Accounting Pronouncements

In September 2011, the FASB issued authoritative guidance to allow entities to use a qualitative approach to test goodwill for impairment. This authoritative guidance permits an entity to first perform a qualitative assessment to determine whether it is more likely than not that the fair value of a reporting unit is less than its carrying value. If it is concluded that this is the case, it is necessary to perform the two-step goodwill impairment test. Otherwise, the two-step goodwill impairment test is not required. This guidance is effective for annual and interim goodwill impairment tests performed for fiscal years beginning after December 15, 2011 and earlier adoption is permitted. We do not expect the implementation of this authoritative guidance to have an impact on our financial position or results of operations.

In June 2011, the FASB issued authoritative guidance on the presentation of comprehensive income to require an entity to present the total of comprehensive income, the components of net income, and the components of other comprehensive income either in a single continuous statement of comprehensive income or in two separate but consecutive statements. This authoritative guidance eliminates the option to present the components of other comprehensive income as part of the statement of equity. This guidance is effective for us in the first quarter of fiscal 2012, with early adoption permitted, and should be applied retrospectively. The implementation of this authoritative guidance will only change the presentation of comprehensive income and will have no impact on our financial position or results of operations.

In May 2011, the FASB issued authoritative guidance to provide a consistent definition of fair value and ensure that the fair value measurement and disclosure requirements are similar between U.S. GAAP and International Financial Reporting Standards. This authoritative guidance limits the highest-and-best-use measure to nonfinancial assets, permits certain financial assets and liabilities with offsetting positions in market or counterparty credit risks to be measured at a net basis, and provides guidance on the applicability of premiums and discounts. This authoritative guidance also expands the disclosures on Level 3 inputs by requiring quantitative disclosure of the unobservable inputs and assumptions, as well as description of the valuation processes and the sensitivity of the fair value to changes in unobservable inputs. The new guidance will be effective for us in the first quarter of fiscal 2012. The implementation of this authoritative guidance is not expected to have a material impact on our financial position or results of operations.

In December 2010, the FASB amended its existing guidance for goodwill and other intangible assets. This authoritative guidance modifies Step 1 of the goodwill impairment test for reporting units with zero or negative carrying amounts. For those reporting units, an entity is required to perform Step 2 of the goodwill impairment test if there are qualitative factors indicating that it is more likely than not that a goodwill impairment exists. The qualitative factors are consistent with the existing guidance which requires goodwill of a reporting unit to be tested for impairment between annual tests if an event occurs or circumstances change that would more likely than not reduce the fair value of a reporting unit below its carrying amount. This authoritative guidance becomes

 

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effective for us in the first quarter fiscal 2012. The implementation of this authoritative guidance is not expected to have a material impact on our financial position or results of operations.

Seasonality

Seasonality has not had a material impacted on our business and we do not expect it to have a material impact in the future.

 

ITEM 7A.

QUANTITATIVE AND QUALITATIVE DISCLOSURES ABOUT MARKET RISK

We are exposed to market risks from changes in interest rates under our senior secured facility. The facility provides for a $500 million term loan facility and a $100 million revolving credit facility. At the closing of the facility, we borrowed the full amount of the term loan facility. As of December 31, 2011, we had not drawn any amounts under the revolving credit facility.

Borrowings under the senior credit facility bear interest, at our option, at a rate equal to either an adjusted LIBOR rate or a base rate, in each case, plus the applicable margin. The applicable margin for borrowings under the term loan facility is 4.5% for adjusted LIBOR loans or 3.5% for base rate loans. The applicable margin for borrowings under the revolving credit facility may change depending upon our leverage ratio, up to a maximum of 4.5%. Our term loan facility currently bears interest based upon the LIBOR-based rate.

Based upon the amounts outstanding under the term loan facility as of December 31, 2011 and assuming that the facility is outstanding for a full calendar year, a 100 basis point increase in interest rates would result in an increase in our annual interest expense under the facility of approximately $5.0 million. We may decide in the future to engage in various hedging transactions in order to hedge the interest rate risk under our senior secured credit facility but have not done so at this time.

We are exposed to various market risks that arise from transactions entered into in the normal course of business. Certain contractual relationships with customers and vendors mitigate risks from currency exchange rate changes that arise from normal purchasing and normal sales activities.

We do not currently have any material foreign currency exposure. Our revenue contracts are primarily denominated in U.S. dollars and the majority of our purchase contracts are denominated in U.S. dollars.

 

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ITEM 8.

FINANCIAL STATEMENTS AND SUPPLEMENTARY DATA

INDEX TO CONSOLIDATED FINANCIAL STATEMENTS

 

     Page  

Report of Independent Registered Public Accounting Firm

     48   

Consolidated Statements of Operations

     49   

Consolidated Balance Sheets

     50   

Consolidated Statements of Cash Flows

     51   

Consolidated Statements of Stockholders’ Equity and Comprehensive Income (Loss)

     52   

Notes to Consolidated Financial Statements

     53   

 

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Report of Independent Registered Public Accounting Firm

To the Board of Directors and Stockholders of DigitalGlobe, Inc.

In our opinion, the accompanying consolidated balance sheets and the related consolidated statements of operations, stockholders’ equity and comprehensive income (loss), and cash flows present fairly, in all material respects, the financial position of DigitalGlobe, Inc. and its subsidiaries at December 31, 2011 and 2010, and the results of their operations and their cash flows for each of the three years in the period ended December 31, 2011 in conformity with accounting principles generally accepted in the United States of America. Also in our opinion, the Company did not maintain, in all material respects, effective internal control over financial reporting as of December 31, 2011, based on criteria established in Internal Control — Integrated Framework issued by the Committee of Sponsoring Organizations of the Treadway Commission (COSO) because material weaknesses in internal control over financial reporting related to the Company’s accounting for its Direct Access Program and its complement of personnel with appropriate accounting knowledge and training existed as of that date. A material weakness is a deficiency, or a combination of deficiencies, in internal control over financial reporting, such that there is a reasonable possibility that a material misstatement of the annual or interim financial statements will not be prevented or detected on a timely basis. The material weaknesses referred to above are described in Management’s Report on Internal Control over Financial Reporting appearing under Item 9A. We considered these material weaknesses in determining the nature, timing, and extent of audit tests applied in our audit of the 2011 consolidated financial statements and our opinion regarding the effectiveness of the Company’s Internal control over financial reporting does not affect our opinion on those consolidated financial statements. The Company’s management is responsible for these financial statements, for maintaining effective internal control over financial reporting and for its assessment of the effectiveness of internal control over financial reporting included in management’s report referred to above. Our responsibility is to express opinions on these financial statements and on the Company’s internal control over financial reporting based on our integrated audits. We conducted our audits in accordance with the standards of the Public Company Accounting Oversight Board (United States). Those standards require that we plan and perform the audits to obtain reasonable assurance about whether the financial statements are free of material misstatement and whether effective internal control over financial reporting was maintained in all material respects. Our audits of the financial statements included examining, on a test basis, evidence supporting the amounts and disclosures in the financial statements, assessing the accounting principles used and significant estimates made by management, and evaluating the overall financial statement presentation. Our audit of internal control over financial reporting included obtaining an understanding of internal control over financial reporting, assessing the risk that a material weakness exists, and testing and evaluating the design and operating effectiveness of internal control based on the assessed risk. Our audits also included performing such other procedures as we considered necessary in the circumstances. We believe that our audits provide a reasonable basis for our opinions.

A company’s internal control over financial reporting is a process designed to provide reasonable assurance regarding the reliability of financial reporting and the preparation of financial statements for external purposes in accordance with generally accepted accounting principles. A company’s internal control over financial reporting includes those policies and procedures that (i) pertain to the maintenance of records that, in reasonable detail, accurately and fairly reflect the transactions and dispositions of the assets of the company; (ii) provide reasonable assurance that transactions are recorded as necessary to permit preparation of financial statements in accordance with generally accepted accounting principles, and that receipts and expenditures of the company are being made only in accordance with authorizations of management and directors of the company; and (iii) provide reasonable assurance regarding prevention or timely detection of unauthorized acquisition, use, or disposition of the company’s assets that could have a material effect on the financial statements.

Because of its inherent limitations, internal control over financial reporting may not prevent or detect misstatements. Also, projections of any evaluation of effectiveness to future periods are subject to the risk that controls may become inadequate because of changes in conditions, or that the degree of compliance with the policies or procedures may deteriorate.

/s/ PricewaterhouseCoopers LLP

Denver, Colorado

February 29, 2012

 

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DigitalGlobe, Inc.

Consolidated Statements of Operations

 

     For the Year  Ended
December 31,
 
       2009             2010    
Revised
        2011      
    

(In millions, except
per share data)

 

Revenue

   $ 281.9      $ 322.5      $ 339.5   

Costs and expenses:

      

Cost of revenue, excluding depreciation and amortization

     31.1        44.2        64.9   

Selling, general and administrative

     88.6        112.2        130.2   

Depreciation and amortization

     74.4        118.9        117.1   
  

 

 

   

 

 

   

 

 

 

Income from operations

     87.8        47.2        27.3   

Loss from early extinguishment of debt

     (7.7            (51.8

Loss on derivative instruments

     (1.8              

Other income (expense), net

                   0.2   

Interest income (expense), net

     0.1        (40.4     (21.7
  

 

 

   

 

 

   

 

 

 

Income (loss) before income taxes

     78.4        6.8        (46.0

Income tax (expense) benefit

     (31.0     (4.3     17.9   
  

 

 

   

 

 

   

 

 

 

Net income (loss)

   $ 47.4      $ 2.5      $ (28.1
  

 

 

   

 

 

   

 

 

 

Earnings (loss) per share:

      

Basic earnings (loss) per share

   $ 1.07      $ 0.05      $ (0.61
  

 

 

   

 

 

   

 

 

 

Diluted earnings (loss) per share

   $ 1.06      $ 0.05      $ (0.61
  

 

 

   

 

 

   

 

 

 

Weighted average common shares outstanding:

      

Basic

     44.2        45.7        45.9   
  

 

 

   

 

 

   

 

 

 

Diluted

     44.9        46.1        45.9   
  

 

 

   

 

 

   

 

 

 

 

The accompanying notes are an integral part of these Consolidated Financial Statements.

 

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DigitalGlobe, Inc.

Consolidated Balance Sheets

 

     As of December 31,  
   2010
Revised
    2011  
     (In millions)  

ASSETS

  

CURRENT ASSETS:

    

Cash and cash equivalents

   $ 179.3      $ 198.5   

Restricted cash

     6.7        7.7   

Accounts receivable, net of allowance for doubtful accounts of $1.0 and $3.6, respectively

     45.3        50.7   

Prepaid and current assets

     21.4        19.6   

Deferred taxes

     62.7        65.1   
  

 

 

   

 

 

 

Total current assets

     315.4        341.6   

Property and equipment, net of accumulated depreciation of $478.2 and $563.9, respectively

     878.6        1,019.8   

Goodwill

     8.7        8.7   

Intangibles, net of accumulated amortization of $8.9 and $7.4, respectively

     0.3          

Aerial image library, net of accumulated amortization of $21.1 and $25.1, respectively

     1.9        13.0   

Long-term restricted cash

     13.6        9.8   

Long-term deferred contract costs

     42.4        44.7   

Other assets, net

     7.2        14.0   
  

 

 

   

 

 

 

Total assets

   $ 1,268.1      $ 1,451.6   
  

 

 

   

 

 

 

LIABILITIES AND STOCKHOLDERS’ EQUITY

  

CURRENT LIABILITIES:

    

Accounts payable

   $ 15.0      $ 19.7   

Accrued interest

     6.2        0.2   

Current note payable

            5.0   

Other accrued liabilities

     27.2        37.5   

Current portion of deferred revenue

     39.1        36.6   
  

 

 

   

 

 

 

Total current liabilities

     87.5        99.0   

Long-term accrued liability

     8.7        1.4   

Deferred rev e nue

     246.7        319.3   

Deferred lease incentive

     4.6        3.3   

Long-term debt, net of discount

     346.1        481.6   

Long-term deferred tax liability, net

     75.6        59.6   
  

 

 

   

 

 

 

Total liabilities

   $ 769.2      $ 964.2   
  

 

 

   

 

 

 

COMMITMENTS AND CONTINGENCIES (Note 14)

    

STOCKHOLDERS’ EQUITY

    

Preferred stock, $0.001 par value; 24,000,000 shares authorized; no shares issued and outstanding at December 31, 2010 and December 31, 2011

              

Common stock; $0.001 par value; 250,000,000 shares authorized; 46,029,652 shares issued and outstanding at December 31, 2010 and 46,320,471 shares issued and outstanding at December 31, 2011

     0.2        0.2   

Treasury stock, at cost; 44,039 shares at December 31, 2010 and 66,175 shares at December 31, 2011

     (0.7     (1.2

Additional paid-in capital

     512.9        530.0   

Accumulated deficit

     (13.5     (41.6
  

 

 

   

 

 

 

Total stockholders’ equity

     498.9        487.4   
  

 

 

   

 

 

 

Total liabilities and stockholders’ equity

   $ 1,268.1      $ 1,451.6   
  

 

 

   

 

 

 

The accompanying notes are an integral part of these Consolidated Financial Statements.

 

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DigitalGlobe, Inc.

Consolidated Statements of Cash Flows

 

     For the Year Ended December 31,  
       2009             2010             2011      
           Revised        
    

(In millions)

 

CASH FLOWS FROM OPERATING ACTIVITIES:

      

Net income (loss)

   $ 47.4      $ 2.5      $ (28.1

Adjustments to reconcile net income to net cash provided by operating activities:

      

Depreciation and amortization expense

     74.4        118.9        117.1   

EnhancedView deferred revenue

            24.8        94.6   

Recognition of pre-FOC payments

     (25.5     (25.5     (25.5

Amortization of aerial image library, deferred contract costs and lease incentive

     5.3        8.7        10.2   

Non-cash stock compensation expense

     7.2        6.6        14.4   

Amortization of debt issuance costs

            4.4        4.4   

Write off of debt financing fees

     5.3               12.0   

Gain on sale of asset

                   (0.5

Deferred income taxes

     33.6        3.3        (18.5

Changes in working capital, net of investing activities:

      

Accounts receivable, net

     (2.6     4.3        (5.4

Accounts receivable from related party

     (0.3              

Income tax receivable

     (3.9     3.9          

Prepaids and other assets

     (12.4     (3.9     (14.7

Accounts payable

     1.5        (1.8     5.5   

Accounts payable and accrued liabilities to related parties

     3.5                 

Accrued liabilities

     (5.0     14.3        (4.2

Deferred contract costs from related party

     (15.3              

Deferred contract costs

            (18.0     (9.0

Deferred revenue

     28.0        10.6        4.5   

Deferred revenue related party

     2.1                 

Deferred lease incentive

            0.2          

Payment of Senior Secured Note discount

                   (13.2

Premium payment on senior secured notes

                   (0.8
  

 

 

   

 

 

   

 

 

 

Net cash flows provided by operating activities

     143.3        153.3        142.8   
  

 

 

   

 

 

   

 

 

 

CASH FLOWS FROM INVESTING ACTIVITIES:

      

Construction in progress additions

     (155.9     (74.1     (255.6

Other property, equipment and intangible additions

     (10.9     (10.6     (6.6

Decrease (increase) in restricted cash

     (21.5     3.8        2.7   

Settlements from derivative instrument

     (2.8              
  

 

 

   

 

 

   

 

 

 

Net cash flows used in investing activities

     (191.1     (80.9     (259.5
  

 

 

   

 

 

   

 

 

 

CASH FLOWS FROM FINANCING ACTIVITIES:

      

Proceeds from issuance of debt

     341.8               487.0   

Proceeds from initial public offering, net of issuance costs

     21.7        (0.3       

Repayment of notes

     (270.0            (341.8

Payment of debt issuance cost

     (10.9            (11.1

Repurchase of common stock

     (0.5              

Proceeds from exercise of stock options

     1.9        10.2        1.8   
  

 

 

   

 

 

   

 

 

 

Net cash flows provided by financing activities

     84.0        9.9        135.9   
  

 

 

   

 

 

   

 

 

 

Net increase (decrease) in cash and cash equivalents

     36.2        82.3        19.2   

Cash and cash equivalents, beginning of period

     60.8        97.0        179.3   
  

 

 

   

 

 

   

 

 

 

Cash and cash equivalents, end of period

   $ 97.0      $ 179.3      $ 198.5   
  

 

 

   

 

 

   

 

 

 

SUPPLEMENTAL CASH FLOW INFORMATION:

      

Cash paid for interest, net of capitalized amounts of $37.4, $7.7 and $18.6, respectively

   $      $ 30.2      $ 23.2   

Cash received (paid) for income taxes

   $ (2.4   $ 4.2      $ (1.7

NON-CASH INVESTING AND FINANCING ACTIVITIES:

      

Changes to non-cash construction in progress accruals, including interest

   $ 9.7      $ 16.9      $ (0.5

The accompanying notes are an integral part of these Consolidated Financial Statements.

 

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DigitalGlobe, Inc.

Consolidated Statements of Stockholders’ Equity and Comprehensive Income (Loss)

 

    Common Stock     Treasury Stock     Additional
Paid-in
    Accumulated
Deficit
    Accumulated
Other
Comprehensive
Income (Loss)
    Comprehensive
Income (Loss)
    Total
Stockholders’
Equity
 
    Shares     Amount     Shares     Amount            
    (In millions, excluding share and per share data)  

Balance at December 31, 2008

    43,468,941      $ 0.2        (21,555   $ (0.2   $ 467.2      $ (63.4   $ (1.5   $ 52.0      $ 402.3   

Stock issued upon exercise of stock options

    258,377                             1.9                             1.9   

Common stock issued in connection with successful initial public offering

    1,395,275                             19.0                             19.0   

Repurchases common stock

                  (22,484     (0.5                                 (0.5

Stock compensation expense, net of forfeitures

                                7.9                             7.9   

Effective financial derivatives, net of tax

                                              1.5        1.5        1.5   

Net income

                                       47.4               47.4        47.4   
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Balance at December 31, 2009

    45,122,593      $ 0.2        (44,039   $ (0.7   $ 496.0      $ (16.0   $      $ 48.9      $ 479.5   

Stock issued upon exercise of stock options and stock grants

    951,098                             10.2                             10.2   

Public offering fees

                                (0.3                          (0.3

Stock compensation expense, net of forfeitures

                                7.0                             7.0   

Net income (revised)

                                       2.5               2.5        2.5   
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Balance at December 31, 2010 (revised)

    46,073,691      $ 0.2        (44,039   $ (0.7   $ 512.9      $ (13.5   $      $ 2.5      $ 498.9   
                 

Stock issued upon exercise of stock options and stock grants

    312,955                             1.8                             1.8   

Repurchases common stock

                  (22,136     (0.5                                 (0.5

Stock compensation expense, net of forfeitures

                                15.3                             15.3   

Net loss

                                       (28.1            (28.1     (28.1
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Balance at December 31, 2011

    46,386,646      $ 0.2        (66,175   $ (1.2   $ 530.0      $ (41.6   $      $ (28.1   $ 487.4   
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

 

The accompanying notes are an integral part of these Consolidated Financial Statements.

 

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DigitalGlobe, Inc.

Notes to Consolidated Financial Statements

(Dollars in millions except for share and per share data, unless otherwise noted)

 

NOTE 1.

General Information

DigitalGlobe, Inc. (“DigitalGlobe”, the “Company” or “we”) is a leading global provider of commercial high-resolution earth imagery products and services that support a wide variety of uses, including defense, intelligence and homeland security applications, mapping and analysis, environmental monitoring, oil and gas exploration, and infrastructure management. We own and operate three imagery satellites — QuickBird, WorldView-1 and WorldView-2 — which collect panchromatic (black and white) and color imagery using visible and near-infrared wavelengths. We also offer a range of on-line and off-line distribution options designed to enable customers to easily access and integrate our imagery into their business operations and applications.

 

NOTE 2.

Summary of Significant Accounting Policies

Principles of Consolidation and Basis of Presentation

The consolidated financial statements include the accounts of DigitalGlobe, Inc. and its wholly owned subsidiaries. All significant intercompany transactions have been eliminated in consolidation. The consolidated financial statements have been prepared in accordance with accounting principles generally accepted in the United States of America (GAAP) and the instructions to Form 10-K of the Securities and Exchange Commission (SEC).

Use of Estimates

The preparation of financial statements in conformity with GAAP requires management to make estimates and assumptions that affect the reported amounts of assets and liabilities and disclosure of contingent assets and liabilities at the date of the financial statements and reported amounts of revenue and expenses during the reporting period. However, due to the inherent uncertainties in making estimates, actual results could differ from those estimates.

Accounts Receivable

The Company’s customer base includes customers located in foreign countries. The Company controls credit risk related to accounts receivable through credit approvals, credit limits and monitoring processes. In making the determination of the appropriate allowance for doubtful accounts, the Company considers specific accounts, analysis of accounts receivable aging reports, changes in customer payment patterns, historical write-offs, changes in customer demand and relationships, and customer creditworthiness.

Property and Equipment

Property and equipment are recorded at cost less accumulated depreciation. The cost of our satellites and related ground systems include capitalized interest costs incurred during the construction and development period, as well as capitalized costs for internal direct labor. Ground systems are placed into service when they are ready for their intended use. While under construction, the costs of our satellites are capitalized assuming the eventual successful launch and in-orbit operation of the satellite. If a satellite were to fail during launch or while in-orbit, the resulting loss would be charged to expense in the period in which such loss was to occur. The amount of any such loss would be reduced to the extent of insurance proceeds received as a result of the launch or in-orbit failure.

The Company performs an annual assessment of the useful lives of the satellites or more frequently should facts and circumstances indicate. The assessment evaluates the efficiencies of the operation of the satellite and the fuel level. An adjustment will be made to the estimated depreciable life of the satellite, if deemed necessary

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

by the assessment performed. Any changes to the estimated useful life of our satellites and the related impact on depreciation expense will be accounted for on a prospective basis as of the date of the change.

The Company reviews the carrying value of its long-lived assets whenever events or changes in circumstances indicate that the carrying amount of the assets might not be recoverable. Factors that would require an impairment assessment include a significant change in the extent or manner in which an asset is used, a significant adverse change in the operation of the Company’s satellites, a change in government spending or customer demand that could affect the value of the asset group, or a significant decline in the observable market value of an asset group. If these factors indicate a potential impairment, the Company would assess the recoverability of the asset group by determining if the carrying value of the asset group exceeds the projected undiscounted cash flows expected to result from the use and eventual disposition of the asset group over the remaining economic life of the asset group. If the recoverability test indicates that the carrying value of the asset group is not recoverable, the Company will estimate the fair value of the asset group estimating discounted cash flows. Any impairment would be measured as the difference between the asset’s carrying amount and its estimated fair value. There were no impairment charges recorded in 2009, 2010 or 2011.

The Company capitalizes certain costs incurred to develop software for internal use. The Company expenses the costs of developing computer software until the software has reached the application development stage and capitalizes all costs incurred from that time until the software is ready for its intended use, at which time amortization of the capitalized costs begins. Determination of when the software has reached the application development stage is based upon completion of conceptual designs, evaluation of alternative designs and performance requirements. Costs of major enhancements to internal use software are capitalized while routine maintenance of existing software is charged to expense as incurred. The determination of when the software is in the application development stage and the ongoing assessment of the recoverability of capitalized computer software development costs requires considerable judgment by management with respect to certain factors, including, but not limited to, estimated economic life and changes in software and hardware technology.

Depreciation is computed using the straight-line method over the estimated useful lives of the respective assets (three to seven years for computer equipment and five to eleven years for most other assets, including the satellites and ground stations). Leasehold improvements and assets used pursuant to leases are depreciated on a straight-line basis over the shorter of their useful lives or lease terms; such depreciation is included in depreciation expense. Upon sale or retirement, the cost and related accumulated depreciation are eliminated from the respective accounts and the resulting gain or loss is included in operations. Repairs and maintenance are expensed as incurred.

Internal use capitalized software costs are amortized over their expected useful life, which is generally three to five years. Software costs that are directly related to a satellite are capitalized with the satellite and amortized over the satellite’s estimated useful life on a straight line basis. Amortization expense related to capitalized software costs, exclusive of software cost amortized as part of the cost of our satellites, was $7.5 million, $11.0 million and $10.7 million for 2009, 2010 and 2011, respectively.

Goodwill and Intangible Assets

Goodwill represents the excess of purchase price over the fair value of net assets acquired. Intangible assets (identified as trademarks, core technology, customer relationships and non-compete agreements) are recorded at fair value as determined at the time of acquisition. The goodwill and intangible assets are attributable to the commercial segment.

We test the carrying value of goodwill for impairment on the reporting unit level on an annual basis and more often if a triggering event occurs that would more likely than not reduce the fair value of a reporting unit below its carrying amount. The impairment test consists of comparing the fair value of the reporting unit, determined using discounted cash flows, with its carrying amount including goodwill. If the carrying amount of

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

the reporting unit exceeds its fair value, the Company compares the implied value of the goodwill with its carrying amount. If the carrying amount of the goodwill exceeds the implied fair value of goodwill, an impairment loss would be recognized to reduce the carrying amount to its implied fair value. We have completed our impairment test on goodwill at December 31, 2011, and determined that there was no impairment.

Aerial Image Library

Our aerial image library costs are composed of the direct costs of contracting with third parties to collect aerial imagery. Our aerial image library costs are charged to cost of revenue over the estimated economic life of the imagery, which has been estimated to be two to five years. Such costs are charged to cost of revenue on an accelerated basis reflective of the pattern in which the economic benefit of the asset is expected to be realized. Charges to cost of revenue for the aerial imagery library were $5.6 million, $4.0 million and $4.0 million for 2009, 2010 and 2011, respectively.

Deferred Contract Costs

The Company capitalized certain costs reimbursable under the NextView agreement, incurred in the construction and development of our WorldView-1 satellite and related ground systems during the construction and development period. These costs were related to internal support costs and reimbursable expenditures under the NextView agreement. These costs were not capitalized as fixed assets, but were deferred in accordance with government contract accounting guidelines. Upon the successful launch of the WorldView-1 satellite, the deferred contract costs began being amortized ratably over the customer relationship period (the same as the expected life of the satellite, or 10.5 years). There were no deferred contract costs capitalized for our QuickBird or WorldView-2 satellites.

The Company defers certain direct costs incurred in the construction of direct access facilities built for DAP customers, consisting of hardware, software and labor purchased from a related party. The direct access facility will allow the Company’s DAP customers to communicate with the Company’s satellites. The deferred contract costs are recognized as expense over the same period that the related revenue is recognized, which is the estimated customer relationship period, except when deferred contract costs are in excess of related revenues, in which case the excess costs are recognized over the initial contract period. The customer relationship period is based on the estimated useful life of the satellite being used. If more than one satellite is being used the satellite with the longest life is used as the basis for the amortization. The Company has deferred contract costs in excess of related contract deferred revenue for some of its customers. As of December 31, 2010 and 2011 deferred contract costs totaled $49.2 million and $52.5 million, respectively.

Debt Issuance Costs and Debt Discounts

Debt issuance costs and debt discounts are deferred and amortized to interest expense using the effective interest method.

Revenue Recognition

Our principal source of revenue is the licensing of earth imagery products and services for end users and resellers. Revenue is recognized when the following criteria have been met: persuasive evidence of an arrangement exists, delivery has occurred or services have been rendered, the fee is fixed or determinable and the collection of funds is reasonably assured. Our revenue is generated from: (i) sales of or royalties arising from licenses of imagery; and (ii) subscription services and other service arrangements.

Sales of Licenses.     Revenue from sales of imagery licenses is recognized when the images are physically delivered to the customer or, in the case of electronic delivery, when the customer is able to directly download the image from our system. In certain customer arrangements, we must satisfy certain acceptance provisions. For

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

these arrangements, revenue is recognized upon acceptance by these customers. Revenue is recognized net of contractually agreed discounts.

Royalties.     Revenue from royalties is based on agreements or licenses with third parties that allow the third party to incorporate our product into their value added product for commercial distribution. Revenue from these royalty arrangements is recorded in the period earned or on a systematic basis over the term of the license agreement. For those royalties that are due to third parties based on our revenue sharing arrangements, we report royalty revenue on a net basis.

Subscriptions.     We sell online subscriptions to our products. These arrangements allow customers access to our products via the internet for a set period of time and a fixed fee. The subscription revenue is recorded as deferred revenue and recognized ratably over the subscription period. In addition, we have other arrangements in which customers pay for their subscription to one of our web-based products by paying for a predetermined amount of access (for example, each time users click on an image of their home). In the case of prepayment, each time a product is accessed, a portion of the customer’s prepayment is earned. These prepayments are recorded as deferred revenue when received and the revenue is recognized based on the number of times the product is accessed. Revenue is recognized net of contractually agreed discounts.

Service Level Agreements (SLA).     We recognize service level agreement revenue net of any allowances resulting from failure to meet certain stated monthly performance metrics. Net revenue is either recognized ratably over time for a defined and fixed level of service, or based on proportional performance when the level of service changes based on certain criteria stated in the agreement.

Multiple Deliverable Arrangements .    We enter into revenue arrangements that may consist of multiple deliverables of our product and service offerings based on the needs of our customers. These arrangements may include products delivered at the onset of the agreement, as well as products or services that are delivered over multiple reporting periods.

In October 2009, the FASB issued ASU 2009-13, “Multiple-Deliverable Revenue Arrangements” and ASU 2009-14, “Certain Revenue Arrangements That Include Software Elements.” We concurrently adopted ASU 2009-13 and ASU 2009-14 prospectively on January 1, 2011. ASU 2009-13 changes the requirements for establishing separate units of accounting in a multiple deliverable arrangement and requires the allocation of arrangement consideration to each deliverable based on the relative selling price. The selling price for each deliverable is based on vendor-specific objective evidence (VSOE) if available, third-party evidence (TPE) if VSOE is not available, or best estimate selling price (BESP) if neither VSOE nor TPE is available. ASU 2009-14 excludes software that is contained in a tangible product from the scope of software revenue guidance if the software is essential to the tangible product’s functionality.

We have generally been unable to establish VSOE for any of our products due to our infrequently selling each deliverable separately or only having a limited sales history, such as in the case of new or emerging products. As of December 31, 2011, we have been unable to establish TPE for any of our offerings due to the unique nature of our products and services and the limited number of competitors. As we are unable to establish price on the basis of VSOE or TPE, we use BESP to determine the allocation of arrangement consideration. The objective of BESP is to determine the price at which we would transact a sale if the product or service were sold on a standalone basis. We determine BESP for a product or service by considering multiple factors, including but not limited to market conditions, competitive landscape, internal costs, gross margin objectives, product technology lifecycles, pricing practices, and our go-to-market strategy.

The adoption of ASU 2009-13 and ASU 2009-14 was not material to our financial results for the year ended December 31, 2011. We are not able to reasonably estimate the effect of adopting these standards on future periods as the impact will vary based on the nature and volume of new or materially modified multiple element arrangements transacted in any given period.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

While multiple deliverable arrangements occur throughout our business, the EnhancedView contract (EnhancedView) with National Geospatial-Intelligence Agency (NGA) and the Direct Access Program (DAP) make up the majority of our multiple deliverable arrangement activity. EnhancedView and four of our DAP agreements were entered into prior to the January 1, 2011 adoption of ASU 2009-13 and ASU 2009-14 and none have been subsequently materially modified. As we adopted the new guidance on a prospective basis, the agreements will continue to be accounted for under the pre-adoption guidance unless they are materially modified. The following is a description of the accounting for these arrangements.

EnhancedView.     The EnhancedView contract contains multiple deliverables, including an SLA, infrastructure enhancements, and other services. We determined that these deliverables do not qualify as separate units of accounting due to a lack of standalone value for the delivered elements and a lack of objective reliable evidence of fair value for any of the undelivered elements in the arrangement. We recognize revenue on a single unit of accounting using a proportional performance method based on the estimated capacity of our constellation made available to NGA compared to the total estimated capacity to be provided over the life of the contract.

Direct Access Program.     Revenue under the direct access program includes construction of the direct access facility and an arrangement to allow the customer access to the satellite to task and download imagery. In these arrangements the facility is delivered upon completion and customer acceptance, and the maintenance and access services occur over several subsequent reporting periods. These arrangements have generally been treated as a single unit of accounting due to a lack of standalone value for the delivered elements and a lack of objective reliable evidence of fair value for any of the undelivered items. Accordingly, all funds received are initially recorded as deferred revenue. As the direct access facilities are brought into service, the deferred revenue is amortized ratably over the estimated customer relationship period, which is consistent with the estimated remaining useful life of the satellite being used.

Satellite Insurance

As of December 31, 2011, we maintain the following insurance coverage on our satellites:

 

Satellite

   Policy Period      Coverage  
            (In millions)  

QuickBird

     10/2011 — 10/2012       $ 11.0   

WorldView-1

     10/2011 —10/2012         235.0   

WorldView-2

     10/2011 — 10/2012         182.0   

WorldView-2

     10/2009 — 10/2012         68.0   

The satellite insurance coverage will pay us in the event of a total loss of a satellite or will indemnify us for partial losses if the functional capacity of the satellite is significantly impaired due to anomalies with the satellite equipment or other events causing significant impairment.

Satellite insurance premiums, corresponding to the launch and in-orbit commissioning period prior to the satellite reaching FOC, are capitalized in the original cost of the satellite and are amortized over the estimated useful life of the asset. The remainder of the insurance premiums that are not capitalized to the cost of the satellite are recorded as prepaid expenses and amortized to expense ratably over the related policy periods and are included in selling, general and administrative costs.

Research and Development Costs

We record as research and development expense all engineering costs, consisting primarily of internal labor and consulting fees, where the Company maintains the risk associated with design failure. We incurred $0.9 million, $1.7 million and $2.0 million in research and development costs for the years ended December 31, 2009, 2010 and 2011, respectively. Any research and development expenses incurred are included in selling, general and administrative expenses.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

Derivative Instruments

Prior to 2010, the Company used derivative financial instruments for the purpose of hedging exposures to fluctuations in interest rates. The Company’s derivative instruments were recorded in the consolidated balance sheets at fair value within accounts receivable from related party or accounts payable to related party dependent upon the asset or liability position of the instrument. Upon settlement of the contracts, the cash flow was presented as an investing activity in the consolidated statements of cash flows. For a derivative designated as a cash flow hedge, the effective portion of the derivative gain or loss was initially reported as a component of accumulated other comprehensive income and subsequently reclassified into earnings when the forecasted transaction affected earnings. For derivatives that did not qualify or were not designated as cash flow hedges, all gains or losses associated with changes to the fair market value of these financial instruments were recorded in the income statement. As of December 31, 2010 and 2011, the Company did not hold any derivative instruments.

Earnings Per Share (EPS)

Basic EPS is computed by dividing net income by the weighted average number of shares of common stock outstanding (excluding non-vested restricted shares). Diluted EPS is determined by dividing net income by the sum of (1) the weighted average number of common shares outstanding and (2) the dilutive effect of outstanding potentially dilutive securities and stock options determined utilizing the treasury stock method.

Stock-Based Compensation

Stock-based compensation expense is measured at the grant date based on the fair value of the award and is recognized as expense over the requisite service period. See Note 10 for further information regarding our stock-based compensation expense and underlying assumptions.

Income Taxes

Deferred tax assets and liabilities are recognized for the estimated future tax effects attributable to the temporary differences between the financial statement carrying amounts of existing assets and liabilities and their respective tax bases as well as operating loss and tax credit carryforwards. The effect on deferred tax assets and liabilities of a change in enacted tax laws is recognized as an adjustment to the tax provision or benefit in the period of enactment. The overall change in deferred tax assets and liabilities during the period is equal to the deferred tax expense or benefit for the period. The carrying value of deferred tax assets may be reduced by a valuation allowance if, based upon the judgmental assessment of available evidence, it is deemed more likely than not that some or all of the deferred tax assets will not be realizable.

We utilize a two-step approach to recognizing and measuring uncertain tax positions (tax contingencies). The first step is to evaluate the tax position for recognition by determining if the weight of available evidence indicates it is more likely than not that the position will be sustained on audit, including resolution of related appeals or litigation processes. The second step is to measure the tax benefit as the largest amount which is more than 50% likely of being realized upon ultimate settlement. We consider many factors when evaluating and estimating our tax positions and tax benefits, which may require periodic adjustments and which may not accurately forecast actual outcomes. We include interest and penalties related to our tax contingencies in income tax expense.

Fair Values of Financial Instruments

When measuring our financial instruments we use a market-based measurement, not an entity-specific measurement, and determine the fair value based on the assumptions that market participants would use in pricing the asset or liability. Fair value losses or gains are reported when identified.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

We use the valuation hierarchy for disclosure of the inputs to valuation used to measure fair value. This hierarchy prioritizes the inputs into three broad levels as follows.

Level 1 inputs utilize observable, quoted prices (unadjusted) in active markets for identical assets or liabilities that the Company has the ability to access. Financial assets and liabilities utilizing Level 1 inputs include actively traded equity securities.

Level 2 inputs are inputs other than quoted prices included within Level 1 that are observable for the asset or liability, either directly or indirectly. If the asset or liability has a specified (contractual) term, a Level 2 input must be observable for substantially the full term of the asset or liability. Level 2 inputs include the quoted prices for similar assets or liabilities in active markets, quoted prices for identical or similar assets or liabilities in markets that are not active, that is, markets in which there are few transactions for the asset or liability, the prices are not current, or price quotations vary substantially either over time or among market makers (for example, some brokered markets), or in which little information is released publicly (for example, a principal-to-principal market), inputs other than quoted prices that are observable for the asset or liability (for example, interest rates and yield curves observable at commonly quoted intervals, volatilities, prepayment speeds, loss severities, credit risks, and default rates) or inputs that are derived principally from or corroborated by observable market data by correlation or other means (market-corroborated inputs).

Level 3 inputs are unobservable inputs for the asset or liability. Unobservable inputs shall be used to measure fair value to the extent that observable inputs are not available, thereby allowing for situations in which there is little, if any, market activity for the asset or liability at the measurement date.

The following table provides information about the assets and liabilities measured at fair value on a recurring basis as of December 31, 2010 and 2011 and indicates the valuation technique utilized by the Company to determine the fair value.

 

     Total
Carrying
Value
     Quoted Prices
in Active
Markets

(Level 1)
     Significant
Other
Observable
Inputs
(Level 2)
     Significant
Unobservable
Inputs
(Level 3)
 
     (In millions)  

Cash equivalents at December 31, 2010

   $ 98.7       $ 98.7       $       $   

Cash equivalents at December 31, 2011

     166.0         166.0                   

Our cash equivalents consist of investments acquired with maturity dates of less than 90 days, are quoted from market rates and are classified within Level 1 of the valuation hierarchy. At December 31, 2010 and 2011, our cash equivalents consisted of funds held in U.S. Treasury money markets. The Company has not identified any Level 2 or Level 3 financial instruments as of December 31, 2010 and 2011.

The Company’s senior secured notes were traded on an active market through October 12, 2011, when they were paid in full. The fair value of the senior secured notes was based on quoted market rates. The Company entered into a senior secured facility on October 12, 2011. The Fair value of the senior secured facility was based upon trading activity among lenders.

 

     Carrying
Amount
     Estimated
Fair Value
 
     (In millions)  

Senior Secured Notes at December 31, 2010

   $ 346.1       $ 403.8   

Senior Secured Facility at December 31, 2011

     486.6         490.0   

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

Concentration of Credit Risk

The Company’s cash and cash equivalents and derivative instruments are maintained in or with various financial institutions. We have not experienced any losses in such accounts and believe we are not exposed to any significant credit risk in this area. For a discussion of our credit risk with significant customers see Notes 4 and 5.

New Accounting Pronouncements

In September 2011, the FASB issued authoritative guidance to allow entities to use a qualitative approach to test goodwill for impairment. This authoritative guidance permits an entity to first perform a qualitative assessment to determine whether it is more likely than not that the fair value of a reporting unit is less than its carrying value. If it is concluded that this is the case, it is necessary to perform the two-step goodwill impairment test. Otherwise, the two-step goodwill impairment test is not required. This guidance is effective for annual and interim goodwill impairment tests performed for fiscal years beginning after December 15, 2011 and earlier adoption is permitted. We do not expect the implementation of this authoritative guidance to have an impact on the Company’s financial position or results of operations.

In June 2011, the FASB issued authoritative guidance on the presentation of comprehensive income to require an entity to present the total of comprehensive income, the components of net income, and the components of other comprehensive income either in a single continuous statement of comprehensive income or in two separate but consecutive statements. This authoritative guidance eliminates the option to present the components of other comprehensive income as part of the statement of equity. This guidance is effective for the Company in the first quarter of fiscal 2012, with early adoption permitted, and should be applied retrospectively. The implementation of this authoritative guidance will only change the presentation of comprehensive income and will have no impact on the Company’s financial position or results of operations.

In May 2011, the FASB issued authoritative guidance to provide a consistent definition of fair value and ensure that the fair value measurement and disclosure requirements are similar between U.S. GAAP and International Financial Reporting Standards. This authoritative guidance limits the highest-and-best-use measure to nonfinancial assets, permits certain financial assets and liabilities with offsetting positions in market or counterparty credit risks to be measured at a net basis, and provides guidance on the applicability of premiums and discounts. This authoritative guidance also expands the disclosures on Level 3 inputs by requiring quantitative disclosure of the unobservable inputs and assumptions, as well as description of the valuation processes and the sensitivity of the fair value to changes in unobservable inputs. The new guidance will be effective for the Company in the first quarter of fiscal 2012. The implementation of this authoritative guidance is not expected to have a material impact on the Company’s financial position or results of operations.

In December 2010, the FASB amended its existing guidance for goodwill and other intangible assets. This authoritative guidance modifies Step 1 of the goodwill impairment test for reporting units with zero or negative carrying amounts. For those reporting units, an entity is required to perform Step 2 of the goodwill impairment test if there are qualitative factors indicating that it is more likely than not that a goodwill impairment exists. The qualitative factors are consistent with the existing guidance which requires goodwill of a reporting unit to be tested for impairment between annual tests if an event occurs or circumstances change that would more likely than not reduce the fair value of a reporting unit below its carrying amount. This authoritative guidance becomes effective for the Company in the first quarter fiscal 2012. The implementation of this authoritative guidance is not expected to have a material impact on the Company’s financial position or results of operations.

 

NOTE 3.

Revision of Previously Issued Financial Statements

In connection with the preparation of the Company’s consolidated financial statements for the year ended December 31, 2011, errors were identified primarily relating to the year ended December 31, 2010 and the first three quarters of the year ended December 31, 2011. These errors were primarily related to the Company’s

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

accounting for the Direct Access Program (“DAP”), as described below. The Company has assessed the impact of these errors on each period involved, in accordance with the SEC’s Staff Accounting Bulletin No. 99, “Materiality”, and has determined that the impact of the errors was not material, both individually and in the aggregate, to any previously issued financial statements. While the Company has also determined that the cumulative effect of correcting the errors in the fourth quarter of the year ended December 31, 2011 would not be material to the 2011 consolidated financial statements, the Company has elected to revise its previously issued financial statements to facilitate comparisons among periods. As part of its revision, the Company has determined to reverse immaterial out-of-period adjustments that were previously recorded in the Company’s 2011 quarterly periods and to reflect those adjustments as corrections to the periods in which the errors originated.

The following is a description of the nature of the errors as well as the impact of errors to the year ended December 31, 2010 (see Note 16 for the impact on the 2010 and 2011 quarterly financial information):

 

   

In three of the Company’s four current DAP customer contracts, the up-front payments contractually negotiated for each Facility were less than the actual third-party costs to manufacture each Facility. As each of the three Facilities was brought into service, it was the Company’s accounting policy to amortize both the deferred revenue and deferred contracts costs over the estimated customer relationship periods, which periods are consistent with the estimated remaining useful life of the satellite being accessed. However, the Company has concluded that this accounting policy was in error and that it should have been recognizing the deferred contract costs in excess of the deferred revenues (for each individual customer) over the related initial contract period. The impact of this error is an increase in cost of revenue of $1.5 million.

 

   

Certain costs for two DAP customers were previously netted against the related revenue. However, the Company concluded that this was an error as the Company acts as the principal in these arrangements. The cost and revenue should have been recorded on a gross basis, with the effect being an increase in both revenue and cost of revenue of $1.1 million.

 

   

The Company incorrectly capitalized interest related to the construction of its direct access facilities and other discrete projects. The impact of this error is an increase to interest expense of $0.8 million.

 

   

The Company previously recognized maintenance revenue for one DAP customer over a one-year period. However, the Company concluded that this was an error and that the revenue should have been recognized over the customer relationship period. The impact of this error is to reduce revenue by $0.5 million.

 

   

The Company incorrectly calculated certain DAP access minutes. The impact of this error is to reduce revenue by $0.3 million.

 

   

The Company has also corrected other immaterial errors including (i) over- or under-capitalization of certain internal and external costs, (ii) the accounting for stock compensation, including under capitalization of stock compensation for certain assets under construction, (iii) the effects of properly reconciling certain accrued liability accounts, and (iv) the classification of payments received for a sales type lease from operating to investing cash flows.

The following tables reflect the effect of correcting the errors on the Company’s consolidated financial statements as of and for the year ended December 31, 2010.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

Consolidated Income Statements

Revision

 

     For the Year Ended December 31, 2010  
     As
Previously
Reported
    Adjustment     Revised  
     (In millions, except per share data)  

Revenue

   $ 322.2      $ 0.3      $ 322.5   

Costs and expenses:

      

Cost of revenue, excluding depreciation and amortization

   $ 41.7      $ 2.5      $ 44.2   

Selling, general and administrative

     112.5        (0.3     112.2   

Depreciation and amortization

     118.9               118.9   
  

 

 

   

 

 

   

 

 

 

Income from operations

   $ 49.1      $ (1.9   $ 47.2   

Interest income (expense), net

     (39.6     (0.8     (40.4
  

 

 

   

 

 

   

 

 

 

Income before income taxes

     9.5        (2.7     6.8   

Income tax expense

     (5.4     1.1        (4.3
  

 

 

   

 

 

   

 

 

 

Net income

   $ 4.1      $ (1.6   $ 2.5   
  

 

 

   

 

 

   

 

 

 

Earnings per share:

      

Basic earnings per share

   $ 0.09      $ (0.04   $ 0.05   
  

 

 

   

 

 

   

 

 

 

Diluted earnings per share

   $ 0.09      $ (0.04   $ 0.05   
  

 

 

   

 

 

   

 

 

 

Weighted average common shares outstanding:

      

Basic

     45.7        45.7        45.7   
  

 

 

   

 

 

   

 

 

 

Diluted

     46.1        46.1        46.1   
  

 

 

   

 

 

   

 

 

 

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

Consolidated Balance Sheets

Revision

 

     As of December 31, 2010  
     As
Previously
Reported
    Adjustment     Revised  
     (In millions)  

ASSETS

      

CURRENT ASSETS:

      

Prepaid and current assets

   $ 19.4      $ 2.0      $ 21.4   
  

 

 

   

 

 

   

 

 

 

Total current assets

   $ 313.4      $ 2.0      $ 315.4   

Property and equipment, net of accumulated depreciation of $478.2

     879.1        (0.5     878.6   

Long-term deferred contract costs

     42.1        0.3        42.4   
  

 

 

   

 

 

   

 

 

 

Total assets

   $ 1,266.3      $ 1.8      $ 1,268.1   
  

 

 

   

 

 

   

 

 

 

LIABILITIES AND STOCKHOLDERS’ EQUITY

      

CURRENT LIABILITIES:

      

Other accrued liabilities

   $ 26.3      $ 0.9      $ 27.2   

Current portion of deferred revenue

     38.9        0.2        39.1   
  

 

 

   

 

 

   

 

 

 

Total current liabilities

   $ 86.4      $ 1.1      $ 87.5   

Long-term accrued liability

     6.0        2.7        8.7   

Deferred rev e nue

     246.2        0.5        246.7   

Long-term deferred tax liability, net

     76.7        (1.1     75.6   
  

 

 

   

 

 

   

 

 

 

Total liabilities

   $ 766.0      $ 3.2      $ 769.2   
  

 

 

   

 

 

   

 

 

 

COMMITMENTS AND CONTINGENCIES

      

STOCKHOLDERS’ EQUITY

      

Additional paid-in capital

   $ 512.7      $ 0.2      $ 512.9   

Accumulated deficit

     (11.9     (1.6     (13.5
  

 

 

   

 

 

   

 

 

 

Total stockholders’ equity

     500.3        (1.4     498.9   
  

 

 

   

 

 

   

 

 

 

Total liabilities and stockholders’ equity

   $ 1,266.3      $ 1.8      $ 1,268.1   
  

 

 

   

 

 

   

 

 

 

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

Consolidated Statements of Cash Flows

Revision

 

     For the Year Ended December 31, 2010  
     As
Previously
Reported
    Adjustment     Revised  
     (In millions)  

CASH FLOWS FROM OPERATING ACTIVITIES:

      

Net income

   $ 4.1      $ (1.6   $ 2.5   

Adjustments to reconcile net income to net cash provided by operating activities:

      

Amortization of aerial image library, deferred contract costs and lease incentive

     7.1        1.6        8.7   

Non-cash stock compensation expense

     6.8        (0.2     6.6   

Deferred income taxes

     4.4        (1.1     3.3   

Changes in working capital, net of investing activities:

      

Accrued liabilities

     10.6        3.7        14.3   

Deferred contract costs

     (14.2     (3.8     (18.0

Deferred revenue

     13.4        (2.8     10.6   
  

 

 

   

 

 

   

 

 

 

Net cash flows provided by operating activities

     157.5        (4.2     153.3   
  

 

 

   

 

 

   

 

 

 

CASH FLOWS FROM INVESTING ACTIVITIES:

      

Construction in progress additions

     (78.3     4.2        (74.1
  

 

 

   

 

 

   

 

 

 

Net cash flows used in investing activities

   $ (85.1   $ 4.2      $ (80.9
  

 

 

   

 

 

   

 

 

 

 

NOTE 4.

Significant Customers

In September 2003, we entered into the NextView agreement with NGA under which we agreed to provide a minimum of $531.0 million of imagery products and services from our WorldView-1 satellite. Of this amount, $266.0 million was received between September 2003 and November 2007, the month WorldView-1 became operational. The $266.0 million was used to offset the construction costs of WorldView-1, and was recorded as deferred revenue when received. When WorldView-1 reached full operational capacity (FOC) in November 2007, we began recognizing the deferred revenue on a straight line basis over the estimated useful life of WorldView-1. Based on the current estimated useful life of WorldView-1, we recognized $25.5 million of revenue related to the pre-FOC payments for each of the years ended December 31, 2010 and 2011.

On August 6, 2010, we entered into the EnhancedView contract with NGA. The SLA portion of the EnhancedView contract (Enhanced View SLA) became effective on September 1, 2010, commencing upon the expiration of the NextView SLA. The EnhancedView contract has a ten year term, inclusive of nine one-year options exercisable by NGA, and is subject to Congressional appropriations and the right of NGA to terminate or suspend the contract at any time.

The EnhancedView SLA portion of the award is $2.8 billion over the term of the contract; $250.0 million annually, or $20.8 million per month, for the first four contract years, commencing September 1, 2010, with an increase to $300.0 million annually, or $25.0 million per month, for the remaining six years of the contract term. The award also provides for up to $750.0 million for value added products, infrastructure enhancements and other services, including the option for NGA to require us to lower the altitude of WorldView-2 to an altitude of 496 km at any time after September 1, 2013. DigitalGlobe will be required to meet certain service level requirements related to the operational performance of the satellites comprising the WorldView constellation and related ground systems. To support requirements under this agreement, we have begun the procurement and construction of our next satellite, WorldView-3 as well as certain other infrastructure improvements.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

We recognize revenue for the $2.8 billion in services to be provided under the EnhancedView SLA using a proportional performance method based upon the percentage of capacity of our constellation made available to NGA compared to the total capacity to be provided over the life of the contract. The contract requires the Company to increase capacity of the constellation through the installation of seven additional remote ground terminals above the number the Company operated prior to the EnhancedView contract, which communicate directly with our satellites, as well as the addition of a new satellite, WorldView-3. As capacity is added to our constellation, and as contractually agreed to by NGA, we recognize revenue in direct proportion to the amount of incremental capacity that is made available to NGA. For the year ended December 31, 2011, we recognized approximately $157.0 million of revenue and we recorded $94.6 million of deferred revenue related to the EnhancedView SLA contract. As of December 31, 2011, there was $119.4 million in total deferred revenue from the inception of the EnhancedView SLA.

Under the EnhancedView SLA, and assuming all option years under the agreement are exercised and funded, we will receive a monthly non-refundable cash payment of approximately $20.8 million from NGA during the first four years of the EnhancedView contract, with an increase to $25.0 million per month in years five through ten. Each month is subject to a holdback, up to 10% of the monthly payment, depending upon the Company’s performance against pre-defined criteria. If NGA certifies that we have performed all requirements in the agreement each month, no holdback will be applied to that month. If funds are held back, the Company retains the cash. The retained cash, however, can be applied to future products and services or will fund a pro-rated extension beyond the current contract period. Accordingly, all amounts held back will cause the Company to defer recognition of a corresponding revenue amount until such additional products or services have been provided. During the year ended December 31, 2011, there was $0.2 million of holdback, all of which has been applied to other products and recognized as revenue as of December 31, 2011.

On July 25, 2011, NGA provided the Company with an Amendment of Solicitation/Modification of Contract (the Amendment) to the EnhancedView contract. The Amendment exercises the first option under the EnhancedView SLA to extend the EnhancedView SLA for the period of September 1, 2011 through August 31, 2012.

 

NOTE 5.

Information on Segments and Major Customers

We conduct our business through two segments: (i) defense and intelligence and (ii) commercial. Our imagery products and services consist of imagery that we process to varying levels according to the customer’s specifications. Customers can purchase satellite or aerial images that are archived in our ImageLibrary. Customers can also order imagery content by placing custom orders, which require tasking of our satellites, for a specific area of interest, or as a bundle of imagery and data for a region or type of location, such as cities, ports and harbors or airports.

We have organized our business around the defense and intelligence and commercial segments because we believe that customers in these two groups are functionally and identifiably similar in terms of their purchasing habits. We deliver our products and services using the distribution method that best suits our customers’ needs.

The vast majority of the dollar value of our fixed assets are the satellites and the ground based production and support facilities that are common to all segments. There are no significant identifiable assets specifically dedicated to either segment.

Only those costs directly associated with the two segments are shown in cost of revenue and selling, general and administrative expenses in those segments. All expenses which are common to both segments and/or represent corporate operating costs are included in the unallocated cost section. Substantially all of the Company’s assets are located in the United States.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

 

     Year Ended December 31,  
   2009     2010
Revised
    2011  
     (In millions)  

Defense and Intelligence

      

Revenue

   $ 231.0      $ 252.4      $ 261.4   

Cost of revenue, excluding depreciation and amortization

     5.7        13.5        20.7   

Selling, general and administrative

     11.8        11.8        10.2   
  

 

 

   

 

 

   

 

 

 

Segment results of operations

   $ 213.5      $ 227.1        230.5   
  

 

 

   

 

 

   

 

 

 

Commercial

      

Revenue

   $ 50.9      $ 70.1        78.1   

Cost of revenue, excluding depreciation and amortization

     7.8        6.6        4.9   

Selling, general and administrative

     10.6        15.2        20.5   
  

 

 

   

 

 

   

 

 

 

Segment results of operations

   $ 32.5      $ 48.3      $ 52.7   
  

 

 

   

 

 

   

 

 

 

Unallocated common costs

      

Cost of revenue, excluding depreciation and amortization

     17.6        24.1        39.3   

Selling, general and administrative

     66.2        85.2        99.5   

Depreciation and amortization

     74.4        118.9        117.1   
  

 

 

   

 

 

   

 

 

 

Unallocated costs

   $ 158.2      $ 228.2        255.9   
  

 

 

   

 

 

   

 

 

 

Income from operations

     87.8        47.2        27.3   

Loss from early extinguishment of debt

     (7.7     —          (51.8

Loss on derivative instruments

     (1.8     —          —     

Other income (expense), net

     —          —          0.2   

Interest income (expense), net

     0.1        (40.4     (21.7
  

 

 

   

 

 

   

 

 

 

Income before income taxes

   $ 78.4      $ 6.8      $ (46.0
  

 

 

   

 

 

   

 

 

 

Total U.S. and foreign sales were as follows:

 

     Year Ended December 31,  

Revenue

   2009      2010
Revised
     2011  
     (In millions)  

U.S.

   $ 232.7       $ 227.8       $ 228.3   

Foreign

     49.2         94.7         111.2   
  

 

 

    

 

 

    

 

 

 

Total

   $ 281.9       $ 322.5       $ 339.5   
  

 

 

    

 

 

    

 

 

 

Revenue percentages from all customers whose revenue exceeded 10% of the total company revenue were as follows:

 

     Year Ended December 31,  

Customer

   2009       2010  
Revised
    2011  

NGA

     75.0     62.1     60.1

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

Percentages of accounts receivable (net of allowance for doubtful accounts) for all customers whose receivable exceeded 10% of the net accounts receivable as of:

 

     December 31,  

Customer

   2009     2010     2011  

NGA

     61.8     34.9     30.5

 

NOTE 6.

Property and Equipment

Property and equipment consisted of the following as of:

 

     Year ended December 31,  
     2010
Revised
    2011  
     (In millions)  

Construction in progress

   $ 79.3      $ 305.9   

Computer equipment and software

     126.3        127.1   

Machinery and equipment

     25.8        24.5   

Furniture and fixtures

     14.6        15.1   

Land and land improvements

     —          0.3   

WorldView-2 satellite

     463.2        463.2   

WorldView-1 satellite

     473.2        473.2   

QuickBird satellite

     174.4        174.4   
  

 

 

   

 

 

 

Total property and equipment

   $ 1,356.8      $ 1,583.7   
  

 

 

   

 

 

 

Accumulated depreciation and amortization

     (478.2     (563.9
  

 

 

   

 

 

 

Property and equipment, net

   $ 878.6        1,019.8   
  

 

 

   

 

 

 

Construction in progress includes our WorldView-3 satellite, ground station construction, infrastructure projects, certain internally developed software costs and capitalized interest. Depreciation expense for property and equipment was $72.6 million, $117.4 million and $116.9 million for the year ended December 31, 2009, 2010 and 2011, respectively.

The capitalized costs of our satellites and related ground systems include internal and external direct labor costs, internally developed software and direct material costs which support the construction and development of our satellites, and related ground systems. The cost of our satellites also includes capitalized interest incurred during the construction, development and initial in-orbit testing period. The portion of the launch insurance premium allocable to the period from launch through in-orbit calibration and commissioning has been capitalized as part of the cost of the satellites and is amortized over the useful life of the satellites.

Following each satellite launch, and at least annually thereafter, we review the expected operational life of our satellites. We determine a satellite’s expected operational life by considering certain factors including: (i) the probabilities of failure of the satellite’s components from design or manufacturing defects, (ii) environmental stresses or other causes, (iii) the quality of construction, (iv) the supply of fuel, (v) the expected gradual environmental degradation of solar panels and other components, (vi) projected levels of solar radiation, (vii) the durability of various satellite components, and (viii) the orbits in which the satellites are placed.

We have generally aligned the annual assessment of the useful life of the operating satellites with the timing of our insurance renewals in the second half of the calendar year, and we perform the annual assessment of the useful life of the QuickBird, WorldView-1 and WorldView-2 satellites in the second half of the calendar year or when events or circumstances dictate that a reevaluation of the useful life should be done at an earlier date. An adjustment will be made to the estimated depreciable life of the satellite if deemed necessary by the assessment

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

performed. Changes to the estimated useful life of our satellites and related impact on the depreciation expense will be accounted for on a prospective basis as of the date of the change.

As a result of our annual assessment during the third quarter of 2009, we extended the estimated useful life of our QuickBird satellite, which resulted in a change in the depreciation expense associated with the QuickBird satellite on a prospective basis beginning July 1, 2009. For the year ended December 31, 2009, this change resulted in reduced depreciation expense and a corresponding increase in income from continuing operations of $2.9 million, an increase in net income of $1.7 million and had a $0.04 impact on diluted earnings per share.

Commencing on March 21, 2011, the Company initiated an increase in the altitude of the QuickBird satellite. The change in altitude was completed April 7, 2011, and resulted in an increase in the anticipated useful life of the QuickBird satellite by approximately 17 months through the third quarter of 2013. There will be no material change to the products and solutions DigitalGlobe is able to produce using the QuickBird satellite. For the year ended December 31, 2011, this change resulted in reduced depreciation expense and a corresponding decrease in loss before income taxes of $2.2 million, a decrease in net loss of $1.3 million and had a $0.03 impact on diluted earnings per share.

 

NOTE 7.

Goodwill and Intangibles

Intangible assets generally consist of customer relationships, non-compete agreements, trademarks and core technology. The identifiable intangible assets are being amortized on a straight-line basis over their useful lives, ranging from three to five years, except for customer relationships, which are being amortized using a declining balance method over their estimated life of five years. Goodwill is not being amortized for financial statement purposes, but is deductible for income tax purposes.

Amortization expense for intangibles was $1.8 million, $1.5 million and $0.2 million for the years ended December 31, 2009, 2010, and 2011, respectively. These intangible assets have become fully amortized in 2011. The goodwill balance as of December 31, 2010 and 2011 was $8.7 million and is included in our commercial segment. The Company has not recorded an impairment of goodwill for any of the periods presented.

 

NOTE 8.

Other Accrued Liabilities

 

     At December 31,  
     2010
Revised
     2011  
     (In millions)  

Compensation and other employee benefits

   $ 11.0       $ 10.3   

Accrued taxes

     2.1         0.8   

Accrued expense

     5.4         8.2   

Construction in progress accruals

     1.0         10.7   

Other

     7.7         7.5   
  

 

 

    

 

 

 

Total other accrued liabilities

   $ 27.2       $ 37.5   
  

 

 

    

 

 

 

Compensation and other employee benefits include accrued bonus expense and vacation accrual. Accrued expense primarily represents the current portion of payments to third parties for work performed on our direct access facilities. Construction in progress accruals include amounts due for milestone payments due on the procurement and construction of our WorldView-3 satellite. Other accruals consist of third party commission expense, professional fees and the current portion of deferred lease incentives.

Long-term accrued liabilities consist of future payments related to the construction of a direct access facility.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

NOTE 9.

Debt

Senior Secured Credit Facility

On October 12, 2011, the Company entered into a $500.0 million, seven-year senior secured term loan facility and a $100.0 million, five-year senior secured revolving credit facility, the terms of which are set forth in a Credit and Guaranty Agreement dated as of October 12, 2011 among the Company, the guarantors party thereto, the lenders named therein and J.P. Morgan Chase Bank, N.A., as administrative agent and as collateral agent (the “Credit Agreement”). The Company has borrowed the full amount of the term loan facility to fund its cash tender offer to purchase all of its senior secured notes. The Company received net cash proceeds from the term loan facility of $66.0 million following the payment of $410.9 million for the tender of the senior secured notes, $11.8 million in underwriting and other fees and expenses incurred in connection with the Credit Agreement and net of the term loan issuance discount of $12.5 million. The Company paid $1.2 million in fees related to the tender offer. The company recorded a loss of $51.8 million during the fourth quarter of 2011. As a result of the tender offer, 100% of all bonds were tendered and retired by the Company. The Company will use the remaining cash proceeds for general corporate purposes, which may include acquisitions and share repurchases. As of the date of this filing, the revolving credit facility remains undrawn.

The obligations of the Company under the credit facility are guaranteed by certain of the Company’s domestic subsidiaries and are secured by substantially all of the assets of the Company and the guarantors, subject to certain exceptions. Assets collateralizing the senior secured notes had a net book value of $1,434.1 million as of December 31, 2011. The Credit Agreement contains affirmative and negative covenants that the Company believes are usual and customary for a senior secured credit agreement. The negative covenants include, among other things, limitations on asset sales, mergers and acquisitions, indebtedness, liens, dividends, investments and transactions with the Company’s affiliates. The Credit Agreement also requires the Company to comply with a maximum leverage ratio and minimum interest coverage ratio. As of December 31, 2011 the Company is in compliance with our debt covenants.

Borrowings under the Credit Agreement will bear interest, at the Company’s option, at a rate equal to either an adjusted LIBOR rate or a base rate, in each case plus the applicable margin. The applicable margin for borrowings under the term loan facility is 4.50% for adjusted LIBOR loans or 3.50% for base rate loans. The applicable margin for borrowings under the revolving credit facility may change depending on the Company’s leverage ratio, up to a maximum of 4.50%. The term loan facility current bears interest based upon the LIBOR-based rate. The Company will also pay a commitment fee of between 37.5 to 50.0 basis points, payable quarterly, on the average daily unused amount of the revolving credit facility based on the Company’s leverage ratio.

Interest expense, accretion of debt discount and amortization of the deferred financing fees for the year ended December 31, 2011 were $35.6 million, $3.2 million and $1.9 million, respectively, of which $18.8 million was capitalized to assets under construction. Interest expense, accretion of debt discount and amortization of the deferred financing fees for the year ended December 31, 2010 were $37.3 million, $2.6 million and $2.0 million, respectively, of which $2.8 million was capitalized to assets under construction. Total interest incurred, accretion of debt discount and amortization of the deferred financing fees for the year ended December 31, 2009 were $34.8 million, $1.7 million and $1.3 million, respectively. All amounts were capitalized in 2009 to our WorldView-2 satellite.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

The following table represents our future debt payments as of December 31, 2011:

 

     Long Term Debt
(Excluding  Interest
Payments)
 
     (In millions)  

2012

   $ 5.0   

2013

     5.0   

2014

     5.0   

2015

     5.0   

2016

     5.0   

Thereafter

     475.0   
  

 

 

 

Total

   $ 500.0   
  

 

 

 

Senior Secured Notes

We issued $355.0 million principal amount of our senior secured notes in April 2009, net of the issuance discount of $13.2 million and paid fees and expenses of $10.2 million, which were recorded in deferred financing costs. As of December 31, 2010, the senior secured notes had a carrying value of $346.1 million. The Company had the right to call the senior secured notes at a predetermined price beginning on May 1, 2012. The senior secured notes were guaranteed by certain of our subsidiaries and secured by nearly all of our assets, including the shares of capital stock of certain of our subsidiaries, and the QuickBird, WorldView-1 and WorldView-2 satellites. Assets collateralizing the senior secured notes had a net book value of $1,246.0 million as of December 31, 2010.

In May 2010, the Company offered to exchange up to $355.0 million aggregate principal amount of the senior secured notes for notes that have been registered under the Securities Act of 1933, as amended (the Securities Act). The terms of the registered notes were the same as the terms of the original notes, except that the notes were registered under the Securities Act and the transfer restrictions, registration rights and additional interest provisions are not applicable to the registered notes. The Company has accepted the exchange of $355.0 million aggregate principal amount of the senior secured notes that were properly tendered.

On October 12, 2011 the Company entered into a new senior secured facility and has subsequently paid the full obligation under the senior secured notes and recorded a loss on extinguishment of $51.8 million.

Prior to 2010, we had outstanding a $230.0 million senior credit facility and $40.0 million of senior subordinated notes. With the issuance of our senior secured notes on April 28, 2009, the senior credit facility and the senior subordinated notes and accrued interest were paid in full.

As a result of the issuance of our senior secured notes during the second quarter of 2009, we recorded an early extinguishment of debt representing the expensing of the deferred financing costs of $5.9 million related to the senior credit facility and senior subordinated notes, and a prepayment penalty of $1.8 million related to the senior subordinated notes.

The Company had an interest rate swap agreement associated with the senior secured notes that original qualified as a cash flow hedge. As a result of an amendment to the senior credit facility in 2009, the swap became ineffective and no longer qualified as a cash flow hedge. The fair value changes of this derivative instrument were recorded in the Consolidated Statements of Operations. As a result of the payoff of the senior credit facility in 2009, the swap was no longer required and therefore was terminated.

Letters of Credit

At December 31, 2010 and 2011, we had $1.2 million of restricted cash under the lease agreement for our headquarters in Longmont, Colorado. At December 31, 2010 and 2011, we had $19.1 million and $16.3 million,

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

respectively, in letters of credit and performance guarantees used in the ordinary course of business to support advanced payments from customers under certain of our DAP contracts. These letters of credit are secured by restricted cash that has been recorded in our financial statements. The letters of credit, and related restricted cash amounts are released when the respective contractual obligations have been fulfilled by the Company.

 

NOTE 10.

Stockholders’ Equity and Other Comprehensive Income (Loss)

On May 14, 2009, the Company completed an IPO consisting of 14.7 million shares of common stock at $19.00 per share. The offering included 13.3 million shares sold by selling stockholders and 1.4 million shares sold by the Company. On September 15, 2010, the Company priced a secondary offering of shares of common stock at $30.25 per share. The Company did not receive proceeds from the sale of the shares of its common stock in the secondary offering, therefore we expensed the $0.4 million of the costs associated with the offering. At December 31, 2011, the Company has 250.0 million authorized shares of common stock. At December 31, 2011, 46.4 million shares of common stock were issued and outstanding.

Treasury Stock

There were no open market repurchases of our common stock during 2010 and 2011. During 2011, certain participants elected to have the Company withhold 22,136 shares to pay for minimum taxes due, in accordance with the 2007 Employee Stock Option Plan, at the time their restricted stock vested. Such shares have been included in treasury shares.

Other Comprehensive Income (Loss)

Other comprehensive income (loss) include the effect of realized and unrealized gains and losses on derivative instruments receiving cash flow hedge accounting treatment during the year ended December 31, 2009. With the expiration and settlement of our financial derivatives the amounts recorded in accumulated other comprehensive earnings (loss) were capitalized to the cost of the WorldView-2 satellite as of December 31, 2009. For December 31, 2010 and December 31, 2011 we have no other comprehensive income (loss) items therefore our net income (loss) is the same as our other comprehensive income (loss).

Stock-Based Compensation Programs

On February 15, 2000, the board of directors approved the 1999 Equity Incentive Plan (the 1999 Plan) pursuant to which qualified and nonqualified stock options to purchase shares of the Company’s common stock may be granted to employees, officers, directors, and consultants. Options granted pursuant to the 1999 Plan are subject to certain terms and conditions as contained in the 1999 Plan, have a ten-year term, generally vest ratably over a four-year period.

On February 15, 2007, the board of directors approved the 2007 Employee Stock Option Plan (the 2007 Plan), pursuant to which the following awards may be granted to employees, officers, directors, and consultants: qualified and nonqualified stock options to purchase shares of the Company’s common stock, restricted stock, unrestricted shares, stock appreciation rights and shares of the stock itself. Options granted pursuant to the 2007 Plan are subject to certain terms and conditions as contained in the 2007 Plan, have a ten-year term and generally vest over a four-year period. The Company amended this plan in 2008 to extend the exercise period of terminated employees from thirty days to ninety days. The number of shares available for grant at December 31, 2010 and 2011 was 1,787,337 and 953,668, respectively.

The Company has equity incentive plans that provide for the grant to employees of stock-based compensation. To date, issued equity awards have consisted of stock options, restricted stock and unrestricted shares. The date of grant of the awards is used as the measurement date. The awards are valued as of the measurement date and are amortized on a straight-line basis over the requisite vesting period.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

A summary of stock option activity for the year ended December 31, 2009, 2010 and 2011 is presented below:

 

     Options Outstanding  
     Number of
Shares
     Weighted-
Average
Exercise Price
     Weighted
Average
Remaining
Contractual Term
(In Years)
     Aggregate
Intrinsic
Value
(In Millions)(1)
 

Outstanding — December 31, 2008

     2,758,284       $ 19.10         7.75       $ 8.6   
  

 

 

    

 

 

    

 

 

    

 

 

 

Granted

     942,459         20.64         

Exercised

     248,377         6.93         

Forfeited/Expired

     254,952         19.88         
  

 

 

    

 

 

    

 

 

    

 

 

 

Outstanding — December 31, 2009

     3,197,414       $ 20.29         7.38       $ 14.8   

Granted

     666,608         27.02         

Exercised

     683,605         15.02         

Forfeited/Expired

     188,567         23.13         
  

 

 

    

 

 

    

 

 

    

 

 

 

Outstanding — December 31, 2010

     2,991,850       $ 22.96         7.65       $ 22.8   

Granted

     727,290         25.97         

Exercised

     87,521         20.68         

Forfeited/Expired

     135,419         27.14         
  

 

 

    

 

 

    

 

 

    

 

 

 

Outstanding — December 31, 2011

     3,496,200       $ 23.49         7.11       $ 0.3   

Expected to Vest — December 31, 2011

     3,426,276         23.49         7.11           

Exercisable — December 31, 2009

     1,945,332       $ 19.10         6.42       $ 11.3   

Exercisable — December 31, 2010

     1,786,744       $ 21.72         6.92       $ 17.9   

Exercisable — December 31, 2011

     2,182,865       $ 22.34         6.23       $ 0.1   

 

(1)

Represents the total pretax intrinsic value for stock options with an exercise price less than the Company’s calculated common stock price as of December 31, 2009, 2010 and 2011, respectively that option holders would have realized had they exercised their options as of that date.

Weighted-average grant-date fair values for option awards granted was $10.44, $13.45 and $12.28 for the years ended December 31, 2009, 2010 and 2011, respectively. The total fair value of options vested for the years ended December 31, 2009, 2010 and 2011 was $7.2 million, $5.9 million and $12.5 million, respectively.

The Company recognized stock-based compensation during the year ended December 31, 2009, 2010 and 2011 of $7.7 million, $6.9 million and $15.3 million, respectively, of which $0.5 million, $0.3 million and $0.9 million was capitalized to assets under construction for the year ended December 31, 2009, December 31, 2010 and December 31, 2011, respectively.

On April 4, 2011, Ms. Jill D. Smith, former Chief Executive Officer of the Company, terminated her employment relationship with the Company. The provisions in Ms. Smith’s Amended and Restated Employment agreement provided for a modification in the option and stock awards that she previously received. This modification included continued vesting of her equity awards through the two year term of her non-compete agreement and included an extension of the exercise period for her options to 90 days following the expiration of her non-compete agreement with the Company. This modification resulted in a $5.1 million non-cash charge to stock compensation expense during the second quarter of 2011.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

The fair value of each option grant was estimated on the date of grant using the Black-Scholes option-pricing model with the following assumptions:

 

     2009     2010     2011  

Expected dividend yield

     0.0     0.0     0.0

Expected stock price volatility

     56.6 – 59.0     55.6 – 56.7     49.3 – 51.1

Risk-free interest rate

     1.8 – 2.4     1.2 – 2.3     0.9 –1.9

Expected life of options (years)

     5.0       5.0       5.0  

Expected volatility is based on a weighted average of a variety of comparable companies within our industry and our own volatility covering a look back period of five years. The expected life and forfeiture rate 2.0% are based on the Company’s historical experience. The risk-free rate is based on the five-year Treasury note rate.

The total pre-tax intrinsic value or the difference between the exercise price and the market price on the date of exercise, of stock options exercised during the year ended December 31, 2009, 2010 and 2011 was $4.1 million, $7.6 million and $0.5 million, respectively.

As of December 31, 2010 and 2011 there was a total of $12.8 million and $13.2 million, respectively, of unrecognized expense remaining to be recognized over a weighted average period of 2.8 and 2.2 years, respectively.

On November 3, 2008, the Company granted a total of 30,000 shares of restricted stock under the 2007 Plan to executives as part of the Long Term Incentive Plan (LTIP) with a fair value of $22.10 per share. All units granted vest one-third each year beginning on March 31, 2009. Upon vesting units are converted into shares of common stock. As of December 31, 2010 and December 31, 2011, 20,000 and 30,000, respectively units had vested.

During 2010 and 2011, the Company awarded 47,711 and 226,312 shares, respectively, of restricted stock to certain employees, which will vest over four years and 24,069 and 24,538 unrestricted shares, respectively, to independent members of our board of directors pursuant to applicable compensation plans which vest immediately on the date of grant. During the fourth quarter of 2010, the Company awarded 164,243 shares of restricted stock to certain executives which will vest over two years. A summary of restricted stock activity for the years ended December 31, 2009, 2010 and 2011 is shown below:

 

Restricted Stock Awards

   No. of
Shares
     Weighted
Average Grant

Date  Fair Value
 

Non-vested at December 31, 2008

     30,000       $ 22.10   

Granted

               

Forfeited

               

Vested

     10,000           
  

 

 

    

 

 

 

Non-vested at December 31, 2009

     20,000       $ 22.10   

Granted

     236,023         30.53   

Forfeited

     4,094           

Vested

     34,069         26.90   
  

 

 

    

 

 

 

Non-vested at December 31, 2010

     217,860       $ 30.45   

Granted

     250,850         25.48   

Forfeited

     2,531         31.54   

Vested

     94,402         28.61   
  

 

 

    

 

 

 

Non-vested at December 31, 2011

     371,777       $ 27.55   
  

 

 

    

 

 

 

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

As of December 31, 2010 and 2011, there was $5.9 million and $6.3 million, respectively, of total unrecognized compensation cost related to the non-vested share-based compensation arrangements. That cost is expected to be recognized over a weighted average period of 1.9 and 2.7 years, respectively.

 

NOTE 11.

Earnings Per Share

Basic earnings (loss) per share (EPS) is computed by dividing net income (loss) available to common stockholders by the weighted average number of common shares outstanding for the period excluding issued, but unvested, restricted shares. Diluted EPS is computed by dividing net income (loss) by the weighted average number of common shares outstanding and dilutive potential common shares for the period. The Company includes as potential common shares the weighted average dilutive effects of outstanding stock options and restricted shares using the treasury stock method.

The following table sets forth the number of weighted average shares used to compute basic and diluted EPS:

 

     Years Ended December 31,  
     2009      2010
Revised
     2011  
     (In millions, except
per share data)
 

Earnings (loss) per share:

        

Net income (loss)

   $ 47.4       $ 2.5       $ (28.1
  

 

 

    

 

 

    

 

 

 

Basic weighted average number of common shares outstanding

     44.2         45.7         45.9   

Assuming exercise of stock options and restricted shares

     0.7         0.4           
  

 

 

    

 

 

    

 

 

 

Diluted weighted average number of common shares outstanding

     44.9         46.1         45.9   
  

 

 

    

 

 

    

 

 

 

Earnings (loss) per share:

        

Basic

   $ 1.07       $ 0.05       $ (0.61
  

 

 

    

 

 

    

 

 

 

Diluted

   $ 1.06       $ 0.05       $ (0.61
  

 

 

    

 

 

    

 

 

 

The number of options and nonvested restricted stock awards that were excluded from the computation of diluted EPS, because the effects thereof were anti-dilutive were 2.3 million, 0.1 million and 3.9 million for the years ended December 31, 2009, 2010 and 2011, respectively.

 

NOTE 12.

Income Taxes

Accounting for income taxes requires deferred tax assets and liabilities to be recognized for temporary differences between the tax basis and financial reporting basis of assets and liabilities, computed at the expected tax rates for the periods in which the assets or liabilities will be realized, as well as for the expected tax benefit of net operating loss and tax credit carryforwards.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

The benefit (provisions) for income taxes reflected in the statements of operations for the years ended December 31, 2009, 2010 and 2011 consisted of:

 

     2009     2010
Revised
    2011  
     (In millions)  

Current:

      

Federal

   $ 2.7      $ (0.1   $   

State

     (0.1            1.2   

Foreign

            (0.9     (1.8
  

 

 

   

 

 

   

 

 

 

Total current

     2.6        (1.0     (0.6
  

 

 

   

 

 

   

 

 

 

Deferred:

      

Federal

     (31.4     (2.8     18.3   

State

     (2.2     (0.5     0.2   

Foreign

                     
  

 

 

   

 

 

   

 

 

 

Total deferred

     (33.6     (3.3     18.5   
  

 

 

   

 

 

   

 

 

 

Income tax (expense) benefit

   $ (31.0   $ (4.3   $ 17.9   
  

 

 

   

 

 

   

 

 

 

The Company’s deferred tax assets and liabilities consisted of the following as of December 31:

 

     2010
Revised
    2011  
     (In millions)  

Deferred tax assets:

    

Current

    

Other

   $ 0.7      $ 1.6   

Compensation accrual

     1.2        5.1   

Net operating loss carryforwards

     60.8        58.4   
  

 

 

   

 

 

 

Total current deferred tax asset

     62.7        65.1   
  

 

 

   

 

 

 

Long-term deferred tax assets (liabilities), net

    

Net operating loss carryforwards

     38.6        39.2   

Research and development tax credits

     9.0        11.2   

Deferred revenue

     74.4        79.9   

Other assets

     4.1        7.5   

Fixed assets

     (201.7     (197.4
  

 

 

   

 

 

 

Total long-term deferred tax (liabilities), net

     (75.6     (59.6
  

 

 

   

 

 

 

Net deferred tax (liability) asset

   $ (12.9   $ 5.5   
  

 

 

   

 

 

 

At December 31, 2011, the Company had net operating loss (NOL) carryforwards for federal and state income tax purposes of approximately $264.5 million and $245.9 million, respectively. Included in this NOL, is approximately $6.4 million attributable to tax deductions related to equity compensation in excess of compensation recognized for financial reporting. In addition, the Company has research and development tax credits of approximately $11.2 million, which may be available to offset future federal income tax liabilities. If unused, the Federal carryforwards and credits will begin to expire during the years 2019 to 2031. If unused, the state carryforwards and credits will begin to expire during the years 2019 to 2031. The Internal Revenue Code places certain limitations on the annual amount of net operating loss carryforwards, which can be utilized if certain changes in the Company’s ownership occur. Included in the Company’s federal net operating loss carryforward is $16.4 million that is subject to a $2.0 million annual IRC 382 limitation, which is expected to be fully utilized in future periods.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

The benefit (expense) for income taxes differs from the amount computed by applying the U.S. federal income tax rate of 35% to income or loss before income taxes as follows:

 

     2009     2010
Revised
    2011  
     (In millions)  

Federal income tax (expense) benefit

   $ (27.4   $ (2.4   $ 16.1   

Non-deductible stock-based compensation

     (0.9     (0.7     (1.4

State income tax expense, net of federal impact

     (2.4     (0.3     1.4   

Stock-based compensation shortfalls

            (0.5     (0.2

Research and Experimentation Tax Credit

                   2.2   

Other

     (0.3     (0.4     (0.2
  

 

 

   

 

 

   

 

 

 

Income tax (expense) benefit

   $ (31.0   $ (4.3   $ 17.9   
  

 

 

   

 

 

   

 

 

 

The tax years 1996 through 2011 remain open to examination by the United States taxing jurisdictions to which we are subject. The Company recognizes accrued interest and penalties related to uncertain tax positions as a component of tax expense. The Company did not have any accrued interest or penalties recorded at December 31, 2011. The Company does not anticipate a material change to the amount of uncertain tax positions within the next 12 months. If any of the uncertain tax positions were recognized it would affect the effective tax rate.

A reconciliation of the Company’s uncertain tax positions is as follows:

 

     2009      2010      2011  
     (In millions)  

Balance as of January 1

   $ 4.5       $ 4.5       $ 4.5   

Current year addition

                     0.9   
  

 

 

    

 

 

    

 

 

 

Balance as of December 31

   $ 4.5       $ 4.5       $ 5.4   
  

 

 

    

 

 

    

 

 

 

While management believes the Company has adequately provided for all tax positions, amounts asserted by taxing authorities could materially differ from our accrued positions as a result of uncertain and complex application of tax regulations. Additionally, the recognition and measurement of certain tax benefits includes estimates and judgment by management and inherently includes subjectivity. Accordingly, additional provisions on tax-related matters could be recorded in the future as revised estimates are made or the underlying matters are settled or otherwise resolved.

 

NOTE 13.

Benefit Plan

In October 1995, we adopted a 401(k) Savings and Retirement Plan (the 401(k) Plan), a tax-qualified plan covering substantially all of the Company’s employees. Employees may elect to contribute, subject to certain limitations, up to 60% of their annual compensation to the 401(k) plan. The 401(k) Plan provides that we may contribute matching contributions to the 401(k) Plan at the discretion of the Company’s management as approved by the board of directors. We recorded approximately $1.5 million, $1.6 million and $2.0 million of matching contribution expense for the years December 31, 2009, 2010 and 2011, respectively.

 

NOTE 14.

Related Party Transactions

Prior to the Company’s IPO in May 2009, the Company had several related party relationships with vendors and customers due to their ownership of the Company’s stock. As a result of the IPO, the Company re-evaluated its related party relationships and concluded that Morgan Stanley and Beach Point Capital Management L.P. continued to be related parties and Ball Corporation, Hitachi Ltd./Hitachi Software Engineering Co., Ltd., ITT

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

Industries, Inc./Eastman Kodak, MacDonald Dettwiler and Associates and Telespazio S.p.A./Eurimage S.p.A. were no longer related parties as they sold their shares. As of the second quarter of 2010, Beach Point Capital Management L.P. had sold a majority of its shares and therefore was no longer considered a related party. Historical information pertaining to related parties will be disclosed only if balances and activity for these entities are included in the relevant financial statements presented.

Morgan Stanley/Morgan Stanley & Co. Incorporated

As discussed in Note 13, on October 12, 2011, we entered into a new senior secured credit facility and completed the tender offer and consent solicitation regarding our senior secured notes pursuant to which we repurchased all of our previously outstanding senior secured notes. Morgan Stanley Senior Funding, Inc. served as a joint lead arranger and joint bookrunner for the new credit facility and Morgan Stanley served as a dealer manager in connection with the tender offer. As a result of these transactions, Morgan Stanley and its affiliates received compensation in the amount of $3.9 million.

On September 21, 2010, the Company consummated a secondary offering of 6.9 million shares of common stock, on behalf of selling shareholders, at $30.25 per share. Morgan Stanley served as a joint book-runner, and was a seller of the majority of the shares included in the offering, and received compensation in the amount of $5.7 million.

At December 31, 2010 and 2011, Morgan Stanley and its affiliates held 7.5 million shares, or 16.1% and 16.1%, respectively, of the Company’s common stock. Pursuant to the Investor Agreement between the Company and Morgan Stanley, five of our current board of directors were originally Morgan Stanley’s designees. The Directors who were Morgan Stanley designees are Mr. Zervigon, Mr. Albert, Mr. Jenson, Mr. Whitehurst and Mr. Cyprus. Mr. Albert, Mr. Jenson, Mr. Whitehurst and Mr. Cyprus are independent directors, as defined under the applicable rules of the New York Stock Exchange. As a result of the reduction in Morgan Stanley’s ownership percentage subsequent to the sale of shares in the September 2010 secondary offering, Morgan Stanley currently has the right to propose three directors for nomination to the Board of Directors, all of whom must be independent.

Beach Point Capital Management L.P. (assignee of Post Advisory Group LLC)

In January 2009, Beach Point Capital Management L.P. (Beach Point Capital) assumed certain rights and obligations from Post Advisory Group LLC. In connection with that assignment, Beach Point Capital became investment manager of certain funds that hold common stock of the Company.

In April 2009, we paid our senior subordinated notes in full. As a result of the repayment, all deferred financing fees paid to Beach Point Capital associated with this debt were expensed to the income statement in loss from early extinguishment of debt. As a result of the early extinguishment of debt, the Company paid a penalty of $0.9 million as a loss to Beach Point Capital.

Ball Corporation

Under various contracts with Ball Aerospace and Technologies Corporation, we incurred costs of $13.1 million for January 1, 2009 through May 14, 2009, which were capitalized as part of the costs of building our WorldView-2 satellite.

Hitachi, Ltd./Hitachi Software Engineering Co., Ltd.

On January 28, 2005, we entered into a data distribution agreement with Hitachi Software Engineering Co., Ltd. (Hitachi Software) which appoints Hitachi, Ltd. (Hitachi) as a reseller of our products and services and authorized Hitachi to sell access time to our WorldView-2 satellite. Under the data distribution agreement we

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

received a payment of $10.0 million in 2005. We entered into a direct access facility purchase agreement with Hitachi Software on March 23, 2007. Under this agreement, we have constructed and sold to Hitachi Software a direct access facility, which allows a customer of Hitachi Software to directly access and task our WorldView-1 and WorldView-2 satellites. Under our direct access facility purchase agreement we received $16.7 million as of March 31, 2009. Engineering work associated with the agreement has been subcontracted to MacDonald Dettwiler and Associates Ltd. (MDA).

Hitachi earned sales commissions on direct sales by the Company to customers in its region of $0.5 million for January 1, 2009 through May 14, 2009. This amount is accounted for as a reduction of revenue in the consolidated statements of operations.

Hitachi Software purchased approximately $2.7 million of the Company’s products for January 1, 2009 through May 14, 2009.

ITT Industries, Inc./Eastman Kodak

Under the various contracts with ITT Industries, Inc. including the Kodak agreement, we incurred expenditures of $0.8 million for January 1, 2009 through May 14, 2009, which were capitalized as part of the costs of building the satellites.

MacDonald Dettwiler and Associates, Ltd.

Since September 1996, we have had a series of agreements with MDA, for purchase of various goods, software licenses and engineering and related services.

Under various agreements we have incurred expenditures of $3.1 million for January 1, 2009 through May 14, 2009, which were capitalized as part of the costs of building the satellites.

Telespazio S.p.A./Eurimage S.p.A.

Telespazio S.p.A. (Telespazio), is a reseller of our products and services in Europe. Telespazio earned sales commissions on direct sales by the Company to customers in its region of $0.5 million for the year 2009 until May 14, 2009, respectively.

Telespazio and its reseller and subsidiary, Eurimage S.p.A. (Eurimage), purchased approximately $1.6 million of products and services from the Company between January 1, 2009 and May 14, 2009.

 

NOTE 15.

Commitments and Contingencies

The Company is obligated under certain non-cancelable operating leases for office space and equipment. We currently lease 233,903 square feet of office and operations space in two locations in Longmont, Colorado. This space includes our principal executive offices. The rent varies in amounts per year through its expiration date in August 2015. Lease expense for the Longmont location has been recorded on the straight line basis over the term of the lease. The Company received approximately $9.1 million of certain rent incentives that we have deferred and are amortizing over the life of the lease. We have $3.6 million and $2.4 million of net leasehold improvements at December 31, 2010 and 2011, respectively, which we are amortizing ratably over the shorter of the remaining lease term or the useful life of the leasehold improvement.

Rent expense net of sublease income approximated $2.8 million, $2.6 million and $2.3 million, for the year ended December 31, 2009, 2010 and 2011, respectively.

We enter into agreements in the ordinary course of business with resellers and others. Most of these agreements require us to indemnify the other party against third-party claims alleging that one of our products infringes or misappropriates a patent, copyright, trademark, trade secret or other intellectual property right.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

Certain of these agreements require us to indemnify the other party against claims relating to property damage, personal injury or acts or omissions by us, our employees, agents or representatives. In addition, from time to time we have made guarantees regarding the performance of our systems to our customers.

The majority of these agreements do not limit the maximum potential future payments the Company could be obligated to make. The Company evaluates and estimates potential losses from such indemnification based on the likelihood that the future event will occur. To date, the Company has not incurred any material costs as a result of such obligations and has not accrued any material liabilities related to such indemnification and guarantees in the Company’s financial statements.

Future minimum lease payments under all non-cancelable operating leases (net of aggregate future minimum non-cancelable sublease rentals) as of December 31, 2011 are summarized below:

 

     Operating
Leases
    Other
Commitments
 

2012

   $ 3.6      $ 153.9   

2013

     3.3        194.3   

2014

     2.6        11.4   

2015

     1.6        14.9   

2016

     0.1        16.2   

2017 and thereafter

     2.8        16.2   
  

 

 

   

 

 

 

Subtotal

   $ 14.0      $ 406.9   
  

 

 

   

 

 

 

Sublease rentals

     (0.5       
  

 

 

   

 

 

 

Total

   $ 13.5      $ 406.9   
  

 

 

   

 

 

 

In addition to operating lease commitments, other contractual commitments related to the manufacture and delivery of key components for the Company’s EnhancedView program are included in the table above.

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

NOTE 16.

Quarterly Results from Operations (unaudited)

The following table relates to our results of operations for each quarter of the years ended December 31, 2010 and 2011. The selected quarterly financial information for each of the quarters in the year ended December 31, 2010 and for the first three quarters in the year ended December 31, 2011 have been revised to correct the errors described in Note 3, Revision of Previously Issued Financial Statements to the consolidated financial statements in this Annual Report on Form 10-K.

 

     2010  
     For the Quarters Ended  
     March 31     June 30     September 30     December 31  
     As
Previously
Reported
    Revised     As
Previously
Reported
    Revised     As
Previously
Reported
    Revised     As
Previously
Reported
    Revised  
     (In millions, except per share amounts)  

Revenue

   $ 77.1      $ 77.3      $ 81.0      $ 80.9      $ 80.5      $ 80.6      $ 83.6      $ 83.7   
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Cost of revenue, excluding deprecation and amortization

     10.1        10.3        10.1        10.4        11.0        11.9        10.5        11.6   

Selling, general and administrative

     24.8        24.8        28.2        28.0        28.2        28.2        31.3        31.2   

Depreciation and amortization

     29.1        29.2        31.0        31.1        29.2        29.1        29.6        29.5   
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Income from operations

     13.1        13.0        11.7        11.4        12.1        11.4        12.2        11.4   

Interest income (expense), net

     (9.9     (10.0     (10.7     (10.7     (10.0     (10.5     (9.0     (9.2
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Income before income taxes

     3.2        3.0        1.0        0.7        2.1        0.9        3.2        2.2   

Income tax benefit (expense)

     (1.7     (1.6     (0.5     (0.4     (1.3     (0.8     (1.9     (1.5
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Net income (loss)

   $ 1.5      $ 1.5      $ 0.5      $ 0.3      $ 0.8      $ 0.1      $ 1.3      $ 0.6   
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Earnings (loss) per share — basic

   $ 0.03      $ 0.03      $ 0.01      $ 0.01      $ 0.02      $ 0.00      $ 0.03      $ 0.01   
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Earnings (loss) per share — diluted

   $ 0.03      $ 0.03      $ 0.01      $ 0.01      $ 0.02      $ 0.00      $ 0.03      $ 0.01   
  

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

 

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DigitalGlobe, Inc.

Notes To Consolidated Financial Statements — (Continued)

 

 

    2011  
    For the Quarters Ended  
    March 31     June 30     September 30     December 31(1)  
    As
Previously
Reported
    Revised     As
Previously
Reported
    Revised     As
Previously
Reported
    Revised        
    (In millions, except per share amounts)  

Revenue

  $ 77.1      $ 77.4      $ 81.7      $ 82.5      $ 81.3      $ 81.9      $ 97.7   
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Cost of revenue, excluding depreciation and amortization

    11.8        13.1        14.4        15.4        17.6        18.5        17.9   

Selling, general and administrative

    30.1        30.2        33.7        34.2        30.7        30.8        35.0   

Depreciation and amortization

    29.2        29.2        29.2        29.2        29.1        29.1        29.6   
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Income from operations

    6.0        4.9        4.4        3.7        3.9        3.5        15.2   

Interest income (expense), net

    (7.7     (7.9     (5.5     (5.7     (4.6     (4.1     (4.0
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Income before income taxes

    (1.6     (2.8     (1.1     (2.0     (0.7     (0.6     (40.6

Income tax benefit (expense)

    0.9        1.5        0.7        1.1        1.8        1.7        13.6   
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Net income (loss)

  $ (0.7   $ (1.3   $ (0.4   $ (0.9   $ 1.1      $ 1.1        (27.0
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Earnings (loss) per share — basic

  $ (0.02   $ (0.03   $ (0.01   $ (0.02   $ 0.02      $ 0.02      $ (0.58
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

Earnings (loss) per share — diluted

  $ (0.02   $ (0.03   $ (0.01   $ (0.02   $ 0.02      $ 0.02      $ (0.58
 

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

   

 

 

 

All revenue revisions for each period presented apply specifically to the Company’s Direct Access business. Total Direct Access revenue as revised for each period presented during 2010 was $5.2 million; $9.5 million; $10.6 million; and $9.4 million for the first quarter; second quarter; third quarter and fourth quarter, respectively. Total Direct Access revenue as revised for each period presented during 2011 was $9.8 million; $13.5 million; and $12.1 million for the first quarter, second quarter and third quarter, respectively.

 

(1)

During the fourth quarter ended December 31, 2011 the Company recorded a loss on extinguishment of debt of $51.8 million pretax.

 

NOTE 17.

Valuation and Qualifying Accounts

The following table shows the roll-forward for our allowance for doubtful accounts.

 

       Balance at
Beginning
of Period
     Additions
(Reductions)

Charged to
Operations
     Write-offs
and
Adjustments
    Balance at
End of
Period
 
     (In millions)  

Allowance for doubtful accounts

          

Year Ended:

          

December 31, 2011

     1.0         4.7         (2.1     3.6   

December 31, 2010

     1.2                 (0.2     1.0   

December 31, 2009

     0.9         1.0         (0.7     1.2   

 

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ITEM 9.

CHANGES IN AND DISAGREEMENTS WITH ACCOUNTANTS ON ACCOUNTING AND FINANCIAL DISCLOSURE

None.

 

ITEM 9A.

CONTROLS AND PROCEDURES

Evaluation of Disclosure Controls and Procedures

Under the supervision of and with the participation of management, including our Chief Executive Officer and Chief Financial Officer, the Company conducted an evaluation of the effectiveness of the design and operation of our disclosure controls and procedures, as defined in Rules 13a-15(e) and 15d-15(e) of the Securities and Exchange Act of 1934, as amended (the “Exchange Act”), as of December 31, 2011. The Company’s evaluation has identified certain material weaknesses in its internal control over financial reporting as noted below in Management’s Report on Internal Control over Financial Reporting. Based on the evaluation of these material weaknesses, the Chief Executive Officer and Chief Financial Officer have concluded that the Company’s disclosure controls and procedures were not effective as of December 31, 2011 to ensure that information required to be disclosed by the Company in the reports that it files or submits under the Exchange Act is recorded, processed, summarized and reported, within the time periods specified in the SEC’s rules and forms, and that such information is accumulated and communicated to management, including our Chief Executive Officer and Chief Financial Officer, to allow timely decisions regarding required disclosure. In light of the material weaknesses described below, the Company performed additional analysis and other post-closing procedures including but not limited to, a detailed review of balance sheet accounts as of and for the year-ended December 31, 2011, a review of the Company’s compliance with its critical accounting policies and discussions with independent technical advisors of certain of our complex accounting transactions to ensure the consolidated financial statements were prepared in accordance with generally accepted accounting principles in the United States (“U.S. GAAP”).

Accordingly, management concluded that the consolidated financial statements in this Annual Report fairly present, in all material respects, our financial position, results of operations and cash flows as of the dates, and for the periods presented, in conformity with U.S. GAAP.

Management’s Report on Internal Control over Financial Reporting

Management is responsible for establishing and maintaining adequate internal control over financial reporting, as defined in Rules 13a-15(f) and 15d-15(f) of the Exchange Act. The Company’s internal control over financial reporting is a process designed to provide reasonable assurance regarding the reliability of its financial reporting and the preparation of its financial statements for external purposes in accordance with GAAP and includes those policies and procedures that: (i) pertain to the maintenance of records that, in reasonable detail, accurately and fairly reflect the transactions and dispositions of the assets of the Company; (ii) provide reasonable assurance that transactions are recorded as necessary to permit preparation of financial statements in accordance with generally accepted accounting principles, and that receipts and expenditures of the Company are being made only in accordance with authorizations of management and directors of the Company; and (iii) provide reasonable assurance regarding prevention or timely detection of unauthorized acquisition, use, or disposition of the Company’s assets that could have a material effect on the financial statements. Because of its inherent limitations, internal control over financial reporting may not prevent or detect misstatements. Also, projections of any evaluation of effectiveness to future periods are subject to the risk that controls may become inadequate because of changes in conditions or that the degree of compliance with the policies or procedures may deteriorate.

Under the supervision of and with the participation of management, including the Chief Executive Officer and Chief Financial Officer, the Company conducted an evaluation of the effectiveness of its internal control over financial reporting based on the criteria in Internal Control—Integrated Framework issued by the Committee of Sponsoring Organizations of the Treadway Commission (“COSO”). A material weakness is a control deficiency, or combination of control deficiencies, such that there is a reasonable possibility that a

 

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material misstatement to the annual or interim financial statements will not be prevented or detected on a timely basis. Based upon that evaluation, management identified the following material weaknesses as of December 31, 2011 in the Company’s internal control over financial reporting.

Account ing for Direct Access Program (“ DAP ).    Management did not maintain effective controls over the accuracy, completeness and presentation of the accounting for DAP contracts in accordance with U.S. GAAP. Specifically, effective controls were not designed to provide reasonable assurance that the identification and application of the accounting principles was appropriate related to the amortization of deferred contract costs, the proper recognition of revenue for DAP customers, the determination of the principal in the arrangements for gross versus net revenue presentation, and the capitalization of interest related to each DAP contract.

Insufficient Complement of Personnel with Appropriate Accounting Knowledge and Training.     Management did not maintain a sufficient complement of personnel with an appropriate level of accounting knowledge, experience and training in the application of U.S. GAAP, which resulted in audit adjustments related to the DAP (as discussed above), stock-based compensation, and certain accrued liability accounts.

These material weaknesses resulted in the revision of the Company’s previously reported results for the year ended December 31, 2010 and our unaudited quarterly financial information for the first three quarters of 2011 and all the quarters in 2010. Additionally, these material weaknesses could result in misstatements to the Company’s accounts and disclosures that would result in a material misstatement to the consolidated financial statements that would not be prevented or detected.

As a result of the material weaknesses in internal control over financial reporting described above, management concluded that the Company’s internal control over financial reporting was not effective as of December 31, 2011 based on the criteria established in Internal Control—Integrated Framework issued by the COSO. The effectiveness of the Company’s internal control over financial reporting as of December 31, 2011 has been audited by PricewaterhouseCoopers LLP, an independent registered public accounting firm, as stated in their report which appears in this Form 10-K.

Plan for Remediation of the Material Weaknesses in Internal Control over Financial Reporting

Management is actively engaged in the planning for and implementation of remediation efforts to address the material weaknesses. These remediation efforts, outlined below, are intended both to address the identified material weaknesses and to enhance the Company’s overall financial control environment. Management believes that these material weaknesses arose due to the Company’s rapid growth and the challenges of being a publicly held company, including increased SEC reporting requirements, which have outpaced the development of the Company’s accounting infrastructure and processes.

During 2011 the Company increased its accounting staff, including key technical accounting positions, to enhance the overall financial control environment. Specifically, during the fourth quarter of 2011, the Company added five resources to the accounting and finance staff, including two certified public accountants, to strengthen the Company’s accounting processes.

Management’s planned actions to further address these issues in 2012 include:

 

   

the addition of more experienced accounting staff with appropriate expertise to address technical accounting issues;

 

   

an evaluation of the company’s critical accounting policies to ensure they are documented, reviewed, and circulated to appropriate company personnel, as well as reviewed and updated on a periodic basis;

 

   

a formal training program for all technical accounting personnel to enable them to remain current with accounting rules, regulations and trends;

 

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development of a process for the identification, documentation, review and approval of all complex technical contracts and issues; and

 

   

enhancement of the monthly process to review balance sheet fluctuations to identify, new and/or unusual transactions.

 

The audit committee has directed management to develop a detailed plan and timetable for the implementation of the foregoing remedial measures and will monitor their implementation. In addition, under the direction of the audit committee, management will continue to review and make necessary changes to the overall design of the Company’s internal control environment, as well as policies and procedures to improve the overall effectiveness of internal control over financial reporting.

Management believes the measures described above and other procedures that will be implemented will remediate the control deficiencies the Company has identified and strengthen its internal control over financial reporting. Management is committed to continuous improvement of the Company’s internal control processes and will continue to diligently review the Company’s financial reporting controls and procedures. As management continues to evaluate and work to improve internal control over financial reporting, the Company may determine to take additional measures to address control deficiencies or determine to modify, or in appropriate circumstances not to complete, certain of the remediation measures described above.

Changes in Internal Control over Financial Reporting

During the fiscal quarter ended December 31, 2011 the Company added five resources to the accounting and finance staff, including two certified public accountants, to strengthen the Company’s accounting processes. These changes are reasonably likely to materially affect the Company’s internal control over financial reporting.

 

ITEM 9B.

OTHER INFORMATION

None.

 

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PART III

 

ITEM 10.

DIRECTORS, EXECUTIVE OFFICERS AND CORPORATE GOVERNANCE

 

Information regarding our directors, including the audit committee and audit committee financial experts, and executive officers and compliance with Section 16(a) of the Exchange Act will be included in our definitive proxy statement for the 2012 Annual Meeting of Stockholders (the Proxy Statement) and is incorporated herein by reference.

We have adopted a Code of Ethics and Business Conduct that governs our senior officers, including our chief executive officer and chief financial officer, and employees. Copies of our Code of Ethics and Business Conduct are available on our website at www.digitalglobe.com and may also be obtained upon request without charge by writing to the Secretary of the Company, DigitalGlobe, Inc., 1601 Dry Creek Drive, Suite 260, Longmont, Colorado 80503. We will post to our website any amendments to the Code of Ethics and Business Conduct, and any waivers that are required to be disclosed by the rules of either the SEC or the NYSE.

Copies of our Corporate Governance Guidelines and the charters of our Audit Committee, Compensation Committee and Nominating and Governance Committee are available on our website and may also be obtained upon request without charge as described in the preceding paragraph.

 

ITEM 11.

EXECUTIVE COMPENSATION

The information required by this item will be included in the Proxy Statement and is incorporated herein by reference.

 

ITEM 12.

SECURITY OWNERSHIP OF CERTAIN BENEFICIAL OWNERS AND MANAGEMENT AND RELATED STOCKHOLDER MATTERS

The information required by this item, including information relating to security ownership of certain beneficial owners of our common stock and of our management, will be included in the Proxy Statement and is incorporated herein by reference.

 

ITEM 13.

CERTAIN RELATIONSHIPS AND RELATED TRANSACTIONS, AND DIRECTOR INDEPENDENCE

The information required by this item, including information under the caption “Certain Relationships and Related Transactions” in the Proxy Statement and information regarding director independence, will be included in the Proxy Statement and is incorporated herein by reference.

 

ITEM 14.

PRINCIPAL ACCOUNTING FEES AND SERVICES

The information required by this item, including information under the caption “Independent Registered Public Accounting Firm Fees and Services” in the Proxy Statement, will be included in the Proxy Statement and is incorporated herein by reference.

 

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PART IV

 

ITEM 15.

EXHIBITS AND FINANCIAL STATEMENT SCHEDULES

(a) List of documents filed as part of this report:

(1) Consolidated Financial Statements and Report of Independent Registered Public Accounting Firm See the Index to Financial Statements and Financial Statement Schedules set forth in Part II, Item 8 of this report.

(2) Financial Statement Schedules

None required

(3) List of Exhibits

The agreements included as exhibits to this report contain representations and warranties by each of the parties to the applicable agreement. These representations and warranties were made solely for the benefit of the other parties to the applicable agreement and (i) were not intended to be treated as categorical statements of fact, but rather as a way of allocating the risk to one of the parties if those statements prove to be inaccurate; (ii) may have been qualified in such agreement by disclosures that were made to the other party in connection with the negotiation of the applicable agreement; (iii) may apply contract standards of “materiality” that are different from “materiality” under the applicable securities laws; and (iv) were made only as of the date of the applicable agreement or such other date or dates as may be specified in the agreement.

We acknowledge that, notwithstanding the inclusion of the foregoing cautionary statements, the Company is responsible for considering whether additional specific disclosures of material information regarding material contractual provisions are required to make the statements in this report not misleading.

 

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SIGNATURES

Pursuant to the requirements of Section 13 or 15(d) of the Securities Exchange Act of 1934, the registrant has duly caused this report to be signed on its behalf by the undersigned, thereunto duly authorized.

 

    DigitalGlobe, Inc.

February 29, 2012

   

By:

 

/s/    Yancey L. Spruill

     

Name:  Yancey L. Spruill

Title:    Executive Vice President, Chief Financial Officer and Treasurer

Pursuant to the requirements of the Securities Exchange Act of 1934, this report has been signed by the following persons in the capacities and on the dates indicated.

 

Signature

  

Title

 

Date

/s/    Jeffrey R. Tarr

Jeffrey R. Tarr

  

President and Chief Executive Officer

(Principal Executive Officer)

  February 29, 2012

/s/    Yancey L. Spruill

Yancey L. Spruill

  

Executive Vice President,

Chief Financial Officer and Treasurer

  February 29, 2012

/s/    Carl Long

Carl Long

  

Chief Accounting Officer

(Principal Accounting Officer)

  February 29, 2012

/s/    Paul M. Albert, Jr.

Paul M. Albert, Jr.

   Director   February 29, 2012

/s/    Nick S. Cyprus

Nick S. Cyprus

   Director   February 29, 2012

/s/    General Howell M. Estes III

General Howell M. Estes III

   Director   February 29, 2012

/s/    Warren C. Jenson

Warren C. Jenson

   Director   February 29, 2012

/s/    Alden Munson Jr.

Alden Munson Jr.

   Director   February 29, 2012

/s/    James M. Whitehurst

James M. Whitehurst

   Director   February 29, 2012

/s/    Kimberly Till

Kimberly Till

   Director   February 29, 2012

/s/    Eddy Zervigon

Eddy Zervigon

   Director   February 29, 2012

 

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Exhibit Index

 

Exhibit
Number

  

Description

  3.1   

Amended and Restated Certificate of Incorporation of DigitalGlobe, Inc. (incorporated herein by reference to Exhibit 3.1 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2009, filed on February 24, 2010).

  3.2   

Amended and Restated By-laws of DigitalGlobe, Inc. (incorporated herein by reference to Exhibit 3.2 to the Company’s Quarterly Report on Form 10-Q for the quarter ended June 30, 2009, filed on August 12, 2009).

  4.1   

Specimen Common Stock Certificate of DigitalGlobe, Inc. (incorporated herein by reference to Exhibit 4.1 to Amendment No. 7 to the Company’s Registration Statement on Form S-1 filed on May 13, 2009 (File No. 333-150235)).

  4.2   

Indenture relating to the senior secured notes, by and between DigitalGlobe, Inc. and U.S. Bank, National Association, as trustee, dated as of April 28, 2009 (incorporated herein by reference to the Company’s Registration Statement on Form S-1 (File No. 333-150235)).

  4.3   

First Supplemental Indenture, dated as of October 5, 2011, between the Company and U.S. Bank National Association, as trustee (incorporated herein by reference to Exhibit 4.1 to the Company’s Current Report on Form 8-K filed on October 7, 2011).

10.1   

Credit and Guaranty Agreement, dated October 12, 2011, by and among DigitalGlobe, Inc., the guarantors party thereto, the lenders named therein and J.P. Morgan Chase Bank, N.A., as administrative agent and as collateral agent (incorporated herein by reference to Exhibit 10.1 to the Company’s Current Report on Form 8-K filed on October 13, 2011).

10.2#   

EnhancedView Imagery Acquisition Contract #HM0210-10-C-0002, dated August 6, 2010, by and between DigitalGlobe, Inc. and National Geospatial-Intelligence Agency (incorporated herein by reference to Exhibit 10.1 to the Company’s Quarterly Report on Form 10-Q/A for the quarter ended September 30, 2010 filed on May 24, 2011).

10.3#   

Amendment to EnhancedView Imagery Acquisition Contract #HM021010C0002, by and between DigitalGlobe, Inc. and National Geospatial-Intelligence Agency, dated July 25, 2011 (incorporated herein by reference to Exhibit 10.1 to the Company’s Quarterly Report on Form 10-Q/A for the quarter ended September 30, 2011 filed on February 24, 2012).

10.4†#   

Amendment to EnhancedView Imagery Acquisition Contract #HM021010C0002, by and between DigitalGlobe, Inc. and National Geospatial-Intelligence Agency, dated October 31, 2011.

10.5#   

WorldView-3 Satellite Purchase Agreement #60150, dated September 1, 2010, by and between DigitalGlobe, Inc. and Ball Aerospace & Technologies Corp. (incorporated herein by reference to Exhibit 10.2 to the Company’s Quarterly Report on Form 10-Q/A for the quarter ended September 30, 2010 filed on May 24, 2011).

10.5.1†#   

Amendment No. 1 to WorldView-3 Satellite Purchase Agreement #60150, by and between DigitalGlobe, Inc. and Ball Aerospace & Technologies Corp.

10.5.2†#   

Amendment No. 3 to WorldView-3 Satellite Purchase Agreement #60150, by and between DigitalGlobe, Inc. and Ball Aerospace & Technologies Corp.

10.5.3†#   

Amendment No. 4 to WorldView-3 Satellite Purchase Agreement #60150, by and between DigitalGlobe, Inc. and Ball Aerospace & Technologies Corp.

10.5.4†#   

Amendment No. 5 to WorldView-3 Satellite Purchase Agreement #60150, by and between DigitalGlobe, Inc. and Ball Aerospace & Technologies Corp.

10.6#          

WorldView-3 Instrument Purchase Agreement #60151, dated September 1, 2010, by and between DigitalGlobe, Inc. and ITT Space Systems, LLC (incorporated herein by reference to Exhibit 10.3 to the Company’s Quarterly Report on Form 10-Q/A for the quarter ended September 30, 2010 filed on May 24, 2011).

 

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Exhibit
Number

  

Description

10.6.1†#   

Modifications #1-5 and 7-12 to WorldView-3 Instrument Purchase Agreement #60151, by and between DigitalGlobe, Inc. and ITT Space Systems, LLC.

10.7   

Office Lease, dated March 19, 2004, by and between DigitalGlobe, Inc. and K/B Fund IV (incorporated herein by reference to Exhibit 10.6 to the Company’s Registration Statement on Form S-1 filed on April 14, 2008 (File No. 333-150235)).

10.8   

First Amendment to Office Lease, dated September 10, 2004, by and between K/B Fund IV and DigitalGlobe, Inc. (incorporated herein by reference to Exhibit 10.7 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010 filed on February 28, 2011).

10.9   

First Amendment to Lease, dated April 18, 2005, by and between Hub Properties Trust and DigitalGlobe, Inc. (incorporated herein by reference to Exhibit 10.8 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010, filed on February 28, 2011).

10.10†   

First Amendment to Lease dated October 14, 2011, by and between Hub Properties Trust and DigitalGlobe, Inc.

10.11   

Stockholders’ Agreement, dated as of July 9, 2003, among DigitalGlobe, Inc. and certain stockholders listed on the signature pages thereto (incorporated herein by reference to Exhibit 10.7 to Amendment No. 1 to the Company’s Registration Statement on Form S-1 filed on June 6, 2008 (File No. 333-150235)).

10.12   

Amendment to the Stockholders’ Agreement, dated as of March 24, 2008, among DigitalGlobe, Inc. and certain stockholders listed on the signature pages thereto (incorporated herein by reference to Exhibit 10.8 to Amendment No. 5 to the Company’s Registration Statement on Form S-1 filed on April 29, 2009 (File No. 333-150235)).

10.13   

Investor Agreement by and between DigitalGlobe, Inc. and Morgan Stanley & Co. Incorporated, dated as of April 28, 2009 (incorporated herein by reference to Exhibit 10.11 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010, filed on February 28, 2011).

10.14*   

Employment Agreement by and between DigitalGlobe, Inc. and Yancey L. Spruill, dated as of June 1, 2008 (incorporated herein by reference to Exhibit 10.11 to Amendment No. 4 to the Company’s Registration Statement on Form S-1 filed on March 24, 2009 (File No. 333-150235).

10.15*   

Offer Letter to J. Alison Alfers, dated as of December 13, 2007 (incorporated herein by reference to Exhibit 10.15 to Amendment No. 4 to the Company’s Registration Statement on Form S-1 filed on March 24, 2009 (File No. 333-150235)).

10.16*   

Severance Protection Agreement by and between DigitalGlobe, Inc. and J. Alison Alfers, dated as of June 1, 2008 (incorporated herein by reference to Exhibit 10.16 to Amendment No. 4 to the Company’s Registration Statement on Form S-1 filed on March 24, 2009 (File No. 333-150235)).

10.17*   

Offer Letter to A. Rafay Khan, dated as of December 31, 2008 (incorporated herein by reference to Exhibit 10.13 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2009 filed on February 24, 2010).

10.18*   

Severance Protection Agreement by and between DigitalGlobe, Inc and A. Rafay Khan, dated as of January 16, 2009 (incorporated herein by reference to Exhibit 10.14 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2009 filed on February 24, 2010).

10.19*
  

Offer Letter to John Oechsle, dated as of March 22, 2010 (incorporated herein by reference to Exhibit 10.15 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010 filed on February 28, 2011).

10.20*
  

Severance Protection Agreement by and between DigitalGlobe, Inc. and John Oechsle, dated as of April 15, 2010 (incorporated herein by reference to Exhibit 10.16 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010 filed on February 28, 2011).

 

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Exhibit
Number

  

Description

10.21*   

Amended and Restated Employment Agreement by and between DigitalGlobe, Inc. and Jill Smith (incorporated herein by reference to the Company’s Current Report on Form 8-K filed on October 29, 2010).

10.22*   

Employment Agreement by and between DigitalGlobe, Inc. and Jeffrey R. Tarr, dated as of February 23, 2011 and effective as of April 5, 2011 (incorporated herein by reference to Exhibit 10.1 to the Company’s Current Report on Form 8-K filed on February 28, 2011).

10.23*   

Amended and Restated 1999 Equity Incentive Plan (incorporated herein by reference to Exhibit 10.18 to the Company’s Registration Statement on Form S-1 filed on April 14, 2008 (Registration No. 333-150235)).

10.26†*   

2007 Employee Stock Option Plan, as amended.

10.27*   

2011 Executive Success Sharing Plan (Executive and Director Bonus Plan incorporated herein by reference to Exhibit 10.25 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010 filed on February 28, 2011).

10.28*   

Form of Restricted Stock Award Agreement, 30% vest on August 31, 2011 and 70% vest on August 31, 2012 (incorporated herein by reference to Exhibit 10.1 to the Company’s Current Report on Form 8-K filed on October 29, 2010).

10.29*   

Form of Amendment to Employment Agreement (incorporated herein by reference to Exhibit 10.2 to the Company’s Current Report on Form 8-K filed on October 29, 2010).

10.30*   

Form of Amendment to Severance Protection Agreement (incorporated herein by reference to Exhibit 10.3 to the Company’s Current Report on Form 8-K filed on October 29, 2010).

10.31*   

Form of Incentive Stock Option Award Agreement, 25% vest on the first year anniversary of the grant date and monthly thereafter (incorporated by reference to Exhibit 10.29 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010 filed on February 28, 2011).

10.32*   

Form of Incentive Stock Option Award Agreement, 25% vest annually (incorporated by reference to Exhibit 10.30 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010 filed on February 28, 2011).

10.33*   

Form of Non-Qualified Stock Option Award Agreement, 25% vest on the first year anniversary of the grant date and monthly thereafter (incorporated by reference to Exhibit 10.31 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010 filed on February 28, 2011).

10.34*   

Form of Non-Qualified Stock Option Award Agreement, 25% vest annually (incorporated by reference to Exhibit 10.32 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010 filed on February 28, 2011).

10.35*   

Form of Restricted Stock Award Agreement, 25% vest annually (incorporated by reference to Exhibit 10.33 to the Company’s Annual Report on Form 10-K for the year ended December 31, 2010 filed on February 28, 2011).

21.1†   

Subsidiaries of Registrant.

23.1†   

Consent of PricewaterhouseCoopers LLP, Independent Registered Public Accounting Firm.

31.1†   

Certification of Chief Executive Officer of DigitalGlobe, Inc., pursuant to Section 302 of the Sarbanes-Oxley Act of 2002.

31.2†   

Certification of Chief Financial Officer of DigitalGlobe, Inc., pursuant to Section 302 of the Sarbanes-Oxley Act of 2002.

32.1†   

Certification of Chief Executive Officer of DigitalGlobe, Inc., pursuant to Section 906 of the Sarbanes-Oxley Act of 2002.

32.2†   

Certification of Chief Financial Officer of DigitalGlobe, Inc., pursuant to Section 906 of the Sarbanes-Oxley Act of 2002.

 

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Exhibit
Number

  

Description

101†/+   

The following materials for the DigitalGlobe, Inc. Annual Report on Form 10-K for the year ended December 31, 2011, filed on February 29, 2012 formatted in eXtensible Business Reporting Language (XBRL):

(i.)    Audited Consolidated Statements of Operations

(ii.)  Audited Consolidated Balance Sheets

(iii.) Audited Consolidated Statements of Cash Flows

(iv.) Audited Consolidated Statements of Stockholders’ Equity and Statement of Comprehensive Income (Loss)

(v.)   Related notes, tagged or blocks of text

 

  †

Filed or furnished herewith.

 

  #

Certain portions of this exhibit have been omitted by redacting a portion of the text. This exhibit has been filed separately with the Securities and Exchange Commission pursuant to a request for confidential treatment.

 

  *

Management contract or compensatory plan arrangement.

  +

XBRL (eXtensible Business Reporting Language) Information is furnished and not filed or a part of a registration statement or prospectus for purposes of sections 11 or 12 of the Securities Act of 1933, as amended, is deemed not filed for purposes of section 18 of the Securities Exchange Act of 1934, as amended, and otherwise is not subject to liability under these sections.

 

91

Exhibit 10.4

FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

UNCLASSIFIED

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT   1. CONTRACT ID CODE    PAGE OF PAGES

1          |       10

2. AMENDMENT/MODIFICATION NO.

01

 

3. EFFECTIVE DATE

See Block 16C

  4. REQUISITION/PURCHASE REQ NO.   5. PROJECT NO.  (if applicable)
6. ISSUED BY   CODE   HM0210   7. ADMINISTERED BY (If other than Item 6)   CODE     62LESSERMM
   
[**REDACTED**]       [**REDACTED**]    
   
             
8. NAME AND ADDRESS OF CONTRACTOR INC., (No., street, county, State and ZIP Code)   (x)  

9A.

 

 

AMENDMENT OF SOLICITATION NO.

 

   
    9B.   DATED (SEE ITEM 11)
DIGITALGLOBE, INC.        
Attn: DIGITALGLOBE, INC.   x   10A.  

MODIFICATION OF CONTRACT/ORDER NO.

1601 DRY CREEK DRIVE SUITE 260        
LONGMONT CO 805036493     HM021010C0002
   

0002

 

    10B.   DATED (SEE ITEM 13)    
CODE    1CGQ7       FACILITY CODE      

 

09/21/2011

       

11. THIS ITEM ONLY APPLIES TO AMENDMENTS OF SOLICITATIONS

 

  q The above numbered solicitation is amended as set forth in Item 14. The hour and date specified for receipt of Offers                     ¨   is extended. ¨ is not extended.
     Offers must acknowledge receipt of this amendment prior to the hour and date specified in the solicitation or as amended, by one of the following methods: (a) By completing Items 8 and 15, and returning              copies of the amendment, (b) By acknowledging receipt of this amendment on each copy of the offer submitted; or (c) By separate letter of telegram which includes a reference to the solicitation and amendment numbers. FAILURE OF YOUR ACKNOWLEDGEMENT TO BE RECEIVED AT THE PLACE DESIGNATED FOR THE RECEIPT OF OFFERS PRIOR TO THE HOUR AND DATE SPECIFIED MAY RESULT IN REJECTION OF YOUR OFFER. If by virtue of this amendment you desire to change an offer already submitted, such change may be made by telegram or letter, provided each telegram or letter makes reference to the solicitation and this amendment, and is received prior to the opening hour and date specified.

 

12. ACCOUNTING AND APPROPRIATION DATA (If required)

Not Applicable

 

13. THIS ITEM ONLY APPLIES TO MODIFICATION OF CONTRACTS/ORDERS. IT MODIFIES THE CONTRACT/ORDER NO. AS DESCRIBED IN ITEM 14.

 

CHECK ONE

 

 

A.

 

 

THIS CHANGE ORDER IS ISSUED PURSUANT TO: (Specify authority) THE CHANGES SET FORTH IN ITEM 14 ARE MADE IN THE CONTRACT ORDER NO. IN ITEM 10A.

 

   
    B.  

THE ABOVE NUMBERED CONTRACT/ORDER IS MODIFIED TO REFLECT THE ADMINISTRATIVE CHANGES (such as changes in paying office, appropriation date, etc.) SET FORTH IN ITEM 14. PURSUANT TO THE AUTHORITY OF FAR 43.103(b).

 

    C.  

THIS SUPPLEMENTAL AGREEMENT IS ENTERED INTO PURSUANT TO AUTHORITY OF:

 

X   D.  

OTHER (Specify type of modification and authority)

Mutual Agreement of the Parties

    E.  IMPORTANT:                             Contractor   ¨ is not,     x   is required to sign this document and return 1 copies to the issuing office.

14, DESCRIPTION OF AMENDMENT/MODIFICATION (Organized by UCF section headings, including solicitation/contract subject matter where feasible.)

Tax ID Number: 31-1420852

DUNS Number: 789638418

The purpose of this no - cost modification is to (1) delete the first paragraph from DD Form 1155, Optional Form 336, page 2 of 15 and to replace the second paragraph of the Statement of Work (SOW) [ **REDACTED**] in order to provide clarification [ **REDACTED**] and (2) Add [**REDACTED**] as a billable country under item 0001, Sub-Item 000101, Item 0002, Sub - Item 000201, and Item 0003, Sub-Item 000201. Accordingly, the Order is revised changed as follows:

Continued …

Except as provided heroin, all terms and conditions of the document referenced In Item 9A or 10A as heretofore changed, remains unchanged and in full force and effect.

15h. NAME AND TITLE OF SIGNER (Type or print)

 

[**REDACTED**]

     

16A. NAME AND TITLE OF CONTRACTING OFFICER (Type or print)

 

[**REDACTED**]

 

   
15B. CONTRACTOR/OFFEROR       16B. UNITED STATES OF AMERICA    
   

 

[/s/    **REDACTED**]

(Signature of person authorized to sign)

     

15C. DATE SIGNED

 

10/26/11

     

 

[/s/    **REDACTED**]

(Signature of Contracting Officer)

     

16C DATE SIGNED

 

10/31/11

NSN 7540-01-152-8070

   STANDARD FORM 30 (REV. 10-83)

Previous edition unusable

   Prescribed by GSA
   FAR (46 CFR) 53.243

UNCLASSIFIED


UNCLASSIFIED

 

CONTINUATION SHEET    REFERENCE NO. OF DOCUMENT BEING CONTINUED   

PAGE    OF

2        |        10

   HM021010C0002/0002/01   

NAME OF OFFEROR OR CONTRACTOR

DIGITALGLOBE, INC.

 

ITEM NO.

(A)

  

SUPPLIES/SERVICES

(B)

  

QUANTITY

(C)

  

UNIT

(D)

  

UNIT PRICE

(E)

  

AMOUNT

(F)

  

1. The first paragraph from DD Form 1155, Optional Form 336, page 2 of 15:

 

[**REDACTED**]

 

is deleted in its entirety without replacement.

 

[**REDACTED**]

 

is deleted and replaced with the following new paragraph:

 

[**REDACTED**]

 

The date on the SOW is changed from 03 August 2011 to 21 October 2011 under Items 0001, 0002,

 

Continued …

           

 

            NSN 7540-01-152-8067   

OPTIONAL FORM 336 (4-86)            

Prescribed by GSA

FAR (48 CFR) 53.110

UNCLASSIFIED


UNCLASSIFIED

 

CONTINUATION SHEET    REFERENCE NO. OF DOCUMENT BEING CONTINUED   

PAGE    OF

3        |        10

   HM021010C0002/0002/01   

NAME OF OFFEROR OR CONTRACTOR

DIGITALGLOBE, INC.

 

ITEM NO.

(A)

  

SUPPLIES/SERVICES

(B)

  

QUANTITY

(C)

  

UNIT

(D)

  

UNIT PRICE

(E)

  

AMOUNT

(F)

  

0003 and 0004.

 

3. [**REDACTED**] is added to Item 0001, Sub-Item 000101, Item 0002, Sub-Item 000201, and Item 0003, Sub-Item 000301.

 

The total funding available and the total value of Order 0002 remains unchanged.

 

Discount Terms:

 

Net 30

 

Payment:

 

[**REDACTED**]

 

FOB: Destination

 

Change Item 0001 to read as follows (amount shown is the obligated amount):

 

Enhanced GEOINT Delivery - Foundation GEOINT(FG)

 

Layer: [**REDACTED**] This item also includes expenses associated with the dissemination of imagery and image products on media.

           
0001   

1. The contractor shall provide all personnel, materials, facilities and equipment to complete this requirement.

 

2. This Item is an Indefinite Quantity Cost Item. The sum of all products invoiced for under this Item shall not exceed $ [**REDACTED**] . The Government Contracting Officer’s Representative

 

Continued …

            [**REDACTED**]

 

NSN 7540-01-152-8067   

OPTIONAL FORM 336 (4-86)            

Prescribed by GSA

FAR (48 CFR) 53.110

UNCLASSIFIED


UNCLASSIFIED

 

CONTINUATION SHEET    REFERENCE NO. OF DOCUMENT BEING CONTINUED   

PAGE    OF

4        |        10

   HM021010C0002/0002/01   

NAME OF OFFEROR OR CONTRACTOR

DIGITALGLOBE, INC.

 

ITEM NO.

(A)

  

SUPPLIES/SERVICES

(B)

  

QUANTITY

(C)

  

UNIT

(D)

  

UNIT PRICE

(E)

  

AMOUNT

(F)

  

(COR) or the EGD Technical Points of Contact (POC) will identify areas to be produced.

 

3. The contractor shall invoice for the basic FG imagery product delivered under this item at the fixed rate of $ [**REDACTED**] for quarter cells and at the fixed rate of $ [**REDACTED**] for full cells. Additional associated product pricing shall be invoiced at the rates in the Attachment entitled EGD Product Price List.

 

4. When invoicing, the contractor shall segregate and cite the following specific Accounting Classification Reference Numbers (ACRN) for deliveries associated with the following countries by the indicated informational Sub-Item numbers:

 

Sub-Item 000101, [**REDACTED**]

 

Sub-Item 000102, [**REDACTED**]

 

Sub-Item 000103, [**REDACTED**]

 

Sub-Item 000104, [**REDACTED**]

 

Sub-Item 000105, [**REDACTED**]

 

Sub-Item 000106, [**REDACTED**]

 

5. All deliverables shall be unclassified and shall carry the NextView license.

 

6. The Government will incrementally fund this Item, as such, no legal liability on the part of the Government for any payment or on the part of the Contractor for any performance under any requirement placed under this Item may arise until funds are made available by the Contracting Officer for such requirement and until the Contractor receives notice of such availability in writing from the Contracting Officer.

 

Award Type: Cost

Total Estimated Cost:                 [**REDACTED**]

CLIN VALUE [**REDACTED**]

Product/Service Code: 7640

Product/Service Description: MAPS, ATLASES,

CHARTS, & GLOBES

 

Period of Performance: 09/15/2011 to 09/14/2012

 

Change Item 000101 to read as follows (amount shown is the obligated amount):

 

FG Layer – [**REDACTED**]

 

            [**REDACTED**]
000101    Continued …            

 

NSN 7540-01-152-8067   

OPTIONAL FORM 336 (4-86)            

Sponsored by GSA

FAR (48 CFR) 53.110

UNCLASSIFIED


UNCLASSIFIED

 

CONTINUATION SHEET    REFERENCE NO. OF DOCUMENT BEING CONTINUED   

PAGE    OF

5        |        10

   HM021010C0002/0002/01   

NAME OF OFFEROR OR CONTRACTOR

DIGITALGLOBE, INC.

         

 

ITEM NO.

(A)

  

SUPPLIES/SERVICES

(B)

   QUANTITY
(C)
   UNIT
(D)
   UNIT PRICE
(E)
   AMOUNT
(F)
  

Award Type: Cost

Total Estimated Cost:             [**REDACTED**]

CLIN VALUE [**REDACTED**]

Incrementally Funded Amount:     [**REDACTED**]

Product/Service Code: 7640

Product/Service Description: MAPS, ATLASES, CHARTS, & GLOBES

 

Period of Performance: 09/15/2011 to 09/14/2012

 

Change Item 0002 to read as follows (amount shown is the obligated amount):

           
0002   

Enhanced GEOINT Delivery - Image Strip Layer:

[**REDACTED**] This item also includes expenses associated with the dissemination of imagery and image products on media.

 

1. The contractor shall provide all personnel, materials, facilities and equipment to complete this requirement.

 

2. This Item is an Indefinite Quantity Cost Item. The sum of all products invoiced for under this Item shall not exceed $ [**REDACTED**] . The Government COR or the EGD Technical POC will identify areas to be produced.

 

3. The contractor shall invoice for the basis image strip imagery product delivered under this item at the fixed rate of $ [**REDACTED**] .

 

Additional associated product pricing shall be invoiced at the rates in the Attachment entitled EGD Product Price List.

 

4. When invoicing, the contractor shall segregate and cite the following specific Accounting Classification Reference Numbers

 

Continued …

            [**REDACTED**]

 

NSN 7540-01-152-8067   

OPTIONAL FORM 336 (4-86)            

Sponsored by GSA

FAR (48 CFR) 53.110

UNCLASSIFIED


UNCLASSIFIED

 

CONTINUATION SHEET    REFERENCE NO. OF DOCUMENT BEING CONTINUED   

PAGE    OF

6        |        10

   HM021010C0002/0002/01   

NAME OF OFFEROR OR CONTRACTOR

DIGITALGLOBE, INC.

         

 

ITEM NO.

(A)

  

SUPPLIES/SERVICES

(B)

  

QUANTITY

(C)

  

UNIT

(D)

  

UNIT PRICE

(E)

  

AMOUNT

(F)

  

(ACRN) for deliveries associated with the following countries by the indicated informational Sub-Item numbers:

 

Sub-Item 000201, [**REDACTED**]

 

Sub-Item 000202, [**REDACTED**]

 

Sub-Item 000203, [**REDACTED**]

 

Sub-Item 000204, [**REDACTED**]

 

Sub-Item 000205, [**REDACTED**]

 

Sub-Item 000206, [**REDACTED**]

 

5. All deliverables shall be unclassified and shall carry the NextView license.

 

6. The Government will incrementally fund this Item, as such, no legal liability on the part of the Government for any payment or on the part of the Contractor for any performance under any requirement placed under this Item may arise until funds are made available by the Contracting Officer for such requirement and until the Contractor receives notice of such availability in writing from the Contracting Officer.

 

Award Type: Cost

Total Estimated Cost:             [**REDACTED**]

CLIN VALUE [**REDACTED**]

Product/Service Code: 7640

Product/Service Description: MAPS, ATLASES,

CHARTS, & GLOBES

 

Period of Performance: 09/15/2011 to 09/14/2012

 

Change Item 000201 to read as follows (amount shown is the obligated amount):

 

Image Strip Layer - [**REDACTED**]

Award Type: Cost

           
000201   

Total Estimated Cost:             [**REDACTED**]

CLIN VALUE [**REDACTED**]

Incrementally Funded Amount:     [**REDACTED**]

Product/Service Code: 7640

Product/Service Description: MAPS, ATLASES, CHARTS, & GLOBES

 

Period of Performance: 09/15/2011 to 09/14/2012

 

Change Item 0003 to read as follows (amount shown is the obligated amount):

 

Continued …

            [**REDACTED**]

 

NSN 7540-01-152-8067   

OPTIONAL FORM 336 (4-86)            

Sponsored by GSA

FAR (48 CFR) 53.110

UNCLASSIFIED


UNCLASSIFIED

 

CONTINUATION SHEET    REFERENCE NO. OF DOCUMENT BEING CONTINUED   

PAGE    OF

7        |        10

   HM021010C0002/0002/01   

NAME OF OFFEROR OR CONTRACTOR

DIGITALGLOBE, INC.

         

 

ITEM NO.

(A)

  

SUPPLIES/SERVICES

(B)

  

QUANTITY

(C)

  

UNIT

(D)

  

UNIT PRICE

(E)

  

AMOUNT

(F)

0003   

Enhanced GEOINT Delivery - Rapid Response Ortho

(RRO) Service: [**REDACTED**] This item also includes expenses associated with the dissemination of imagery and image products on media.

 

1. The contractor shall provide all personnel, materials, facilities and equipment to complete this requirement.

 

2. This Item is an Indefinite Quantity Cost Item. The sum of all products invoiced for under this Item shall not exceed [**REDACTED**] . The Government COR or the EGD Technical POC will identify areas to be produced.

 

3. The contractor shall invoice for products delivered under this item using the RRO pricing list in the Attachment entitled EGD Product Price List.

 

4. When invoicing, the contractor shall segregate and cite the following specific Accounting Classification Reference Numbers (ACRN) for deliveries associated with the following countries by the indicated informational Sub-Item numbers:

 

Sub-Item 000301, [**REDACTED**]

 

Sub-Item 000302, [**REDACTED**]

 

Sub-Item 000303, [**REDACTED**]

 

Sub-Item 000304, [**REDACTED**]

 

Sub-Item 000305, [**REDACTED**]

 

Sub-Item 000306, [**REDACTED**]

 

5. All deliverables shall be unclassified and shall carry the NextView license.

 

The Government will incrementally fund this

 

Continued …

            [**REDACTED**]

 

NSN 7540-01-152-8067   

OPTIONAL FORM 336 (4-86)            

Sponsored by GSA

FAR (48 CFR) 53.110

UNCLASSIFIED


UNCLASSIFIED

 

CONTINUATION SHEET    REFERENCE NO. OF DOCUMENT BEING CONTINUED   

PAGE    OF

8        |        10

   HM021010C0002/0002/01   

NAME OF OFFEROR OR CONTRACTOR

DIGITALGLOBE, INC.

         

 

ITEM NO.

(A)

  

SUPPLIES/SERVICES

(B)

  

QUANTITY

(C)

  

UNIT

(D)

  

UNIT PRICE

(E)

  

AMOUNT

(F)

  

Item, as such, no legal liability on the part of the Government for any payment or on the part of the Contractor for any performance under any requirement placed under this Item may arise until funds are made available by the Contracting Officer for such requirement and until the Contractor receives notice of such availability in writing from the Contracting Officer.

 

Award Type: Cost

Total Estimated Cost:             [**REDACTED**]

CLIN VALUE [**REDACTED**]

Product/Service Code: 7640

Product/Service Description: MAPS, ATLASES,

CHARTS, & GLOBES

 

Period of Performance: 09/15/2011 to 09/14/2012

 

Change Item 000301 to read as follows (amount shown is the obligated amount):

           
000301   

RRO - [**REDACTED**]

Award Type: Cost

Total Estimated Cost:             [**REDACTED**]

CLIN VALUE [**REDACTED**]

Incrementally Funded Amount:     [**REDACTED**]

Product/Service Code: 7640

Product/Service Description: MAPS, ATLASES, CHARTS, & GLOBES

 

Period of Performance: 09/15/2011 to 09/14/2012

 

Change Item 0004 to read as follows (amount shown is the obligated amount):

            [**REDACTED**]
0004   

Enhanced GEOINT Delivery, LongView Support - [**REDACTED**]

 

Continued …

            [**REDACTED**]

 

NSN 7540-01-152-8067   

OPTIONAL FORM 336 (4-86)            

Sponsored by GSA

FAR (48 CFR) 53.110

UNCLASSIFIED


UNCLASSIFIED

 

CONTINUATION SHEET    REFERENCE NO. OF DOCUMENT BEING CONTINUED   

PAGE    OF

9        |        10

   HM021010C0002/0002/01   

NAME OF OFFEROR OR CONTRACTOR

DIGITALGLOBE, INC.

         

 

ITEM NO.

(A)

  

SUPPLIES/SERVICES

(B)

  

QUANTITY

(C)

  

UNIT

(D)

  

UNIT PRICE

(E)

  

AMOUNT

(F)

  

[**REDACTED**]. This item also includes expenses associated with the dissemination of imagery and image products on media.

 

1. The contractor shall provide all personnel, materials, facilities and equipment to complete this requirement.

 

2. This Item is an Indefinite Quantity Cost Item. The sum of all products invoiced for under this Item shall not exceed [**REDACTED**] . The Government COR or the EGD Technical POC will identify areas to be produced.

 

3. The contractor shall invoice for any product delivered under this item at the fixed rate based on the level of daily take delivered under this item using the pricing list in the Attachment entitled EGD Product Price List, including delivery expenses, which are incorporated into the sqnmi price.

 

4. All deliverables shall be unclassified and shall carry the NextView license.

 

5. This item is subject to the availability of funds. As such, the Government will incrementally fund this Item, as such, no legal liability on the part of the Government for any payment or on the part of the Contractor for any performance under any requirement placed under this Item may arise until funds are made available by the Contracting Officer for such requirement and until the Contractor receives notice of such availability in writing from the Contracting Officer.

 

Award Type: Cost

Total Estimated Cost:             [**REDACTED**]

CLIN VALUE [**REDACTED**]

Incrementally Funded Amount:     [**REDACTED**]

Product/Service Code: 7640

 

Continued …

           

 

NSN 7540-01-152-8067   

OPTIONAL FORM 336 (4-86)            

Sponsored by GSA

FAR (48 CFR) 53.110

UNCLASSIFIED


UNCLASSIFIED

 

CONTINUATION SHEET    REFERENCE NO. OF DOCUMENT BEING CONTINUED   

PAGE    OF

10        |        10

   HM021010C0002/0002/01   

NAME OF OFFEROR OR CONTRACTOR

DIGITALGLOBE, INC.

         

 

ITEM NO.

(A)

  

SUPPLIES/SERVICES

(B)

  

QUANTITY

(C)

  

UNIT

(D)

  

UNIT PRICE

(E)

  

AMOUNT

(F)

  

Product/Service Description: MAPS, ATLASES, CHARTS, & GLOBES

 

Accounting Info:

TBD

[**REDACTED**] (Subject to Availability of Funds)

Period of Performance: 09/15/2011

           

 

NSN 7540-01-152-8067   

OPTIONAL FORM 336 (4-86)            

Sponsored by GSA

FAR (48 CFR) 53.110

UNCLASSIFIED


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

UNCLASSIFIED

National Geospatial-Intelligence Agency

Imagery and Production Services

Statement of Work

Enhanced GEOINT Delivery (EGD)

21 October 2011

1.0 Scope

[**REDACTED**]

2.0 Background

[**REDACTED**]

3.0 Production Requirements

[**REDACTED**]

 

 

SOW Enhanced GEOINT Delivery 21 October 2011    Page 1 of 12

UNCLASSIFIED

UNCLASSIFIED


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

UNCLASSIFIED

[**REDACTED**]

7.0 Web Services

[**REDACTED**]

7.1 Additional Product Requirements

[**REDACTED**]

8.0 LongView Support

 

 

SOW Enhanced GEOINT Delivery 21 October 2011    Page 10 of 12

UNCLASSIFIED

UNCLASSIFIED

Exhibit 10.5.1

FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

Amendment No. 1

to

WorldView 3 Satellite Purchase Agreement #60150

This Amendment No. 1 (“Amendment”) to the WorldView 3 Satellite Purchase Agreement #60150 (the “Agreement”) is entered into by and between DigitalGlobe, Inc. (“DigitalGlobe”), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, Colorado 80503, and Ball Aerospace & Technologies Corp. (“BATC”), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1600 Commerce Street, Boulder, Colorado 80301. As used in this Agreement, “Party” means either DigitalGlobe or BATC, as appropriate, and “Parties” means DigitalGlobe and BATC.

Now, THEREFORE, the parties hereby agree to amend the Agreement to incorporate the following Engineering Change Proposals (“ECP”):

 

1. ECP 001: Document Updates

This change updates three specifications currently under contract. In addition the Payment Milestone Schedule, Exhibit 3, has been updated.

Therefore, this Amendment updates the following documents which are provided as Attachments 1-4 to the Agreement.

 

  a. Exhibit 1 to the Agreement, titled “Statement of Work for the WorldView 3 Satellite — 10329656, Initial Release,” and dated 23 August 2010, is replaced in its entirety by the updated version “Statement of Work for the WorldView 3 Satellite — 10329656, Rev 1.0,” dated 7 February 2011, included as Attachment 1 to this Amendment; and

 

  b. Exhibit 2 to the Agreement, titled “DigitalGlobe WorldView 3 Satellite Specification — 10329655, Rev 1.0,” and dated 20 August 2010, is replaced in its entirety by the updated version “DigitalGlobe WorldView 3 Satellite Specification — 10329655, Rev 4.0”, dated 2 February 2011, included as Attachment 2 to this Amendment; and

 

  c. Exhibit 3 to the Agreement, titled “WorldView 3 Payment Milestone Schedule — 10329669, Initial Release,” and dated 7 September 2010, is replaced in its entirety by the updated version “WorldView 3 Payment Milestone Schedule, Rev — 10329669, Rev 1.0,” dated 11 February 2011, included as Attachment 3 to this Amendment; and

 

  d. “WV2 Spacecraft Simulator Specification — WV901, Rev 2.0”, and dated 11 Feb 2009, is replaced in its entirety by the document “WV3 Spacecraft Simulator Specification — 10258368, Initial Release”, dated 20 December 2010, included as Attachment 4 to this Amendment.

 

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


2. ECP 002: Purchase of [**Redacted**]

DigitalGlobe desires to purchase [**Redacted**] .

Rev 1.0 of the Statement of Work (SOW) contains the updates to reflect this new work. The updates are listed in section 3.1.o.

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**] .

 

3. ECP 003: Purchase of [**Redacted**]

DigitalGlobe desires to purchase a [**Redacted**] .

Rev 1.0 of the Statement of Work (SOW) contains the updates to reflect this new work. The updates are listed in section 3.1.n.

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**] .

 

4. ECP 004: Change to [**Redacted**]

DigitalGlobe desires to change [**Redacted**] .

Rev 4.0 of the Satellite Specification contains the updates to reflect this new work. The updates are listed in section 3.2.1.7.7.2.7.

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**] .

 

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


5. ECP 005: Enhancements to WV3 Spacecraft Simulator

DigitalGlobe desires to upgrade the functionality on the WV3 Spacecraft Simulator. [**Redacted**]

Rev 1.0 of the Statement of Work (SOW) contains the updates to reflect this new work. The updates are listed in sections 3.1.b, 13.8.1, and Attachment 1. The Initial release of the WV3 Satellite Simulator Specification identifies the items [**Redacted**] .

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**] .

 

6. ECP 006: Upgrade to [**Redacted**]

DigitalGlobe desires to upgrade the [**Redacted**]

The upgrade shall encompass the following: [**Redacted**]

Rev 4.0 of the Satellite Specification contains the updates to reflect this new work. The updates are listed in section 3.2.1.7.7.1.7. Task Order 79 to Agreement 9206-0117 contains the testing methodology for the [**Redacted**] .

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**] .

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


7. ECP 007: [**Redacted**]

As part of the contract with ITT, DigitalGlobe shall be adding a [**Redacted**] .

BATC shall perform the following tasks in support of the [**Redacted**] .

Ball shall also perform the following: [**Redacted**] .

Rev 4.0 of the Satellite Specification contains the updates to reflect this new work. The updates are listed in section 3.1.3.1.7.

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**] .

SUMMARY

The value for these ECPs is $3,677,399.00, outlined in the following table:

 

Change #

  

Change Description

   $  

001

  

Document Updates

   $ 0.00   

002

  

[**Redacted**]

     [**Redacted**]   

003

  

[**Redacted**]

     [**Redacted**]   

004

  

Change to [**Redacted**]

     [**Redacted**]   

005

  

[**Redacted**] WV3 Simulator

     [**Redacted**]   

006

  

Upgrade to [**Redacted**]

     [**Redacted**]   

007

  

[**Redacted**]

     [**Redacted**]   
     

 

 

 
  

TOTAL

   $ 3,677,399.00   
     

 

 

 

 

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


Contract Value Summary

 

Previous Contract Value

   $ 180,575,000.00   

ECPs

   $ 3,677,399.00   

New Contract Value

   $ 184,242,399.00   

All other terms and conditions of the Agreement not noted as changed herein shall remain in full force and effect.

This Amendment No. 1 is agreed to by DigitalGlobe and BATC and shall be binding and effective as of the last date executed below.

 

Ball Aerospace & Technologies Corp.    Digital Globe, Inc.
[**Redacted**]   

/s/ Neal T. Anderson

   VP, Tech. Development
2/25/11    3/2/11

 

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


Attachment 1

Statement of Work for the WorldView 3 Satellite, Rev 1.0

Dated 7 February 2011

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

 

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Exhibit 1 to Agreement 60150

Statement of Work

for the WorldView 3

Satellite

 

 

 

   Document Number    10329656
   Release Date:    Feb 7, 2011
   Issue/Revision:    Release 1.0
   Prepared by:    Brian Uzzle
   Approved by    Steve Linn

RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION

This document contains information proprietary and confidential to DigitalGlobe Incorporated, to its subsidiaries, or to a third party to whom DigitalGlobe Incorporated may have a legal obligation to protect such information from unauthorized disclosure, use or duplication. Any disclosure, use or duplication of this document or of any of the information contained herein for other than the specific purpose for which it was disclosed is expressly prohibited, except as DigitalGlobe Incorporated may otherwise agree to in writing. This document may only be used for the purpose for which it is provided. All copies of this document are the sole property of DigitalGlobe and will be returned promptly upon request.

 

 

 

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Change Record

 

Issue

  

Date

  

Section(s)

  

Description of Change

Initial    20 Aug 2010       Initial Release
Rev 1    7 Feb 2011    2.1    Updated references for Satellite Specification, Satellite Simulator Specification, and Instrument Specification
      3.1.b    Updated dates for Satellite Simulator releases and number of deliveries
      3.1.n    Added deliverable item [**Redacted**]
      3.1.o    Added deliverable item [**Redacted**] .
      13.8.1    Clarified WV3 simulator changes versus WV2 simulator [**Redacted**] .
      Attachment 1    Updated release dates for Satellite Simulator (LM-8), Satellite Simulator Documentation (LM-9), and Satellite Simulator Source Code (LM-10).
      Attachment 1    Updated [**Redacted**] (CFHW-1)
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        

 

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Issue

  

Date

  

Section(s)

  

Description of Change

        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        

 

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1.0 INTRODUCTION

This Statement of Work defines those tasks to be performed by BATC, the Space Segment Integrator, in defining; designing, producing, testing, verifying, and preparing for launch; the DigitalGlobe WorldView 3 Satellite. BATC has the overall responsibility for Satellite performance, as defined in the WV3 Satellite Specification, provided the DG-furnished Instrument meets its interfaces and specifications as defined in Paragraph 2.2. Within this role, BATC has the responsibility to work with DigitalGlobe to define requirements, allocate budgets, analyze performance, execute trade studies, interact with other vendors, define configurations(s), conform to existing Instrument interfaces, assess and mitigate risks, prepare various programmatic documentation, and interact with all participating organizations via meetings, teleconferences, and reviews as defined herein.

BATC shall provide integrating services as defined herein and the hardware and software, exclusive of Customer Furnished Equipment, that comprise the WV3 Satellite.

This document also defines the scope of work required from DigitalGlobe and associated subcontractors in order for BATC to execute this contract successfully.

Associate contractors under contract to DigitalGlobe shall provide the Instrument and Launch services. However, BATC shall fully support defining, documenting, and verifying Satellite(s) to LV and MGB interfaces and integration procedures. BATC shall insure that the Satellite will withstand all launch environments.

 

1.1 Definitions

Agreement: Satellite Purchase Agreement #60150 by and between DigitalGlobe, Inc. and Ball Aerospace and Technologies Corp., dated August 27, 2010, as amended.

Authorization to Proceed (ATP): Effective date of work commencement per the Agreement.

Satellite: The complete space-borne infrastructure required to perform the mission of providing radiometrically and geometrically correct imagery of the Earth. The Satellite consists of the Instrument and the Spacecraft Bus.

Instrument: The Instrument is that part of the Satellite that collects light photons using appropriate mirrors and structure, [**Redacted**] . It also may be designated the Electro-Optical Assembly (EOA). The instrument includes it’s own thermal control system. However, the instrument focus mechanism depends upon drive electronics to be provided by BATC per this Statement of Work. Also, the instrument stimulation lamp depends upon drive electronics to be provided by BATC per this Statement of Work.

Telescope: That part of the Instrument that collects and focuses light onto a focal plane. [**Redacted**] It also may be designated the Optical Telescope Unit (OTU).

Sensor Subsystem (SSS): That part of the Instrument that converts photons to analog voltage signals, [**Redacted**] , and digitizes [**Redacted**] those signals.

Solid State Recorder: The subsystem that accepts digital data from the SSS and Ancillary Data from the spacecraft bus, provides storage, [**Redacted**] and outputs that data to the wideband transmitter(s).

 

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Spacecraft Bus: The Bus is that part of the Satellite that provides the support infrastructure so the Instrument can function.

[**Redacted**]

MGB: “MGB” is a meaningless three letter designation for an additional subsystem being installed on the WV3 satellite. The MGB subsystem consists of three components. The first is a Sensor Unit (SU) which will attach to the aperture end of the OBA. The second is the Interface Adaptor Unit (IAU) which will mount to the spacecraft bus. The third is an inter-connect cable which connects the first two units.

Initial Acceptance: Occurs upon successful completion of the Satellite Pre-Ship Review as defined in paragraph 4.5.3.2.e

Final Acceptance: Occurs following satellite fueling operations and completion of the Satellite Launch Readiness Review as defined in paragraph 4.5.3.2.f

Transfer of Title: Occurs as defined in the Satellite Purchase Agreement paragraph 8.

 

1.2 Program Overview

Under this Scope of Work, DigitalGlobe will procure one satellite to support the EnhancedView program and future commercial operations. DigitalGlobe shall provide the Instrument as Customer Furnished Equipment via a procurement contract with ITT. DigitalGlobe shall provide the “MGB” subsystem. As on the WV2 program, BATC shall deliver a WorldView 2 like stimulation lamp that will be incorporated into the ITT provided instrument. BATC shall also incorporate into the Bus, an instrument focus mechanism electronics capability.

DigitalGlobe shall provide the Launch Services via a procurement contract with Boeing Launch Services (TBD). It is assumed that Boeing Launch Services will in-turn subcontract with United Launch Alliance to provide the Delta 2 launch vehicle and associated launch services. BATC can assume a Delta 2 launch vehicle and a launch from Vandenberg Air Force Base. BATC shall assume satellite processing at Vandenberg AFB will occur in either the Astrotech Payload Processing facility or the Spaceport Systems International (BATC) Processing Facility.

 

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2.0 DOCUMENTS

 

2.1 Applicable Documents

This Statement-of-Work identifies applicable documents. These documents provide detailed requirements regarding Satellite performance, interfaces, and/or standardized design, fabrication, and testing processes/procedures. BATC and DigitalGlobe will perform the defined work according to these standardized processes/procedures such that the delivered products meet the performance and ICD requirements.

In the event of any conflict between these documents, the following order of precedence shall prevail: a) Agreement Terms & Conditions; b) Statement of Work; c) Satellite Specification; d) Other Applicable documents.

 

DigitalGlobe Produced or Provided Documents   

WV3 Satellite Specification

   [**Redacted**]

WV3 Spacecraft Simulator Specification

   [**Redacted**]

WV3 Command & Telemetry Handbook Specification

   [**Redacted**]

WV3 Maneuver Planner Specification

   [**Redacted**]

MGB Data Protection Plan for BATC

   [**Redacted**]

Stim Lamp and Stim Lamp Electronics Specification

   [**Redacted**]

[**Redacted**] Focus Mechanism Electronics Specification

   [**Redacted**]

Star Tracker Simulation Specification

   [**Redacted**]

IRU Simulator Specification

   [**Redacted**]

SSR to DPU Cable Design and Build Documentation

   [**Redacted**]
BATC Produced Documents   

BATC Product Assurance Plan

   [**Redacted**]

BATC Supplier Product Assurance Plan

   [**Redacted**]

BATC Document Control Procedure

   [**Redacted**]

BATC Configuration and Data Management Plan

   [**Redacted**]
Associated Contractor Produced Documents   

Astrotech Vandenberg Facility Accommodations Manual

   [**Redacted**]

Spaceport Systems International, Vandenberg Facility Accommodation Manual

   [**Redacted**]

 

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2.2 Reference Documents

The following documents provide the baseline instrument definition. DigitalGlobe shall provide an instrument that is compliant with these documents.

 

DigitalGlobe Produced or Provided Documents   

Instrument Specification

   [**Redacted**]

Instrument Finite Element Model

   [**Redacted**]

 

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3.0 CONTRACT DELIVERABLES

 

3.1 Deliverable Items

 

  a. WV3 Satellite: Initial Acceptance: [**Redacted**] . Final Acceptance: [**Redacted**] Delivery shall be adjusted for Excusable Delay or failure of customer to [**Redacted**] to the extent that these delays affect the Delivery Date.

 

  b. WV3 Satellite Simulator

Initial release: [**Redacted**]

Simulator Delivery [**Redacted**]

Functional and performance signoff: [**Redacted**]

On orbit performance/tuning update: [**Redacted**]

 

  c. [**Redacted**]

 

  d. [**Redacted**]

 

  e. [**Redacted**]

 

  f. [**Redacted**]

 

  g. [**Redacted**]

 

  h. [**Redacted**]

 

  i. [**Redacted**]

 

  j. [**Redacted**]

 

  k. [**Redacted**]

 

  l. [**Redacted**]

 

  m. [**Redacted**]

 

  n. [**Redacted**]

 

  o. [**Redacted**]

 

3.2 Deliverable Data

Reference Attachment 1: Contractor Data Items List (CDIL)

 

3.3 Deliverable Services

 

  a. Storage and Delivery (Section 11.0)

 

  b. Launch Support (Section 12.0)

 

  c. Mission, Commissioning, & Readiness Support (Section 13.0)

 

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4.0 PROGRAM MANAGEMENT

 

4.1 Program Philosophy

Emphasis throughout all phases and functions of the project shall be to produce a reliable Satellite that meets the performance requirements on the contracted schedule. [**Redacted**]

 

4.2. BATC Organization (CDIL PM-1)

A dedicated Program Manager shall be appointed by BATC prior to the start of the contract. The Program Manager shall lead all of the Contractor’s activities under the contract.

A diagram illustrating the Program Management Structure shall be provided to DigitalGlobe. (CDIL PM-1) This diagram(s) shall indicate job titles and names of the program management team.

The Program Manager shall coordinate changes to contract conditions, price, timescale, deliverables, services or performance levels, unless a specific alternate has been appointed to deal with any of these matters. All changes to the contract documents shall require the written agreement of BATC contracts representative.

BATC shall also appoint a different and dedicated individual to be a single point of contact for each of the following:

 

  a. Program technical management (Satellite System Engineer)

 

  b. Instrument System Engineer

 

  c. Project Engineer Quality Assurance (PEQA)

 

  d. Program Integration and Test management

BATC shall appoint a different individual to be a single point of contact for each of the following:

 

  e. Various Bus Subsystem Lead Engineers

 

  f. Launch Vehicle Integration Engineer

 

  g. Program Contract Management

These individuals are key personnel and, if performing well, should remain unchanged for the duration of the program.

BATC shall appoint a Satellite Simulator Project Lead. This individual will be the technical lead for the Satellite Simulator development effort and will be responsible for meeting its technical and schedule guidelines established herein.

 

4.3 DigitalGlobe Management

DigitalGlobe will appoint a Program Manager who as an individual shall act as DigitalGlobe’s primary point of contact on all program management matters. As required, according to the activity and phase of the contract, the Program Manager will nominate specific individuals to interface directly with BATC.

The DigitalGlobe Program Manager shall coordinate changes to contract conditions, price, timescale, deliverables, services or performance levels, unless a specific alternate has been appointed to deal with any of these matters. All changes to the contract documents shall require the written agreement of the DigitalGlobe contracts representative.

 

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DigitalGlobe will also appoint a responsible individual(s) to be a single point of contact for each of the following.

[**Redacted**]

BATC shall permit direct engineering interactions between these DG individuals and their BATC counterparts.

 

4.4 Space Segment Master Program Schedule (MPS) (CDIL PM-2)

BATC shall develop maintain, and provide a Master Program Schedule (MPS) for the entire program including hardware, software, analyses, data item deliverables, and subcontractor activities for all phases of the program including design, integration, test, and shipment through final acceptance.

 

4.4.1 General

The MPS shall consist of a computer supported dependency network, each element of which shall represent a single program event. Each event shall be attributed a start and finish date. The network must clearly show the interdependency in terms of both time and function amongst the events.

The MPS shall be the major management tool for planning, monitoring and controlling the program, in terms of:

 

  a. Planning the program, monitoring progress, documenting actual activity accomplishment and actual durations.

 

  b. Predicting future progress.

 

  c. Identification of significant milestones e.g. review meeting.

 

  d. Identification of the time critical path.

 

  e. Reflecting actual progress and changes relative to baseline plan.

 

4.4.2 Required Software

The Contractor shall create and maintain the network using Microsoft Project (Version 2003). Schedules of a detailed nature shall be provided electronically on a monthly basis. A hardcopy shall also be provided on request.

 

4.4.3 MPS Construction

Content

The network shall be constructed against the following major classifications:

 

  a. Deliverable hardware down to component level

 

  b. Software development activities

 

  c. Facilities required to support the production of any of the deliverables

 

  d. Other events/items required to support the production of the deliverables or services. e.g. test aids, test software prototypes, etc.

 

  e. Customer Furnished Equipment required from DigitalGlobe

 

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Individual items in each class shall be considered to consist of a number of generic events. These events shall typically consist of such activities as:

 

  a. Plan

 

  b. Design & develop

 

  c. Manufacture

 

  d. Assemble

 

  e. Integrate

 

  f. Test

 

  g. Deliver

 

  h. Reviews

However steps may be omitted or added given unit specific circumstances.

Unique Identifiers

The MPS shall include a unique identifying number for each task. This will more easily allow DigitalGlobe to combine certain tasks into a DigitalGlobe Master Schedule. Unique identifiers will not be deleted, reused, or re-assigned to other tasks.

 

4.4.4 Reports

The MPS shall be capable of generating a number of different types of reports upon demand. All events and milestones shall be coded to permit a variety of sort options to be exercised without program modification. Both GANTT and network form shall be supported.

 

4.5 Meetings & Reviews

BATC shall support the meetings and reviews listed in the following paragraphs.

 

4.5.1 Weekly Status Meeting

BATC Program Manager shall support a weekly meeting/telecon with the DigitalGlobe Program Manager to review program status including schedule, technical, risk register, action item list, and subcontracts.

 

4.5.2 Monthly Program Status Review

BATC Program Manager shall support a monthly Program Status Review with DigitalGlobe.

 

4.5.3 Program Reviews

List of Formal Reviews

BATC will host and conduct formal reviews at the following program milestones. BATC shall prepare charts, viewgraphs, analysis results, trade study results, etc. in the quantity and quality typical of aerospace industries reviews.

 

  a. Satellite Requirements Review (SRR) (CDIL D-34) ) Only changes between WV2 and WV3 must be reviewed.

 

  b. Delta - Preliminary Design Review (PDR) (CDIL D-30) Only changes between WV2 and WV3 must be reviewed.

 

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  c. Delta-Critical Design Review (CDR) (CDIL D-31) Only changes between WV2 and WV3 must be reviewed.

 

  d. Spacecraft Bus Complete/Instrument Integration Readiness Review (IRR) (CDIL – PT-8)

 

  e. Satellite Environmental Testing Readiness Review (CDIL – PT-9)

 

  f. Satellite Pre-Ship Review (CDIL PT-10)

 

  g. Launch Readiness Review (CDIL LM-14)

4.5.3.2    Content of Reviews

 

  A. PDR and CDR: BATC shall conduct “delta” reviews. These reviews will document the design changes between WV2 and WV3. These design reviews (PDR and CDR) shall include information and documentation typical of aerospace industry reviews, such as:

 

  1. Satellite mechanical configuration including stowed and deployed views

 

  2. Satellite mechanical configuration including [**Redacted**]

 

  3. Satellite electrical/electronic design, including system block diagram and redundancy scheme

 

  4. Satellite software design

 

  5. Satellite Operating Modes

 

  6. Satellite Fault Detection and Safing

 

  7. Satellite Budgets and Margins

 

  A. Performance relative to specifications

 

  B. Mass

 

  C. Power

 

  D. Thermal

 

  E. Consumables

 

  F. Attitude control: stability, pointing and knowledge

 

  G. RF links

 

  H. Satellite resources: relays, telemetry stream, CPU throughput, processor memory

 

  I. MTF

 

  J. Reliability: Ps, critical items list, cycle-limited items, FMECA

 

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  B. Spacecraft Bus Complete/Instrument Integration Readiness Review: BATC shall host this review. The purpose is to ensure the readiness to begin Instrument integration. This review will cover information including:

 

  1. Instrument Integration procedure and hardware status

 

  2. Status of all Certification Logs for all Ball built hardware that will be integrated to the Bus. Ball shall provide rationale and recovery plan for all certification logs that are open, even though the hardware is complete and ready for integration.

 

  3. TAR and HAR status from the Bus Integration and Test phase

 

  4. Test Team Personnel status, certifications, and time-sharing with other programs

 

  5. Facility status

 

  6. Satellite configuration review

 

  7. Other issues that may impact the timely and successful completion of Instrument integration.

 

  8. The Spacecraft Bus shall be deemed complete and ready for Instrument integration when: [**Redacted**]

 

  C. Satellite Environmental Testing Readiness Review: BATC shall host this review. The purpose is to ensure the readiness to begin satellite level environmental testing which includes but is not limited to: TVAC, EMI/EMC, Vibration, Shock, and Acoustic. This review will cover information including:

[**Redacted**]

 

  D. Satellite Pre-Ship Review: BATC shall host this review. The purpose is to ensure the readiness to ship the satellite to the launch site. This review shall be held after completion of all significant testing and all post-test reviews. The purpose shall be to review the results of the entire Integration & Test program, and demonstrate compliance to the satellite specification., and provide for satellite preliminary acceptance.

The Pre-ship Review shall be deemed satisfactory and the satellite preliminary acceptance by DigitalGlobe complete when the:

[**Redacted**]

 

  F. Satellite Launch Readiness Review: BATC shall conduct a Satellite Launch Readiness Review (SLRR) on or about [**Redacted**] . (Note, the Launch Services Provider, Boeing/ULA also has a review called the Launch Readiness Review. However, that review encompasses the satellite, launch vehicle, weather, and range support.) This SOW paragraph is only concerned with the readiness to launch the satellite. BATC shall review the results of the launch site Integration & Test activities, review any updates to the Verification Matrix, and provide for satellite final acceptance.

 

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The SLRR shall be deemed satisfactory and the satellite final acceptance by DigitalGlobe complete when the:

[**Redacted**]

 

4.5.4 Component/Subsystem Design Review Listing (CDIL PM-3)

BATC shall prepare a summary listing of all planned component (box level) and subsystem design reviews. This listing shall include BATC and vendor provided hardware, and BATC provided software including the satellite simulator and maneuver planner software. This listing shall define the meeting format and required attendance. BATC shall provide a minimum of 10 days advance notice to DigitalGlobe for the following major reviews:

 

  a. System/Subsystem & Component PDRs

 

  b. System/Subsystem & Component CDRs

DigitalGlobe attendance and participation, including support consultants, shall be allowed, but not required at all reviews. The review activity will not be repeated if DigitalGlobe fails to attend.

 

4.5.5 Component/Subsystem Test Readiness / Data Review Listing (CDIL PM-4)

BATC shall prepare a summary listing of all planned component (box level) and subsystem qualification and acceptance test reviews. This listing shall include BATC provided and vendor provided hardware, and BATC provided software. This listing shall define the meeting format and required attendance. BATC shall inform DigitalGlobe of upcoming reviews in a timely manner.

DigitalGlobe attendance and participation shall be allowed, but not required at all reviews. The review activity will not be repeated if DigitalGlobe fails to attend.

 

4.5.6 DigitalGlobe Meetings

DigitalGlobe will arrange separate contracts for the:

 

  a. Launch Vehicle Segment (LV)

 

  b. Instrument

 

  c. Launch and Mission insurance

A series of technical interchange and review meetings will be held with these contractors jointly and separately, as required. BATC shall provide representation at these meetings as needed to resolve interface issues.

In the case of the insurance (c), BATC will provide inputs to formal presentations and support meetings to be held at the DigitalGlobe facility. DigitalGlobe will be responsible for responses to action items using information made available or provided by BATC during the course of the program.

 

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4.6 Documentation Management

 

4.6.1 Access to Program Technical Data

DigitalGlobe will have access rights to all program technical data that BATC generates and Subcontractor data to which BATC has legal and contractual rights. Program technical data may include Engineering Reports, drawings, software source code, and other tools used in the development of the spacecraft and analysis of requirements.

 

4.6.2 Objective

BATC shall establish a control and monitoring process relating to all deliverable documentation and other technical and test data for the complete program. The program shall account for the following:

 

  a. Preparation, review, and formal release as required

 

  b. Changes

 

  c. Storage, backup, and retrieval

 

  d. Distribution

 

Note:   BATC shall include the DigitalGlobe Satellite Integration and Test Point-of-Contact on the distribution list of all relevant WV3 Engineering Reports. (“Relevant” in this clause refers to all ERs containing design information, analyses, test data, etc that affect the performance and/or operations of the satellite. It does not include ERs that contain BATC proprietary cost data.)

 

  e. DigitalGlobe access to all BATC documentation prepared on the project

 

  f. Long term storage for the purpose of through-life product support

As a primary supporting management tool, BATC shall use a secure project server. All data items except memory intensive drawings, test data, production logs, and QA data shall be maintained electronically on the project server. The project shall use the Microsoft Office software suite for word processing, spreadsheets, presentations, and documentation databases.

 

4.6.3 Documentation Listing (CDIL PM-5)

BATC shall develop and maintain a Documentation Listing that identifies all deliverable reports, analyses, drawings, software items, etc., that are developed on the project. The Documentation Listing shall include a naming convention that uniquely identifies the documents for electronic access where applicable. The List shall also indicate spacecraft name, a short title/description of the document, subsystem affected, the latest revision number and date, planned completion date, and status information. The List shall indicate those WV1 and WV2 documents that are also applicable to WV3. Document updates are required to reflect content changes. Document updates are not required if the sole purpose is to reflect applicability to WV3.

 

4.6.4 Documentation Delivery

The Contractor shall deliver document in native formats, e.g. Microsoft Word, Excel, etc., as opposed to PDF except as noted below. DigitalGlobe will identify the delivery location, such as a Microsoft Office Sharepoint Server (MOSS) internet site, and provide Contractor with username and password-controlled access. Documents shall be submitted or made available to DigitalGlobe according to the dates indicated in the list provided in Attachment 1.

 

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In the case of deliverables generated in Microsoft Office, such as Word, Excel, PowerPoint, etc; BATC shall populate the document property fields with the following minimum information: Title, Subject, Author, and key words.

In the case of deliverables that are not generated in MicroSoft Office, such as BATC drawings, .pdf is acceptable and BATC shall populate the property fields of drawings after they are converted to .pdf format.

 

4.7 Action Item Tracking (CDIL PM-6)

BATC shall maintain an Action Item List indicating all significant action items, including those of BATC as well as those of other organizations that relate to interactions with BATC. The Action Item List will be developed and maintained in a format that allows sorting by subsystem, originating party, receiving party, originating date, and closing date. BATC shall be responsible for ensuring closure of those items relating to BATC interactions and interfaces.

 

4.8 Financial Management

BATC shall define a standard set of formats for reporting program financial payment and billing status and shall submit them on a monthly basis. This shall consist of the following:

 

4.8.1 Historical Record of Payments (CDIL PM-7)

This shall consist of a record of the individual payments made, updated on a monthly basis. This record shall be cross-referenced to the payment schedule incorporated in the contract. Payments made in support of contract amendments shall be separately reported and cross-referenced to the payment schedule incorporated in the amendment.

 

4.8.2 Payments Forecast (CDIL PM-7)

This shall consist of a forecast of the future invoices and shall be cross-referenced to the payment schedule incorporated in the contract. Payment milestone forecasts shall be consistent with program progress reported on the Master Program Schedule. NOTE: Record of Payments and Payment Forecast are delivered as a single CDIL item.

 

4.9 Contract Change Control

These are considered to be of three types only:

 

  a. Contract Amendments

 

  b. Waivers: A written authorization granted after contract award to accept an item, that during production, or after having been submitted for inspection or acceptance, is found to depart from contract or specified configuration requirements. Waivers are intended only as one-time departures from an established configuration for specified items or lots and are not intended to be repeatedly used in place of formal engineering changes.

 

  c. Deviations: A written authorization, granted after contract award and prior to the manufacture of the item, to depart from a particular performance or design requirement of a contract, specification, or referenced document, for a specific number of units or a specified period of time. Deviations are intended only as one-time departures from an established configuration for specified items or lots and are not intended to be repeatedly used in place of formal engineering changes.

 

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BATC shall devise a system to control, monitor, and notify DigitalGlobe of these changes. The control system shall include provision for:

 

  a. A unique numbering scheme to track the changes through to completion.

 

  b. Impact upon contract obligation: - price, performance and delivery schedule, with specific identification of the item(s) of hardware, software or documentation affected.

 

  c. Notification of timescale for acceptance or rejection for each change, typically 10 business days.

 

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5.0 DESIGN

 

5.1 General

BATC shall perform the necessary trade studies, preliminary design, and detailed design of the Satellite, exclusive of the Customer Furnished Equipment as defined in Section 10, in accordance with the applicable documents. BATC shall design and procure the Ground Support Equipment necessary to support Satellite Integration and Test activities, except for items defined in Section 10.0. Design activities shall be featured in the program master schedule.

 

5.2 Working Groups and Trade Studies

 

5.2.1 Working Groups

[**Redacted**]

 

5.2.2 Trade Studies

Reserved.

 

5.3 Satellite Design Data

The satellite shall be designed such that the environmental design criteria of the Instrument as defined in the documents of paragraph 2.2 are not exceeded, and the structural, electrical, and thermal characteristics, as defined in the documents of paragraph 2.2, of the Instrument are accommodated.

DigitalGlobe shall provide information required to update the budgets for the Customer Furnished Equipment, consistent with paragraph 2.2.

 

5.3.1 Satellite to Instrument Interface Control Document(s) (CDIL D-1)

BATC shall produce and maintain the Satellite to Instrument ICD(s). The ICD(s) will address all interface issues including but not limited to: power, commanding, telemetry, mass and mass properties, mechanical envelope and mounting, thermal, fields-of-view, vibration and jitter isolation/management, and accommodation of bus components on the Instrument.

 

5.3.2 Satellite to Ground Terminal Narrowband Link ICD (CDIL D-2)

BATC shall produce and maintain the Satellite to Ground Station Narrowband Link ICD. This link will address both the command uplink and telemetry downlink.

 

5.3.3 Satellite to Ground Terminal Wideband Link ICD (CDIL D-3)

BATC shall produce and maintain the Satellite to Ground Terminal Wideband Link ICD.

 

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5.3.4 Satellite Environmental Design and Test Specification (EDTS) (CDIL D-4)

BATC shall prepare and maintain the EDTS, or equivalent document defining the component environmental design and test requirements. Electromagnetic Interference Design and Testing shall be in accordance with the standards specified in Satellite Specification.

 

5.3.5 Contamination Control Plan(s) (CDIL D-5)

[**Redacted**]

 

5.3.6 Satellite Level Requirements Verification/Compliance Matrix (CDIL D-6)

BATC shall produce a satellite level RVCM. The RVCM will include requirements from the Satellite Specification and the Instrument Specification if applicable. BATC shall update/maintain the Satellite RVCM to reflect changes to these parent specifications. DigitalGlobe shall have review and approval authority over changes to the RVCM. BATC shall include the following information in the RVCM

 

  a. Source of requirement (Parent specification document and paragraph number, i.e. satellite spec, instrument spec, etc)

 

  b. Specification paragraph

 

  c. Paragraph title

 

  d. Summary description of requirement

 

  e. Column indicating status of compliance

 

  f. Summary description of performance

 

  g. Responsible organization

 

  h. Verification Point [**Redacted**]

 

  i. Verification Method [**Redacted**]

 

  j. Verification Source Document indicating applicable paragraph, test sheet, etc.

 

  k. Comments, if required.

 

  l. Other information at BATC’s option

 

5.3.7 Box Level Requirements Verification/Compliance Matrix (CDIL D-7)

BATC shall flow down requirements from the Satellite Specification to box level requirements. BATC shall develop performance requirements for each box level component on the Satellite excluding CFE. For this paragraph, “box level component” also includes all components that are not really “box” like. These include but may not be limited to:

[**Redacted**]

BATC shall use the Box Level RVCM as an input into the box level performance test procedures. BATC shall demonstrate compliance to the box level RVCM.

 

5.3.8 Drawings (CDIL D-8)

A complete file of BATC drawings prepared for the WV3 program, will be maintained on file in electronic and hardcopy form, where appropriate. Electronic transfer to DigitalGlobe will constitute delivery.

 

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5.3.9 Performance Compliance and Risk Management

 

5.3.9.1    Performance Compliance (CDIL D-9)

The contractor shall supply at PDR a Performance Compliance Matrix identifying the performance estimate, allocated uncertainty (and/or contingency as appropriate) and resulting Total Performance (where Total Performance = performance estimate + uncertainty) for the following list. The Performance Compliance Matrix shall be updated and provided with each Quarterly Review following the PDR.

[**Redacted**]

DigitalGlobe shall provide performance information required to update the budgets for any of the Customer Furnished Equipment, in accordance with the documents in Paragraph 2.2.

5.3.9.2    Risk Management Report (CDIL D-10)

BATC and DigitalGlobe shall jointly develop and maintain a Risk Status Report. This report highlights known program risks, assigns risk levels, and documents mitigation strategies and status. BATC shall supply at PDR an initial Risk Status Report covering the system elements to be provided by this SOW. BATC shall updated the Risk Status Report monthly following the PDR.

5.3.10    Subsystem Description Documents (CDIL D-11)

BATC shall prepare Subsystem Description Documents for each satellite subsystem.

The Subsystem Description Documents will include as a minimum, unless provided in other deliverable documents, and referenced in the SDD:

 

a. Subsystem Overview including a detailed block diagram

 

b. Functionality and major performance characteristics of each Subsystem Component

 

c. Redundancy

[**Redacted**]

 

d. [**Redacted**]

 

e. [**Redacted**]

 

f. [**Redacted**]

 

g. Subsystem schematic including power, power returns, commands, and telemetry. This schematic shall be updated to reflect Engineering Change Orders.

 

h. Expected nominal operating methods and telemetry limits

[**Redacted**]

 

i. Operational constraints

[**Redacted**]

 

j. Fault Protection

[**Redacted**]

j.2 List the information available to the operator to reconstruct or identity the fault.

 

k. Interfaces between subsystem components

 

l. Major interfaces with other subsystems

The Subsystem Description Documents shall be delivered at CDR + 4 months. If changes require an update to the document, those updates shall be provided at approximately Launch – 4 months and again at Launch + 4 months. The subsystem schematic (item e.) shall be updated as required throughout the program to reflect Engineering Change Orders.

 

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5.3.11    Analysis and reports

BATC shall perform the following analyses. Updates shall be provided when changes significantly invalidate previous results.

 

  a. (1) Integrated Spacecraft Bus/Instrument thermal analyses, including summary of temperature predictions for unit level components under various operational modes and (2) unit-level thermal analysis [**Redacted**] . (CDIL D-12)

 

  b. Integrated Spacecraft Bus/Instrument structural analysis including [**Redacted**] . (CDIL D-13)

 

  c. Control system analysis including [**Redacted**]. (CDIL D-14)

 

  d. System Level Failure Modes and Effects and Criticality Analysis (FMECA). [**Redacted**] (CDIL D-15)

 

  e. Satellite Reliability Analysis BATC shall calculate satellite reliability using it’s standard process. [**Redacted**] (CDIL D-16)

 

  f. Satellite Life Prediction Data. DigitalGlobe needs to continually assess expected satellite life based upon actual on-orbit operational parameters. BATC shall provide all backup data used by BATC for sizing and life predictions. BATC does not need to produce a life expectancy analysis. DigitalGlobe will use the provided data and make our own Life Prediction. BATC can provide the life prediction data in one summary package, or in other CDILs.

 

  g. Flight Battery Life Prediction Analysis. BATC shall produce a life expectancy analysis for the satellite battery. The battery life prediction shall account for ground handling and will include a family of curves based upon pertinent on-orbit variables including but not necessarily limited to temperature and depth-of-discharge. (CDIL D-35)

 

  h. Satellite Imaging Performance (CDIL D-17)

BATC shall perform a comprehensive analysis regarding imaging performance. This is a comprehensive look at the numerous subsystem and trans-subsystem performance measures that affect imaging. The list includes but is not limited to:

[**Redacted**]

5.3.12    Other Interface Control Documents

BATC shall provide inputs, review, and verify BATC side of the following ICDs.

 

  a. Satellite to Launch Vehicle ICD

In the event that the ICDs require revision, the changes will be discussed between the affected parties to determine the most cost and schedule efficient manner to implement the change. If applicable, any impact will be covered under changes provision of the Contract.

 

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5.3.13    Critical Items list (CDIL D-18)

BATC shall maintain a Critical Items List summarizing all known single point failures on the Satellite and any special efforts required to mitigate risk associated with them. It shall also contain any items requiring special handling due to a high potential of damage, mission criticality, or safety concerns.

5.3.14    Component Heritage Summary (CDIL D-19)

The Component Heritage Summary will consist of a listing of all Satellite units by subsystem summarizing:

 

  a. Unit name

 

  b. Development / qualification history (e.g. engineering model, qual, protoflight)

 

  c. Previous flight heritage

 

  d. Modifications to previous uses

 

  e. Any significant known anomalies on flight units

5.3.15    Engineering Reports (CDIL D-20)

A complete file of all relevant Engineering Reports prepared on the WV3 program funding shall be maintained on file in electronic and hardcopy form where appropriate. Electronic transfer to DigitalGlobe will constitute delivery and shall occur within 5 business days of the ER release date. ERs delivered as a separate CDIL do not need to be delivered twice – once per this paragraph and again per the relevant CDIL paragraph. Those ERs need only be delivered once per the relevant CDIL paragraph.

(“Relevant” in this clause refers to all ERs containing design information, analyses, test data, etc that affect the performance and/or operations of the satellite. It does not include ERs that contain BATC proprietary cost data.)

5.3.16    Flight Software Source Code (CDIL D-21)

Per the terms of the software license agreement set forth in the Agreement, BATC shall grant to DigitalGlobe a limited license to use the flight software code. A copy of the flight software code, as identified below, shall be provided to DigitalGlobe on suitable media. Other elements of the software, as identified below, shall be placed in escrow per the Agreement.

[**Redacted**]

For units that are subcontracted by BATC, software and firmware shall be delivered if delivered to BATC and BATC has the right to deliver it to DigitalGlobe.

5.3.17    Composite Grounding Design (CDIL D-22)

[**Redacted**]

5.3.18    Structural, Power, Thermal, and Reliability Analytical Models (CDIL D-23)

BATC shall provide the analytical models used to predict the integrated spacecraft and instrument Structural [**Redacted**] , Power, and Thermal performance.

 

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Satellite thermal performance modeling shall use the instrument thermal model provided by ITT. BATC shall use the integrated Satellite model to:

 

  a. Verify thermal interface requirements documented in the Spacecraft Bus to Instrument ICD are being met. Although BATC shall not be held contractually responsible for non-compliances on the ITT side of the interfaces, any such non-compliances revealed by Satellite thermal modeling shall be reported to DigitalGlobe.

 

  b. Verify the Bus meets all of its requirements when modeled as a complete Satellite, for example unit temperatures and line of sight stability. BATC shall deliver line of sight motion vs. time profiles to DigitalGlobe (for incorporation into system geolocation budgets).

 

  c. Develop predicted temperature vs. time profiles of key instrument nodes as coordinated with ITT through the established ICD process. BATC shall deliver these temperature profiles to DigitalGlobe and forward a copy to ITT (so that ITT can verify the instrument meets its requirements).

BATC shall also provide the spacecraft bus reliability model down to the component and/or card level. Electronic transfer to DigitalGlobe will constitute delivery.

 

5.3.19     Coordinate Transformation Document (CDIL D-24)

BATC shall provide the documentation of all coordinate reference frames used in the satellite system including their reference points within the spacecraft. Nominal values for all transformations shall be provided. Reference frames requiring on-orbit calibration shall be noted. The document shall be updated with best-estimates from pre-launch calibrations and measurements.

 

5.3.20    Flight Software Users Manual (CDIL D-25)

BATC shall provide documentation of the flight software to include flowchart of routines/modules, structure and calling sequences, commands, telemetry, database constants and uploadable parameters, address tables, and log file definitions and locations.

 

5.3.21    Component Acceptance Data Package (CDIL D-26)

BATC shall provide or make available data acceptance packages for all major components.

 

5.3.22    [**Redacted**]

[**Redacted**]

 

5.3.23    Instrument/Sensor Boresight Stability Data (CDIL D-28)

[**Redacted**]

 

5.3.24     Position and Attitude Accuracy (CDIL D-29)

BATC shall provide detailed analysis and test data showing compliance with position and attitude accuracy requirements.

 

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5.3.25     Satellite to MGB Interface Control Document(s) (CDIL D-32)

BATC shall produce and maintain the Satellite to MGB ICD(s). The ICD will address all interface issues including but not limited to: power, commanding, telemetry, mass and mass properties, mechanical envelope and mounting, thermal, fields-of-view, vibration and jitter isolation/management.

 

5.3.26    DigitalGlobe to BATC Electrical GSE Interface Control Document (CDIL D-33)

BATC shall produce and maintain an ICD for the STOC-to-NarrowBand Rack interface. This includes but is not limited to: grounding, commanding, telemetry, data formats, etc.

 

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6.0 PRODUCT ASSURANCE

 

6.1 Product Assurance Plan

The Contractor and its subcontractors shall have an established quality control system that meets the requirements of BATC’s Product Assurance Plan and BATC’s Supplier Product Assurance Plan

 

6.2 BATC Parts Control Board (PCB)

The Parts Control Board (PCB) shall be constructed as follows: A PCB will be established. The responsibility of this PCB is to ensure each EEE part was evaluated for performance relative to the requirements. With the exception of System Safety, the PCB will also be used as the forum to discuss other Systems Assurance/Product Assurance issues i.e., Materials and Processes, Reliability, etc. The PCB is responsible for the review and disposition of any noncompliance with BATC’s Product Assurance Plan.

The PCB consists of:

 

  a. BATC Product Assurance Manager (Chairman)

 

  b. BATC WV3 Product Assurance Specialist or designated alternate

 

  c. Designated technical specialist from the hardware/software product team as needed

 

  d. Other necessary disciplines as needed

 

  e. DigitalGlobe Designated Representative(s). (The DigitalGlobe member is a non-voting adjunct member).

 

6.2.1 Subcontractor Parts Control Board (PCB)

Subcontractor PCBs shall be established as necessary to implement BATC’s supplied Product Assurance Plan. It is BATC’s responsibility to verify compliance.

 

6.2.2 PCB Meetings

PCB meeting shall be convened as needed. BATC shall notify DigitalGlobe of upcoming meetings at least 2 working days in advance. DigitalGlobe attendance is optional BATC shall maintain meeting minutes to document all decisions and will provide a copy of the minutes to DigitalGlobe within 5 working days.

The minutes may be informal and in most cases shall be delivered to DigitalGlobe electronically via e-mail.

Minimal PCB approval/disposition signatures include BATC PAM and BATC WorldView Product Assurance Specialist or his designated alternate. Once the PCB approves a part, the Parts Engineer will indicate approval on the Advanced or Program Parts List (A/PPL).

 

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6.3 Parts and Materials

 

6.3.1 Electrical, Electronic, and Electro-mechanical Parts (EEE)Parts Listing (CDIL QA-1)

BATC shall prepare, maintain, and deliver a EEE Parts Listing for all satellite hardware except for Customer Furnished Equipment. This listing shall identify all EEE parts intended to be used by BATC and it’s vendors. For each part, the following minimum information shall be identified: manufacturer, description, lot date code. Parts shall be qualified as compared to BATC product assurance criteria and the Satellite Specification and the Satellite Specification Addendum. BATC’s internal process and format for EEE Parts Listing may be utilized.

The Parts List shall be maintained and reviewed by BATC as necessary, but minimally it shall be updated and provided to DigitalGlobe at the following:

 

  a. Prior to manufacturing for each box/component At this phase, it is acknowledged by DigitalGlobe and BATC that the list may be incomplete due to part shortages.

 

  b. Prior to box/component level Test Readiness Review

 

  c. Prior to the integration of any box/component onto the Bus.

 

6.3.2 Material and Processes Reports (CDIL QA-2)

BATC shall prepare and deliver reports documenting their approval of all materials and processes planned for use on the Bus.

 

6.4 As-Built Configuration and Conformance

 

6.2.1 6.4.1 As-Built Configured Article List (CDIL QA-3)

The as-built configured article status shall be maintained throughout the production program in the certification logs and production orders. At the conclusion of integration, the information shall be used to generate the preliminary As-built Configured Article List. After test and modification (if any) the List shall be finalized and presented.

 

6.2.2 6.4.2 Certificate of Conformance (CDIL QA-4)

A Certificate of Conformance shall be generated and signed off by Product Assurance and Program Management. It details the conformance (and exceptions) to the SOWs, specifications and other contractual documents for the delivered article. This Certificate of Conformance shall be delivered to DigitalGlobe at the Launch Readiness Review.

 

6.5 Product Assurance Reviews (CDIL QA-5)

The plan shall include a program for the periodic audit of portions of the Contractor's Product Assurance System in each of the below activity areas to confirm conformance to the requirements. These audits will be conducted by the Program Product Assurance engineer. BATC shall inform DigitalGlobe of the audit results.

 

  a. Reliability

 

  b. Parts Procurement

 

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  c. Materials and Processes

 

  d. Non-Conforming Material Control

 

  e. Configuration Management

 

  f. Safety

 

6.6 Documentation

Documents shall be submitted or made available to DigitalGlobe as indicated in the list provided in Attachment 1.

 

6.7 Known Non-Compliant Hardware

[**Redacted**]

 

6.8 Military Standard 461

[**Redacted**]

 

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7.0 PROCUREMENT

 

7.1 General

BATC shall be responsible for the work associated with the procurement of all material and subcontracts required to provide the deliverable items, except for the CFE items identified in Section 10.0. BATC shall procure according to the CSO Supplier Product Assurance Plan. Procurement activities shall be featured in the program master schedule.

 

7.2 Make/Buy Plans (CDIL PT-1)

BATC shall identify Make/Buy plans for all Satellite components.

 

7.3 Encryption/Decryption Devices

[**Redacted**]

 

7.4 Reviews

A series of reviews shall be established with each subcontractor. A schedule of these reviews shall be included in the Review Listings required by paragraph 4.5.3. The reviews will generally be held at the vendor and DigitalGlobe personnel may attend, at their option.

 

7.5 Program Subcontract Status Report (PSSR) (CDIL PT-2 )

BATC shall prepare a Program Subcontract Status Report (PSSR) for the program. The PSSR will contain critical status information on each major subcontract (larger than $1M) relative to:

 

   

Design & development

 

   

Procurement and Production

 

   

Assembly

 

   

Integration

 

   

Test, including any anomalies

 

   

Delivery schedule

 

   

Reviews

 

7.6 Documentation

Documents shall be submitted or made available to DigitalGlobe as indicated in the list provided in Attachment 1.

 

7.7 Subcontract Flow-downs

 

7.7.1 Assignment Clause

[**Redacted**]

 

7.7.2 Access

[**Redacted**]

 

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8.0 PRODUCTION ACTIVITIES

 

8.1 General

BATC shall appoint a Production engineer responsible for ensuring that BATC’s production capabilities match the requirements of the program. With the support of the Program QA engineer, he shall ensure that the production facilities comply with the Product Assurance requirements.

BATC shall be responsible for the work associated with the production of the deliverable items, except for the CFE items identified in Section 10.0. BATC shall be responsible for the production activities associated with integrating the CFE items as defined in Section 10.

Production activities shall be featured in the program master schedule.

 

8.2 Production Process

BATC shall produce the deliverable hardware according to applicable BATC standardized procedures. As a minimum, standardized BATC procedures shall be followed for the following topics:

[**Redacted**]

 

8.3 Access

The production manager shall arrange access for the DigitalGlobe staff to BATC manufacturing areas where manufacturing activities associated with the program are taking place.

 

8.4 Production Documentation

Production orders and Certification Logs shall document the as-built configuration. These logs shall be available on-site for DigitalGlobe review.

 

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9.0 INTEGRATION AND TEST ACTIVITIES

 

9.1 General

For the WV program the Integration and Test activities fall into four logical categories.

 

  a. Box level / Subsystem level testing

 

  b. Bus level integration and testing including integration of the instrument

 

  c. Satellite level testing

 

  d. Mission and Launch Rehearsals

The Integration and Test Manager shall be responsible to ensure that BATC's integration and test capabilities match the requirements of the program

BATC shall accomplish the work associated with a-d above for all BATC supplied hardware/software. BATC shall accomplish the work associated with b-d above for all CFE.

 

9.2 Box/Subsystem Level Testing

9.2.1     General

BATC shall perform all box level testing per environmental design and test specification and the box level Requirements Verification and Compliance Matrix.

 

9.2.2     [**Redacted**]

[**Redacted**]

 

9.3 WV Bus and Satellite Integration and Test Plans (CDIL PT-3)

BATC shall develop a WV Bus and Satellite Integration and Test Plan (Satellite I&T Plan) for the WV3 satellite. The test plans will include all I&T activities starting from the installation of the first component on to the bus structure through launch.

The WV I&T Plan(s) shall:

[**Redacted 4 Pages**]

 

9.4 Post-Shipment Instrument Testing

ITT will perform post-shipment functional testing to verify the Instrument survived shipment without damage. ITT will provide the necessary test equipment for the Instrument.

BATC shall provide:

[**Redacted**]

For schedule purposes the Instrument is not considered delivered to BATC upon arrival at BATC facility. Rather the instrument is considered delivered on the date that the Instrument has completed all necessary post-shipment testing and is ready and available for BATC to integrate to the telescope/bus.

 

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9.5 Supporting Documents

BATC shall provide as a minimum the following support documents:

 

  a. All necessary box level test procedures, integration procedures, and system level test procedures. Each procedure shall include a detailed test description explaining the “what, how, and why” of each test.

 

  b. A System Level Test Matrix. The test matrix will identify which System Level Test procedures or portions of those procedures will be accomplished at each test phase. The System Level Test phases include, but are not limited to:

[**Redacted**]

 

9.6 System Test Reports (CDIL PT-5)

[**Redacted**]

 

9.6.1 Content

The report shall include a summary of satellite configuration, test objectives, test results, significant hardware/software anomalies if any, resolution of significant anomalies, and a copy of all telemetry plots or other post-test data. The cognizant test engineer and the appropriate subsystem engineer(s) shall sign the report.

 

9.6.2 Timeliness

BATC shall publish the test reports No Later Than 15 working days after test completion.

 

9.7 Uninterruptible Power Supply (UPS)

[**Redacted**]

 

9.8 DigitalGlobe Integration and Test Engineering Access

 

9.8.1 On-Site and Visiting Engineers

BATC shall provide dedicated cubicle space, furniture, high-speed internet access, and phone lines for three resident DigitalGlobe I&T engineers. These DG on-site engineers will serve as the I&T focal point between DG and BATC. It is anticipated these engineers will be on-site at BATC on a full-time basis. BATC shall provide dedicated cubicle space, furniture, high-speed internet access, and phone lines for one visiting DigitalGlobe engineer.

 

9.8.2 Access to Live Satellite Telemetry

Once power-on bus integration begins, BATC shall provide DG with access to the live satellite telemetry from the cleanroom. DG will provide the necessary hardware to connect the Mission Control Center (MCC) to BATC GSE. DG will man and operate the DG hardware as necessary to flow the telemetry to the MCC. DigitalGlobe access to telemetry will occur on a non-interference basis to BATC test team.

 

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9.8.3     Test Observation By Other DG Engineers

BATC shall allow other DG satellite and ground system engineers access to the cleanroom to witness satellite testing. BATC is not obligated to coordinate, inform, or schedule testing according to DG engineer availability.

 

9.8.4     Access to Command and Telemetry Log Files (CDIL PT-6)

BATC shall deliver an archive of all command and telemetry files from satellite integration and test in an electronic format. BATC shall deliver an update weekly. Electronic transfer to the DG server shall constitute delivery. BATC shall maintain information about which command and telemetry database was used in delivered files as well as which test procedures were run in each file.

 

9.9 Test Reviews

The status of the Satellite shall be reviewed during the test phases of the program. See paragraph 4.5.3.2 for the list of reviews and required content.

 

9.10 Optional Testing

The following is a list of optional tests to be performed or supported by BATC. These are tests DigitalGlobe may choose to have BATC perform if the schedule permits. BATC should not show these tests in the baseline schedule. In each case after a test option is exercised by DigitalGlobe, BATC has 30 calendar days to prepare for the test. BATC shall provide a separate option price prior to the start of I&T for each of these tests.

[**Redacted**]

 

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10.0 CUSTOMER FURNISHED EQUIPMENT AND SERVICES

10.1     General

DigitalGlobe has contracts with vendors other than BATC who are responsible for providing portions of the overall system. DigitalGlobe has the responsibility for monitoring, administering, and verifying performance of those subcontracts. This section defines the items and support requirements that DigitalGlobe is responsible for securing and providing to BATC via these other subcontractors. This section also defines the equipment that DigitalGlobe is responsible for providing directly.

The delivery of all items shall be per Attachment 2: Customer Furnished Equipment list. DigitalGlobe will also arrange for the return of loaned equipment, if required, at no cost to BATC. CFE items shall be featured in the program master schedule. Unless otherwise explicitly provided to the contrary in Attachment 2, title to all equipment identified in this Section 10.0 shall remain in DigitalGlobe.

 

10.2 Flight Equipment

[**Redacted**]

 

10.2.1     [**Redacted**]

[**Redacted**]

 

10.2.2     [**Redacted**]

[**Redacted**]

 

10.2.3     [**Redacted**]

[**Redacted**]

 

10.2.4     [**Redacted**]

[**Redacted**]

 

10.2.5     [**Redacted**]

[**Redacted**]

 

10.2.6     [**Redacted**]

[**Redacted**]

 

10.3 Simulators (CSIM-1)

[**Redacted**]

 

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10.4 Launch Vehicle Interfaces

 

10.4.1     Launch Vehicle Interface

DigitalGlobe shall provide a launch vehicle interface adapter to BATC (CLSE-1). BATC shall use this for a fit check and for a separation test as described in paragraph 9.3.e. DigitalGlobe shall provide a match drill template to BATC (CLSE-2).

 

10.4.2     Launch Vehicle Separation Connectors (CLSE-3)

DigitalGlobe shall provide the flight satellite/launch vehicle separation connectors.

 

10.5 Ground Support Equipment

 

10.5.1     Wideband Link RGT Equipment

DigitalGlobe will provide a set of RGT ground equipment for capturing Instrument data in the cleanroom. Nominally, this will include the following equipment and documentation:

[**Redacted**]

 

10.5.2     Narrowband Link RGT Equipment (CGSE-5)

DigitalGlobe will provide a set of RGT ground equipment for processing the S-band uplink and X-band narrowband downlink in the cleanroom. The capability to bypass the RF sections and operate at a baseband Satellite interface shall be provided by BATC . This may include elements of the Mission Control Center [**Redacted**] as dictated by the architecture of the ground system. DigitalGlobe shall deliver to BATC operating documentation and interface details one month prior to delivery.

This equipment shall include: [**Redacted**]

 

10.5.3     Special Test Equipment

DigitalGlobe shall provide special WB Link / WB receiver test equipment for WB link development and testing. This will include:

[**Redacted**]

 

10.5.4 Mission Control Center (CGSE-11)

DigitalGlobe will provide portions of the Mission Control Center (MCC) and software as required to support the Satellite Integration and Test Plan, via data links between the MCC in Longmont, CO and BATC. BATC shall be responsible for work on the Satellite required to resolve problems associated with the Satellite performance and function. All work associated with resolution of DigitalGlobe provided ground equipment and interfaces shall be at DigitalGlobe expense.

 

10.5.5     [**Redacted**]

[**Redacted**]

 

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10.5.6     [**Redacted**]

[**Redacted**]

 

10.5.7     [**Redacted**]

[**Redacted**]

 

10.5.8     MGB Test Equipment (CGSE-15)

DigitalGlobe shall provide a signal generator, up-converter, feedhorn, and control computer.

 

10.6 Launch Vehicle Data (CLD-1 and CLD-2)

DigitalGlobe shall provide a preliminary and final Coupled Loads Analysis (CLA) to BATC from the Launch Services contractor.

 

10.7 Instrument Data

DigitalGlobe shall provide the WV3 instrument data and models, as specified in Paragraph 2.2, to support satellite level analysis and modeling for the areas listed below. BATC shall be responsible for additional data to support the provisions of this document and the spacecraft specification.

 

10.7.1     Instrument Structural Analysis Data (CID-1)

DigitalGlobe shall provide the WV3 instrument structural data and model.

 

10.7.2     Instrument Thermal Analysis Data (CID-2)

DigitalGlobe shall provide WV3 instrument thermal data and model.

 

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11.0 STORAGE AND DELIVERY

 

11.1 General

BATC shall be responsible for storage, if required, and delivery of the WV3 Satellite in accordance with the following paragraphs.

 

11.2 Satellite Pre-Shipment Storage

In the event that the Satellite is completed prior to the contractually scheduled delivery date, BATC shall provide, at their cost, suitable environmentally controlled storage including temperature and humidity monitoring and recording.

If shipment is delayed due to BATC beyond the contractually scheduled delivery date and the Satellite is complete, and such delay by BATC has caused a loss of available launch opportunity, the Satellite shall be placed in storage at BATC’s expense.

If shipment is delayed due to DigitalGlobe beyond the contractually scheduled delivery date and the Satellite is complete, the Satellite shall be placed in storage at DigitalGlobe’s expense.

 

11.3 Pre-Shipment Re-Test

Subject to the length of the storage period, appropriate maintenance and power up of those units sensitive to inactivity shall be undertaken. Any items exhibiting signs of deterioration shall be subject to appropriate follow up action according to the circumstances. All instances shall be reported to DigitalGlobe.

A thorough re-test is required should the storage exceed [**Redacted**] . Details shall be provided in the test requirements document. Appropriate follow up action shall be taken, according to the circumstances, should any problems be detected.

The re-test costs shall be at BATC expense if delay and retest were caused by BATC. The re-test costs shall be at DigitalGlobe’s expense if delay and retest were caused by DigitalGlobe.

 

11.4 Satellite Shipping and Delivery

[**Redacted**]

BATC shall provide shipping from BATC plant to the launch site. BATC shall pack the Satellite and ground support equipment in suitable containers for shipment to the launch site. BATC shall unpack the Satellite and ground support equipment at the payload processing facility at the launch site.

BATC shall provide insurance and security for the satellite and ground support equipment during shipment to the launch site.

BATC shall pack the ground support equipment for return to BATC plant and provide shipping.

BATC shall provide insurance for the ground support equipment during shipment back to BATC plant.

 

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The transportation environment shall be enveloped by the requirements in the Launch Vehicle and Instrument ICD and performance specification. BATC shall be responsible for ensuring the Satellite compatibility with the requirements. BATC shall be responsible for verifying all environmental requirements are met including temperature, humidity, and shock monitoring.

 

11.5 Satellite Launch Site Storage

BATC shall provide volumetric storage and access requirements to DigitalGlobe for shipping containers required at the launch site. The baseline program assumes no Satellite storage requirements at the launch site. However, if the launch should be delayed once the Satellite has been shipped, BATC shall provide, at DigitalGlobe expense, the support necessary to maintain, store, and retest the Satellite.

 

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12.0 LAUNCH SUPPORT SERVICES

BATC shall provide launch support services as defined in the following paragraphs.

 

12.1 General

[**Redacted**] DigitalGlobe will be responsible for overall coordination of launch activities. BATC shall support this activity as defined in this section of the SOW.

The Satellite shall be compatible with U.S. launch safety requirements. BATC shall generate a WV3 Missile System Pre-launch Safety Package (MSPSP) (CDIL LM-1) to document hazardous items or operations and planned safety procedures for the Satellite.

BATC shall support the safety review processes of the Launch Services Contractor and the Launch site.

 

12.2 Requirement Definition

BATC shall support the generation and maintenance of the Launch Vehicle ICD as defined in paragraph 5.3.12. BATC shall supply the following information and any other information normally required by the Delta II Payload Planners Guide to DigitalGlobe and the Launch Services contractor:

 

  a. Launch vehicle interface details and requirements.

 

  b. Requirements for launch site support and services including space, power, environment, contamination control, lifting/moving, telecommunications, etc.

 

  c. Statement of compliance with launch site safety requirements.

 

  d. Environmental requirements pre and post installation on launch vehicle.

 

  e. Verification of applicable portions of the Satellite to Launch Vehicle ICD.

 

  f. Launch Site Procedures.

BATC shall, by means of drawings, analysis, or test, be responsible for specifically confirming Satellite compatibility with the launch vehicle requirements defined in the ICD. BATC shall prepare a RVCM, as defined in paragraph 5.3.6, for those portions of the ICD for which it has responsibility.

 

12.3 Technical Interchange Meetings

BATC shall support up to eight Technical Interchange Meetings (TIM) with the launch organization . [**Redacted**] In addition, BATC will support informal meetings and teleconferences at DigitalGlobe’s Colorado facilities and BATC facility as required to resolve interface and infrastructure issues.

 

12.4 FEM and CLA-to-Design Load Comparisons (CDIL LM-2)

BATC shall provide preliminary Finite Element Models (FEM) and final FEMs for the WV3 Satellite for the purposes of performing coupled loads analyses. DigitalGlobe is responsible for obtaining valid CLA results from the launch service contractor and delivering those to BATC. BATC shall then compare the results of the coupled loads analyses to the design loads used in spacecraft bus and Instrument structural analysis to confirm that the resulting loads are within the design requirements as specified in the respective ICDs. The deliverables are as follows:

[**Redacted**]

 

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12.5 Export Regulations

All contractors on this program are anticipated to be U.S. companies including the launch service contractor. Therefore we anticipate no exports of hardware, software, or technology to foreign companies. However, if that situation changes, DigitalGlobe shall be the single point of contact for all export issues. Therefore:

BATC shall provide information directly to DigitalGlobe and DigitalGlobe will be responsible for obtaining and documenting all export approvals for all documentation transmitted to the launch vehicle agencies.

DigitalGlobe will be responsible for all work associated with compliance to export regulations including licensing, security, customs, document approval, transportation, etc. for documents/data channeled through DigitalGlobe.

It is understood that the Department of State International Traffic in Arms regulations (CFR 22 Part 120 through 130) strictly apply to any data or hardware covered under this SOW.

 

12.6 Adapter Fit-Check

BATC shall perform a launch vehicle interface check on the satellite as defined in the Test Plan. DigitalGlobe will arrange for the launch services contractor to provide the adapter, interface portions of the separation system, and GSE. If required, DigitalGlobe will also arrange for support from the launch services contractor at no cost to BATC.

 

12.7 Launch Site Infrastructure

DigitalGlobe shall arrange for and provide all launch site infrastructure necessary for satellite testing and pre-launch processing. This includes lease of a satellite processing facility.

 

12.8 Launch Site Operations

BATC shall support the launch operations campaign including provision of the test equipment and labor required to perform the launch site unpacking, Satellite checkout as defined by the WV I&T Plan, fueling, final mating to launch vehicle, launch, and repacking for return to BATC plant. Delays associated with BATC performance shall be at BATC expense. Any other delays shall be at DigitalGlobe expense. BATC will be responsible to support meetings for the purpose of coordinating launch site operations including joint operations with the launch services contractor. All efforts associated with reprocessing due to a cancelled or aborted launch shall be at DigitalGlobe expense.

 

12.9 Fueling

BATC shall prepare a fueling plan and the procedures required for fueling the Satellite using an appropriate fueling cart. BATC shall prepare the fueling equipment for hydrazine loading

 

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operations and package for shipment to the launch site. BATC shall be responsible for a single fuel loading operation unless multiple fuelings are required due to reasons under BATC’s control.

BATC shall provide all required consumables, propellant, safety training, and safety equipment including SCAPE gear required to effectively and safely perform satellite fueling operations. DigitalGlobe shall arrange for disposal of all hazardous wastes and any excess materials through its Launch Services provider.

BATC shall provide support to the launch vehicle/range contractor as required to respond to range specific requirements as they pertain to the handling of the hydrazine operations.

 

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13.0 MISSION PREPARATION AND ON-ORBIT COMMISSIONING

BATC shall assist with Mission preparation and On-orbit Commissioning by performing the following tasks and engineering services.

 

13.1     Training (CDIL LM-3)

 

13.1.1     Training Materials

BATC shall develop a training package for each satellite subsystem including the operation of the Instrument to address specifically the changes between WV-2 and WV3. The training package will be based on the Subsystem Description Documents (Paragraph 5.3.10) and include the same minimum information.

The training packages will be delivered on both paper and electronic media.

 

13.1.2     Training Sessions

For each subsystem, a cognizant BATC subsystem engineer shall present the training materials from paragraph 13.1.1. DigitalGlobe will provide the conference room and necessary projectors to support the presentation. DigitalGlobe reserves the right to videotape the training sessions for the purpose of training future DigitalGlobe personnel.

 

13.2     Command and Telemetry Handbook (CDIL LM-4)

BATC shall prepare a command and telemetry handbook. This document shall provide a definitive listing of all satellite telemetry and commands with a full description for each. The handbook shall meet the requirements identified in WV159.

 

13.3     Bus Subsystem Calibration Tools (CDIL LM-5)

BATC shall provide the subsystem calibration tools necessary for on-orbit calibration activities. Depending upon the final satellite design, these tools include but may not be limited to:

[**Redacted**]

 

13.4     DigitalGlobe Procedure Development Support

DigitalGlobe will generate the on-orbit procedures for the WV3 satellite(s). BATC shall understand the DigitalGlobe Concept-of-Operations and assist the procedure development. BATC shall review DigitalGlobe developed procedures for technical, operational, and safety concerns. [**Redacted**]

 

13.5     Commissioning Plan (CDIL LM-6)

DigitalGlobe shall generate the Commissioning Plan for the WV3 satellite. BATC shall assist the commissioning plan development. This includes assisting with the definition of the nominal sequence of events, required prerequisites, allowed out-of-sequence events, and required technical support for each event. DigitalGlobe will provide information about ground contacts, mission control center operations, and other necessary ground information used to create the commissioning plan(s).

 

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The Commissioning Plan shall include subsystem initialization, calibration, and demonstration of performance requirements including, but not limited to, the following:

[**Redacted**]

 

13.6 Anomaly Preparations

DigitalGlobe will generate anomaly resolution flow-charts. BATC shall assist with the anomaly flow-chart development including defining the probable anomalies and proper recovery actions/sequences. BATC shall review DigitalGlobe anomaly resolution flow-charts for technical, operational, and safety concerns.

 

13.7 Satellite Commissioning

 

13.7.1     Launch and Early Operations (LEOP) Phase

DigitalGlobe shall direct Satellite Launch and Early Operations. BATC shall provide a dedicated engineer for all satellite subsystems except for the Instrument subsystem. This support will run 24 hours per day for up to 7 days at the DigitalGlobe Mission Control Center in Longmont, CO.

 

13.7.2     Verification and Calibration (V&C) Phase

DigitalGlobe shall conduct the Verification and Calibration activities necessary to achieve Full Operational Capability (FOC). This includes but is not limited to satellite calibration activities such as star tracker and gyroscope calibrations.

Barring anomalies, V&C activities will nominally occur between 0600 and 1800 hours seven days per week. V&C activities will nominally require 30 days. BATC shall provide a dedicated engineer for all satellite subsystems except for the Instrument subsystem.

BATC shall also provide off-hour, on-call engineering support during V&C. A 30 minute or less call-back response is required.

 

13.7.2.1     Commissioning Reports (CDIL LM-7)

BATC shall produce a Commissioning Report. The report will document spacecraft bus Beginning-of-Life (BOL) performance and will update End-of-Life (EOL) performance predictions for all subsystems for which it has responsibility. At a minimum the report shall include:

 

  a. An explanation of significant deviations from performance metrics as identified in the satellite specification. The explanation shall include the reasons for the performance delta and the anticipated effects, if any, on the subsystem or satellite.

 

  b. An explanation of any known component or sub-component failures encountered during the LEOP or V&C Phases. The explanation shall include the possible causes of the failure, workarounds, updated reliability analysis for the component, subsystem, and satellite, and any impacts to DigitalGlobe’s concept of operation.

 

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13.8 Satellite Simulator

BATC shall provide a high fidelity dynamic satellite simulator. The simulator shall simulate satellite responses to stimuli. BATC shall provide sufficient documentation to accurately capture the design, functionality, capabilities, limitations, maintenance, extension, and operation of the simulator.

 

13.8.1     Satellite Simulator (CDIL LM-8)

BATC shall deliver a high fidelity satellite simulator per the requirements document [**Redacted**] . [**Redacted**] BATC and DigitalGlobe shall mutually agree upon a computer hardware and operating system, called the computing platform, for use in simulator functional and performance acceptance testing. BATC shall execute spacecraft simulator acceptance testing on the identified platform. DigitalGlobe shall execute the simulator testing on the same platform.

The satellite simulator does not need to include the MGB subsystem.

 

13.8.2     Documentation (CDIL LM-9)

BATC shall provide a Users manual with sufficient detail to:

 

   

Develop simulation scenarios including all configuration files, scripts, procedures, ephemeris, initial conditions, etc

 

   

Start-up, shut-down, and operate the simulation console and all simulator components

 

   

Control the simulation in real-time by setting/adjusting variables

 

   

Inspect low level model telemetry through the simulation console and simulator components directly

 

   

Save, modify, and load simulator state files used to start, pause, resume, and diagnose simulation scenarios

 

   

Understand all log files and log entries

 

   

Understand and recover from all error conditions

 

   

Extend, modify, maintain, build and release the simulator.

 

   

Incorporate a new flight software release into the simulator

In this context, “maintain” refers to the functions required to upgrade to new versions of commercial products such as MatLab or Simulink, alter configuration files, or otherwise customize the implementation.

 

13.8.3     Source Code (CDIL LM-10)

Per the terms of the software license agreement set forth in the Agreement, BATC shall provide all BATC developed bus simulator software components in source format (non binary). Source code shall be delivered in originating and native format. BATC does not need to provide development tools or COTS software, but BATC shall provide COTS software tool configuration including supplier, part number, and revision levels of tools used (e.g. compilers, linkers, and other development tools) and all reasonable data/information necessary for DigitalGlobe to enhance, modify, compile, and deploy the simulator.

 

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13.8.4     Delivery Schedule

BATC shall provide the simulator, manuals, and source code per Attachment 1. BATC shall deliver an updated simulator based upon LEOP/commissioning on-orbit performance. At a minimum, the following subsystem models will be updated: thermal, power, and ADCS models.

 

13.8.5     Technical Interchange Meetings and Design Reviews

BATC shall include DigitalGlobe in technical interchange meetings and design reviews such that DigitalGlobe can explain the intent behind various simulator requirements. BATC and DigitalGlobe shall refine high level requirements to detailed requirements during technical interchange meetings. BATC shall hold preliminary and critical design reviews for the Satellite Simulator. BATC shall hold intermediate Technical Interchange Meetings for the following modules at a minimum: the console, sensor and actuator models, redundancy modeling, fault modeling, thermal modeling, and power modeling.

 

13.9 Maneuver Planners

[**Redacted**]

 

13.9.1     [**Redacted**]

[**Redacted**]

 

13.9.2     [**Redacted**]

[**Redacted**]

 

13.9.3     [**Redacted**]

[**Redacted**]

 

13.10     Software Test Bench

BATC shall maintain a test bench suitable for the development and troubleshooting of the satellite computer Flight Software. The bench will include at a minimum:

[**Redacted**]

 

13.11     Ground Stations

DigitalGlobe is responsible for all Ground Station equipment. DigitalGlobe operators will be the lead operators of the Ground Segment.1

 

13.12     Telemetry Packet Creation and Mapping Tools (CDIL LM-15)

BATC shall provide the documentation, software, and training necessary for making changes to the telemetry received from the satellite. This includes changes to both telemetry packets and the mapping of those packets into various telemetry streams under CCSDS Grade C protocol.

 

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Initial delivery shall coincide with initial delivery of the Command & Telemetry Handbook (C&TH). BATC shall update if necessary at a. launch minus 6 months, b. final pre-launch C&TH delivery, and c. launch plus 6 months. Training shall occur coincident with Training Sessions specified in section 13.1 with delta training, if needed, at the final pre-launch C&TH delivery.

 

13.13    Telemetry Monitor and Response (CDIL LM-16)

BATC shall provide the documentation, software, and training necessary for making changes to flight software telemetry monitors and response actions on the satellite. This includes creation of new telemetry monitors and response actions, and changes to existing monitors and response actions.

Initial delivery shall coincide with initial delivery of the Command & Telemetry Handbook (C&TH). BATC shall update if necessary at a. launch minus 6 months, b. final pre-launch C&TH delivery, and c. launch plus 6 months. Training shall occur coincident with Training Sessions specified in section 13.1 with delta training, if needed, at the final pre-launch C&TH delivery.

 

14.0 COMMUNICATIONS FLEXIBILITY AND TT&C DEFINITION

BATC shall work with DigitalGlobe to set/finalize satellite ID’s by CDR.

 

15.0 FACILITIES

BATC shall provide all facilities necessary to perform the scope of this SOW.

 

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ATTACHMENT 1        CONTRACT DATA ITEMS LIST

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

PROGRAM MANAGEMENT

PM-1

   Program Management Structure    4.2    [**Redacted**]    As req’d   

PM-2

   Master Program Schedule    4.4    [**Redacted**]    monthly   

PM-3

   Component/Subsystem Design Review Listing    4.5.4    [**Redacted**]    As req’d   

PM-4

   Component/Subsystem Test Readiness / Data Review Listing    4.5.5    [**Redacted**]    As req’d   

PM-5

   Documentation Listing    4.6.3    [**Redacted**]   

No later than

Bi-monthly

  

PM-6

   Action Item List    4.7    [**Redacted**]    As req’d   

PM-7

   Historical Record of Payments & Payments Forecast    4.8.1 & 4.8.2    [**Redacted**]    monthly   

DESIGN

              

D-1

   Satellite to Instrument ICD    5.3.1    [**Redacted**]    As req’d   

D-2

   Satellite to Ground Station Narrowband ICD    5.3.2    [**Redacted**]    As req’d   

D-3

   Satellite to Ground Station Wideband Link ICD    5.3.3    [**Redacted**]    As req’d   

D-4

   Satellite Environmental Design and Test Specification    5.3.4    [**Redacted**]    As req’d   

D-5

   Contamination Control Plan    5.3.5    [**Redacted**]    As req’d   

D-6

   Satellite Level Requirements Verification/Compliance Matrix    5.3.6    [**Redacted**]    As req’d   

D-7

   Box Level Requirements Verification/Compliance Matrix    5.3.7    [**Redacted**]    As req’d   

D-8

   Drawings    5.3.8    [**Redacted**]    with EOs   

D-9

   Performance Compliance Matrix    5.3.9.1    [**Redacted**]    Quarterly   

D-10

   Risk Management Report    5.3.9.2    [**Redacted**]    Monthly   

 

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Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

D-11

   Subsystem Description Docs    5.3.10    [**Redacted**]    Launch – 4 m; Launch + 4 m    Updates only as required

D-12

   Thermal Analysis and Reports    5.3.11.a    [**Redacted**]    As req’d   

D-13

   Structural Analysis    5.3.11.b    [**Redacted**]    As req’d   

D-14

   Control System Analysis    5.3.11.c    [**Redacted**]    As req’d   

D-15

   Failure Modes and Effects and Criticality Analysis (FMECA)    5.3.11.d    [**Redacted**]    As req’d   

D-16

   Satellite Reliability Analysis    5.3.11.e    [**Redacted**]    As req’d   

D-17

   Satellite Imaging Performance    5.3.11.h    [**Redacted**]    As req’d   

D-18

   Critical Items List    5.3.13    [**Redacted**]    As req’d   

D-19

   Component Heritage Summary    5.3.14    [**Redacted**]    As req’d   

D-20

   System Engineering Reports    5.3.16    [**Redacted**]      

D-21

   Flight Software Code    5.3.16    [**Redacted**]   

As req’d Final

@ PSR

  

D-22

   Composite Grounding Design    5.3.17    [**Redacted**]    As req’d   

D-23

   Structural, Power, Thermal, and Reliability Analytical Models    5.3.18    [**Redacted**]    L+3 m   

D-24

   Coordinate Transformation Document    5.3.19    [**Redacted**]    L – 4m   

D-25

   Flight Software Users Manual    5.3.20    [**Redacted**]    As req’d   

D-26

   Component Acceptance Data Package    5.3.21    [**Redacted**]    As req’d   

D-27

   Jitter Analysis and Test Data    5.3.22    [**Redacted**]    As req’d   

D-28

   Telescope Boresight Stability Data    5.3.23    [**Redacted**]    As req’d   

D-29

   Position and Attitude Accuracy    5.3.24    [**Redacted**]    As req’d   

D-30

   PDR Data Package    4.5.3    [**Redacted**]    As req’d   

D-31

   CDR Data Package    4.5.3    [**Redacted**]    As req’d   

D-32

   Satellite to MGB ICD    5.3.25    [**Redacted**]    As req’d   

 

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Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

D-33

   Electrical GSE ICD    5.3.26    [**Redacted**]    As req’d   

D-34

   Satellite Requirements Review    4.5.3.1    [**Redacted**]      

D-35

   Battery Life Prediction    5.3.11.g    [**Redacted**]    L+ 1m   
PRODUCT ASSURANCE

QA-1

   EEE Parts List    6.2.1    [**Redacted**]      

QA-2

   Material Identification and Use Listing    6.2.2    [**Redacted**]    See para 6.3.2   

QA-3

   As built configured article list    6.3.1    [**Redacted**]    At Launch Readiness Review   

QA-4

   Certification of Conformance    6.3.2    [**Redacted**]      

QA-5

   Product Assurance Reviews    6.4    [**Redacted**]      
PROCUREMENT, PRODUCTION & TEST

PT-1

   Make / Buy Plans    7.2    [**Redacted**]    As req’d   

PT-2

   Program Subcontract Status Report    7.5    [**Redacted**]    monthly   

PT-3

   WV I&T Plan    9.3    [**Redacted**]    As req’d   

PT-4

   Battery Maintenance Plan    9.3.d    [**Redacted**]    As req’d   

PT-5

   System Test Reports    9.6    [**Redacted**]      

PT-6

   I&T Command and Telemetry Log Files    9.8.4    [**Redacted**]    weekly   

PT-7

   Reserved    Na    [**Redacted**]      

PT-8

   Instrument Integration Readiness Review Data Package    4.5.3    [**Redacted**]      

PT-9

   Satellite Environmental Testing Readiness Review Data Package    4.5.3    [**Redacted**]      

PT-10

   Pre-Ship Review Data Package    4.5.3    [**Redacted**]      
LAUNCH AND MISSION

LM-1

   Missile Systems Pre-Launch Safety Package (MSPSP)    12.1    [**Redacted**]   

L-52 wks TBD

L-26 wks TBD

  

LM-2

   Preliminary WV3 FEM    12.4.a    [**Redacted**]      
   Preliminary CLA-to-WV3 Design Loads Comparison    12.4.b    [**Redacted**]      

 

ITAR Controlled Document - DigitalGlobe Proprietary and Confidential
Use or disclosure of data is subject to the restriction on the title page of this document.
   Attch 1 - 3


LOGO

  

WV3 Satellite Statement of Work_

Doc Number 10329656

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

   Final WV3 FEM    12.4.c    [**Redacted**]      
   Final CLA-to-WV3 Design Loads Comparison    12.4.d    [**Redacted**]      

LM-3

   Training Materials and sessions    13.1.1    [**Redacted**]    As revised   

LM-4

   Command &Telemetry Handbook    13.2    [**Redacted**]    As revised   

LM-5

   Calibration Tools    13.3    [**Redacted**]    As revised & L+3 m   

LM-6

   Commissioning Plan    13.5    [**Redacted**]    As revised   

LM-7

   Commissioning Report    13.7.2.1    [**Redacted**]      

LM-8

   Satellite Simulator    13.8.1    [**Redacted**]    See Para 3.1.b   

LM-9

   Satellite Simulator Documentation    13.8.2    [**Redacted**]    With LM-8   

LM-10

   Satellite Simulator Source Code    13.8.3    [**Redacted**]    With LM-8   

LM-11

   High Fidelity Maneuver Planner    13.9.1    [**Redacted**]      

LM-12

   Peak Estimator Algorithm    13.9.2    [**Redacted**]      

LM-13

   Integrative Maneuver Model    3    [**Redacted**]      

LM-14

   Satellite Launch Readiness Review Data Package    4.5.3    [**Redacted**]      

LM-15

   Telemetry Packet Creation and Mapping Tools    13.12    [**Redacted**]    See 13.12   

LM-16

   Telemetry Monitor and Response    13.13    [**Redacted**]    See 13.13   

All items are provided for DigitalGlobe information only. Approvals are not required except for ICDs, changes to ICDs, and as otherwise noted.

ATP +1m is 1 month after Authorization to Proceed.

 

ITAR Controlled Document - DigitalGlobe Proprietary and Confidential
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   Attch 1 - 4


LOGO

  

WV3 Satellite Statement of Work_

Doc Number 10329656

 

ATTACHMENT 2        CUSTOMER FURNISHED EQUIPMENT LIST

 

Item

  

Title

   SOW
Ref
  

Date

  

Comment

FLIGHT HARDWARE

CFHW-1

   [**Redacted**]    10.2.1    [**Redacted**]   

CFHW-2

   [**Redacted**]    10.2.2    [**Redacted**]    Flight and corresponding ground keys.

CFHW-3

   [**Redacted**]    10.2.3    [**Redacted**]   

CFHW-4

   [**Redacted**]    10.2.4    [**Redacted**]   

CFHW-5

   [**Redacted**]    10.2.5    [**Redacted**]   

CFHW-6

   [**Redacted**]    10.2.6    [**Redacted**]   
[**Redacted**]         

CSIM-1

   [**Redacted**]    10.3    [**Redacted**]    Remains the property of DG
[**Redacted**]         

CLSE-1

   [**Redacted**]    10.4.1    [**Redacted**]   

CLSE-2

   [**Redacted**]    10.4.1    [**Redacted**]   

CLSE-3

   [**Redacted**]    10.4.2    [**Redacted**]   
[**Redacted**]         

CGSE-1

   [**Redacted**]    10.5.1.a    [**Redacted**]    Remains the property of DG

CGSE-2

   [**Redacted**]    10.5.1.b    [**Redacted**]    Remains the property of DG
CGSE-3    [**Redacted**]    10.5.1.c    [**Redacted**]    Remains the property of DG
CGSE-4    [**Redacted**]    10.5.1.d    [**Redacted**]    Remains the property of DG
CGSE-5    [**Redacted**]    10.5.2.    [**Redacted**]    Remains the property of DG
CGSE-6    [**Redacted**]    10.5.2.0    [**Redacted**]    Remains the property of DG
CGSE-7    [**Redacted**]    10.5.2.0    [**Redacted**]    Remains the property of DG
CGSE-8    [**Redacted**]    10.5.3.a    [**Redacted**]    Remains the property of DG
CGSE-9    [**Redacted**]    10.5.3.b    [**Redacted**]    Remains the property of DG
CGSE-10    [**Redacted**]    10.5.3.c    [**Redacted**]    Remains the property of DG
CGSE-11    [**Redacted**]    10.5.4    [**Redacted**]    Remains the property of DG

 

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   Attch 1 - 5


LOGO

  

WV3 Satellite Statement of Work_

Doc Number 10329656

 

Item

  

Title

   SOW
Ref
  

Date

  

Comment

CGSE-12    [**Redacted**]    10.5.5    [**Redacted**]    Remains the property of DG
CGSE-13    [**Redacted**]    10.5.6    [**Redacted**]    Remains the property of DG
CGSE-14    [**Redacted**]    10.5.7    [**Redacted**]    Remains the property of DG
CGSE-15    [**Redacted**]    10.5.8    [**Redacted**]    Remains the property of DG
LAUNCH VEHICLE DATA ITEM
CLD-1    WV3 Preliminary CLA    10.6    [**Redacted**]   
CLD-2    WV3 Final CLA    10.6    [**Redacted**]   
INSTRUMENT DATA ITEM
CID-1    WV3 Instrument Structural Data    10.7.1    [**Redacted**]   
CID-2    WV3 Instrument Thermal Data    10.7.2    [**Redacted**]   

DigitalGlobe will provide this equipment in accordance with the requirements of the Agreement.

 

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   Attch 1 - 6


Attachment 2

Specifications for the WorldView 3 Satellite, Rev 4.0

Dated 2 February 2011

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

 

LOGO    Exhibit 2 to Contract 60150

 

 

WorldView-3 Satellite

Specification

 

 

 

  Document #    10329655
  Revision #    4.0
  Release Date    2 Feb 2011
  Prepared by    George Hunyadi
  Approved by    Keith Constantinides

This Document Is ITAR Controlled

This document contains Technical Data as defined and controlled under the International Traffic In Arms Regulations (ITAR). Transfer of this data by any means to a foreign person, whether in the United States or abroad, without an export license or other approval from the U.S. Department of State is prohibited.

RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION

This document contains information proprietary and confidential to DigitalGlobe , to its subsidiaries, or to a third party to whom DigitalGlobe may have a legal obligation to protect such information from unauthorized disclosure, use or duplication. Any disclosure, use or duplication of this document or of any of the information contained herein for other than the specific purpose for which it was disclosed is expressly prohibited, except as DigitalGlobe may otherwise agree to in writing. This document may only be used for the purpose for which it is provided. All copies of this document are the sole property of DigitalGlobe and will be returned promptly upon request.


LOGO   

WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

Change Record

 

Revision

   Date   

Sections

  

Description of Change

1.0    20 Aug 2010    All    Initial Release
[**Redacted**]         
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        

 

 

 

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   i


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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

Table of Contents

 

  1.        SCOPE      7   
    1.1        P URPOSE      7   
    1.2        S YSTEM O VERVIEW      7   
    1.3        D OCUMENT O VERVIEW      7   
  2.        APPLICABLE DOCUMENTS      8   
    2.1        G OVERNMENT D OCUMENTS      8   
      2.1.1        [**Redacted**]      8   
      2.1.2        [**Redacted**]      8   
    2.2        N ON -G OVERNMENT D OCUMENTS      8   
      2.2.1        [**Redacted**]      8   
      2.2.2        [**Redacted**]      8   
      2.2.3        [**Redacted**]      8   
    2.3        R EFERENCE D OCUMENTS      8   
  3.        REQUIREMENTS      8   
    3.1        S ATELLITE D EFINITION      9   
      3.1.1        Satellite Diagrams      9   
        3.1.1.1        Component Tree      9   
        3.1.1.2        Coordinate System      9   
      3.1.2        Satellite Interfaces      9   
        3.1.2.1        Non-interference with Outside Systems      9   
          3.1.2.1.1       [**Redacted**      9   
          3.1.2.1.2       [**Redacted**]      9   
          3.1.2.1.3       [**Redacted**]      9   
        3.1.2.2        Satellite-Global Positioning System Interfaces      9   
          3.1.2.2.1       Compatibility      9   
        3.1.2.3        Satellite-Ground Interfaces      10   
          3.1.2.3.1       Compatibility      10   
          3.1.2.3.2       Remote Ground Terminal Locations      10   
          3.1.2.3.3       Command Uplink      10   
          3.1.2.3.4       Narrowband Telemetry Downlink      10   
          3.1.2.3.5       Wideband Data Downlink      10   
        3.1.2.4        Satellite-Launch Vehicle Interfaces      11   
          3.1.2.4.1       Compatibility      11   
          3.1.2.4.2       [**Redacted**]      11   
          3.1.2.4.3       Umbilical      11   
      3.1.3        Customer Furnished Equipment      11   
        3.1.3.1        Instrument      11   
          3.1.3.1.1       Physical, Structural and Mechanical Requirements      11   
          3.1.3.1.2       Thermal Interfaces      12   
          3.1.3.1.3       Power Interfaces      12   
          3.1.3.1.4       Command and Telemetry Interfaces      12   
          3.1.3.1.5       Image Data Interfaces      13   
          3.1.3.1.6       EOA Thermal Control Interfaces      13   
          3.1.3.1.7       [**Redacted**]      14   

 

 

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

      3.1.3.2   MGB      14   
  3.2   S ATELLITE C HARACTERISTICS      14   
    3.2.1   Performance      14   
      3.2.1.1   General Mission Requirements      14   
        3.2.1.1.1    Mission Life      14   
        3.2.1.1.2    Orbits      14   
      3.2.1.2   Satellite Operating Modes      14   
        3.2.1.2.1    Normal Operating Modes      14   
        3.2.1.2.2    Special / Contingency Modes      15   
        3.2.1.2.3    Intermediate and Transitional Modes      16   
      3.2.1.3   Pre-Launch Operations      16   
        3.2.1.3.1    Ground Storage      16   
        3.2.1.3.2    Launch Delay      16   
      3.2.1.4   Early Orbit Operations      17   
        3.2.1.4.1    Autonomous Operations After Separation      17   
        3.2.1.4.2    First [**Redacted**]      17   
        3.2.1.4.3    Commissioning      17   
      3.2.1.5   Mission Operations      17   
        3.2.1.5.1    Viewing Angles      17   
        3.2.1.5.2    Imaging and Downlink Operations      17   
        3.2.1.5.3    Stereo Imaging      18   
        3.2.1.5.4    Off-Nadir Imaging      18   
        3.2.1.5.5    [**Redacted**]      18   
        3.2.1.5.6    [**Redacted**]      18   
      3.2.1.6   Instrument Requirements      18   
        3.2.1.6.1    Integrated Bus/Instrument Performance Effects      18   
        3.2.1.6.2    [**Redacted**]      18   
        3.2.1.6.3    [**Redacted**]      19   
        3.2.1.6.4    Instrument Cleanliness      20   
      3.2.1.7   Bus Subsystem Requirements      20   
        3.2.1.7.1    [**Redacted**]      20   
        3.2.1.7.2    ADCS      21   
        3.2.1.7.3    Propulsion      23   
        3.2.1.7.4    Flight Software      24   
        3.2.1.7.5    C&DH      25   
        3.2.1.7.6    Narrowband Communications      29   
        3.2.1.7.7    [**Redacted**]      31   
        3.2.1.7.8    EPDS      34   
        3.2.1.7.9    Structures and Mechanisms      35   
        3.2.1.7.10    Thermal Control      36   
        3.2.1.7.11    Direct Tasking      37   
    3.2.2   Physical Characteristics      41   
      3.2.2.1   Size Constraints      41   
      3.2.2.2   Mass Constraints      41   
      3.2.2.3   Shipping Constraints      41   
    3.2.3   Reliability      41   

 

 

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

      3.2.3.1   End of Life Ps      41   
      3.2.3.2   [**Redacted**]      41   
      3.2.3.3   [**Redacted**]      41   
      3.2.3.4   Cycle-Limited Items      41   
        3.2.3.4.1    [**Redacted**]      42   
        3.2.3.4.2    [**Redacted**]      42   
    3.2.4   Availability and Maintainability      42   
      3.2.4.1   Fault Recovery Timeline      42   
      3.2.4.2   Environmental Conditions      42   
        3.2.4.2.1    Launch Induced Environments      42   
        3.2.4.2.2    On-Orbit Environments      42   
        3.2.4.2.3    Pre-Launch Environments      42   
  3.3   S ATELLITE D ESIGN AND C ONSTRUCTION      42   
    3.3.1   General      42   
    3.3.2   SEUs      42   
    3.3.3   Immunity to Latch-Up      43   
    3.3.4   Cleanliness and Contamination Control      43   
      3.3.4.1   [**Redacted**]      43   
      3.3.4.2   [**Redacted**]      43   
      3.3.4.3   [**Redacted**]      43   
      3.3.4.4   [**Redacted**]      43   
    3.3.5   Safety      43   
    3.3.6   [**Redacted**]      43   
4.   VERIFICATION      43   
5.   QUALITY ASSURANCE      43   

 

 

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

List of Tables

[**Redacted**]

List of Figures

[**Redacted**]

 

 

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

1. SCOPE

 

1.1 Purpose

This document describes the requirements for design and implementation of the DigitalGlobe WorldView-3 Satellite, being constructed to support DigitalGlobe commercial imaging operations.

 

1.2 System Overview

Ball Aerospace & Technology Corporation (BATC) is providing the integrated WorldView-3 imaging satellite to DigitalGlobe, Inc. As the Space Segment Integrator (SSI), BATC is manufacturing a Spacecraft Bus that can accommodate the panchromatic + multi-spectral WorldView-3 Instrument. This will be the same Bus design as used for predecessor WorldView Satellites. The Instrument is being supplied by ITT Industries Space Systems Division (ITT) to DigitalGlobe, with miscellaneous support units / functions provided by BATC. All ITT equipment will be provided as Customer Furnished Equipment (CFE) to BATC for Satellite integration. As the SSI, BATC will then perform Satellite level testing, prepare the Satellite for launch, and support on-orbit checkout of the Satellite.

The Satellite will be in a sun-synchronous orbit at an altitude between 450 and 830 km with a descending equator crossing time between 10:00 AM and 2:00 PM. [**Redacted**] Image data is recorded by the Spacecraft Bus and is normally downlinked to DigitalGlobe ground stations. However, direct downlink to user sites may also be performed in certain circumstances. Direct downlink is via the normal wideband downlink.

A key feature of the WordView-3 Satellite is Direct Tasking, where imaging and downlink parameters are directly uplinked from a customer’s ground station to the satellite, and image data is directly downlinked to a customer’s ground station, on the same and/or successive passes. Direct Tasking supports an expanded customer base and fulfills these customers’ desires to compress the overall planning-tasking-collection-downlink timeline and to not expose their task list to outside parties (including DigitalGlobe) prior to image collection. Full command authority is maintained by DigitalGlobe, with key commands needed to initiate the image and downlink operations uploaded from DigitalGlobe ground stations.

 

1.3 Document Overview

This document specifies functional, performance and interface requirements for the integrated Satellite and the Spacecraft Bus, including external Satellite interfaces, Instrument-Bus interfaces and Instrument integration, Bus and Satellite test, launch, and operational requirements. Separate Interface Control Documents (ICDs) detail the specifics of the Instrument-Bus interfaces and Integration and Test processes. Satisfaction of the Satellite-level requirements contained in this specification assume the Instrument provided as CFE meets its requirements, which are documented separately. As the SSI, BATC will refer to the separate Instrument Specifications as necessary to maintain the Spacecraft Bus to Instrument ICDs and develop an integration and test plan sufficient to ensure the integrated Satellite meets its system-level functional and performance requirements.

This specification may contain requirements that have not been fully defined. These open requirements are indicated by a TBR, and/or TBD:

TBR – To Be Resolved: Indicates parameters that exist, but may change after discussions with Contractor and others (e.g.: DigitalGlobe).

 

 

 

ITAR-Controlled Document

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

TBD – To Be Determined: Indicates parameters that have not yet been determined.

 

2. APPLICABLE DOCUMENTS

This document is the Satellite Specification. This specification defines the technical requirements called out in the Contract and a Statement of Work (SOW). The Contract and SOW define schedule requirements, deliverable items and programmatics. However, in the event of a conflict between a specific requirement herein and documents, then the Contract, the Statement of Work, this document, and Applicable documents shall govern in this order. If the revision is not specifically noted, the latest revision of each document applies.

At contract signing, the Environmental Design and Test Specification and Interface Control Documents from predecessor DigitalGlobe WorldView satellite programs listed below shall be considered the baseline release for WV-3. It is anticipated that the WV-3 versions of these documents will require few modifications from the predecessor baselines, with changes focused in a few key areas as driven by WV-3 unique requirements (for example enhanced Instrument thermal control and updated power values). The first release of the WV-3 version of each document shall supersede the predecessor version, which shall no longer be considered an Applicable Document.

Although the Satellite Integrating Contractor physically maintains many of these ICDs, their development is inherently a cooperative process. Accordingly, the latest released ICD revision shall always apply, where release is predicated on mutual agreement between all involved parties; for example the Instrument to Spacecraft ICD requires consensus between the Satellite Integrating Contractor, the Instrument Contractor, and DigitalGlobe.

 

2.1 Government Documents

 

2.1.1 [**Redacted**]

 

2.1.2 [**Redacted**}

 

2.2 Non-Government Documents

 

2.2.1 [**Redacted**]

 

2.2.2 [**Redacted**]

 

2.2.3 [**Redacted**]

 

2.3 Reference Documents

[**Redacted**]

 

3. REQUIREMENTS

Remarks contained as Rationale/Info shall NOT be considered a formal part of this specification and are provided for reference only.

 

 

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

[**Redacted**]

 

3.1 Satellite Definition

This Section defines fundamental terminology and identifies the basic Satellite functions along with the provider of each function. It also provides external interface requirements and internal interface requirements for the equipment to be provided [**Redacted**] to the SSI.

 

3.1.1 Satellite Diagrams

3.1.1.1    Component Tree

[**Redacted**] defines the major elements, subsystems, assemblies and units/functions of the Satellite and shows how they are allocated between DigitalGlobe’s contractors. The figure also indicates items that are delivered to the SSI [**Redacted 1 Page**].

3.1.1.2    Coordinate System

The base coordinate system used for all major Satellite element and segment mechanical interfaces shall be as shown in [**Redacted**] , for example, Instrument to Spacecraft Bus and Satellite to Launch Vehicle.

Other coordinate systems may be used as appropriate within elements and/or subsystems; [**Redacted**] . The relationships between the base coordinate system and other coordinate systems shall be explicitly shown in the appropriate documents (drawings, interface control documents, etc.).

[**Redacted**]

 

3.1.2 Satellite Interfaces

3.1.2.1    Non-interference with Outside Systems

3.1.2.1.1    [**Redacted**]

The Satellite shall not interfere with [**Redacted**].

3.1.2.1.2    [**Redacted**]

During normal operations, RF emissions from the Satellite shall not exceed the limits specified in the [**Redacted**] .

3.1.2.1.3    [**Redacted**]

All RF emissions shall use the frequency allocation of [**Redacted**] , with out-of-band emissions compliant with [**Redacted**].

3.1.2.2    Satellite-Global Positioning System Interfaces

3.1.2.2.1    Compatibility

The Spacecraft Bus shall be compatible with standard GPS interfaces as defined in [**Redacted**] .

 

 

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

3.1.2.3    Satellite-Ground Interfaces

The following paragraphs define high-level requirements for Satellite-Ground compatibility; detailed interface requirements shall be defined in the Narrowband and Wideband Satellite-Ground ICD.

[**Redacted**]

3.1.2.3.1    Compatibility

The Satellite Narrowband and Wideband Communications Subsystems shall be compatible with [**Redacted**] .

3.1.2.3.2    Remote Ground Terminal Locations

Remote Ground Terminals (RGTs) will be located as follows:

[**Redacted**]

3.1.2.3.3    Command Uplink

3.1.2.3.3.1    Effective Isotropic Radiated Power

The minimum Effective Isotropic Radiated Power (EIRP) of the command uplink antenna will be [**Redacted** ].

3.1.2.3.3.2    Axial Ratio

The command uplink antenna will transmit using [**Redacted**] .

3.1.2.3.4    Narrowband Telemetry Downlink

3.1.2.3.4.1    Figure of Merit (G/T)

The minimum G/T of the Narrowband receive antenna will be as follows across the frequency range of [**Redacted**] under all conditions, for the RGT locations defined in Section 3.1.2.3.2 Remote Ground Terminal Locations. These values include the effects of antenna pointing error and atmospheric conditions.

[**Redacted**]

3.1.2.3.4.2    Axial Ratio

The Narrowband receive antenna will receive using [**Redacted**] .

3.1.2.3.4.3    Implementation Loss

The demodulator implementation loss for the Narrowband telemetry receiver will be [**Redacted**] .

3.1.2.3.5    Wideband Data Downlink

3.1.2.3.5.1    Figure of Merit (G/T)

The minimum G/T of the Wideband receive antenna will be as follows across the frequency range of [**Redacted**] under all conditions, for the RGT locations defined in Section 3.1.2.3.2 Remote Ground Terminal Locations. These values include the effects of antenna pointing error and atmospheric conditions.

[**Redacted**]

3.1.2.3.5.2    Axial Ratio

The Wideband receive antenna will receive using [**Redacted**] .

 

 

 

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3.1.2.3.5.3    Implementation Loss

The demodulator implementation loss for the wideband telemetry receiver will be [**Redacted**] .

3.1.2.4    Satellite-Launch Vehicle Interfaces

The following paragraphs define high-level requirements for Satellite – Launch Vehicle compatibility; detailed interface requirements shall be defined in the Mission Specification.

3.1.2.4.1    Compatibility

The Satellite design shall be compatible with the [**Redacted**]

3.1.2.4.2    [**Redacted**]

The Satellite shall accommodate [**Redacted**].

3.1.2.4.3    Umbilical

The Satellite shall accommodate an umbilical to support all required functions for launch mode, including at a minimum the following critical electrical functions:

[**Redacted**]

 

3.1.3 Customer Furnished Equipment

3.1.3.1    Instrument

The Instrument will be provided to the SSI [**Redacted**] . The SSI shall provide interfaces as specified herein, with detailed interface requirements provided in accordance with the [**Redacted**] .

3.1.3.1.1    Physical, Structural and Mechanical Requirements

3.1.3.1.1.1    Configuration

The Spacecraft Bus shall accommodate the following major Instrument assemblies and/or units:

[**Redacted**]

3.1.3.1.1.2    Size

The Spacecraft Bus shall be capable of supporting the Instrument assemblies/units as specified in the Spacecraft Bus to Instrument ICDs.

3.1.3.1.1.3    Mass Properties

[**Redacted**]

3.1.3.1.1.4    EOA-Mounted Spacecraft Bus Equipment

The SSI shall provide the following equipment to be mounted on the EOA:

[**Redacted**]

3.1.3.1.1.5    EOA Fields of View

The Spacecraft Bus shall provide the Instrument with [**Redacted**] .

3.1.3.1.1.6    EOA Purge Fitting

The Satellite shall be configured to provide a purge fitting [**Redacted**] .

 

 

 

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3.1.3.1.1.7    Assembly, Integration and Test

 

a) To the maximum extent possible, the Satellite configuration shall permit independent integration of all Instrument assemblies/units and access to internal Instrument test ports and harness connections.

 

b) The Satellite configuration shall allow clear access to Instrument equipment essential to integration and test activities, for example: test ports, purge lines, aperture cover, interface connectors, etc.

3.1.3.1.1.8    EOA Vibration Environment

The SI shall ensure that the [**Redacted**]

3.1.3.1.1.9    [**Redacted**]

The Spacecraft Bus shall provide radiation shielding for the [**Redacted**] .

3.1.3.1.2    Thermal Interfaces

The Spacecraft Bus shall perform the following thermal functions, with interfaces to the Instrument as specified in the Spacecraft Bus to Instrument ICDs:

[**Redacted**]

3.1.3.1.3    Power Interfaces

The Spacecraft Bus shall provide electrical power to the Instrument as specified below, with the breakdown of individual unit powers and other characteristics as specified in the Spacecraft Bus to Instrument ICDs.

3.1.3.1.3.1    Instrument Power Feeds

The Spacecraft Bus shall provide power to all Instrument units as follows:

[**Redacted**]

3.1.3.1.3.2    Voltage

The Spacecraft Bus shall present power at the Instrument interfaces as follows:

[**Redacted**]

3.1.3.1.3.3    [**Redacted**]

[**Redacted**]

3.1.3.1.3.4    Average Operating Power

During normal operations, the Spacecraft Bus shall be able to perform [**Redacted**]

3.1.3.1.3.5    Survival Power

When in Emergency Mode, the Spacecraft Bus shall provide power as specified in [**Redacted**] via the Essential Bus, as specified in Section 3.1.3.1.3.1 Instrument Power Feeds.

3.1.3.1.3.6    Maximum Power

 

a) The Spacecraft Bus shall be capable of supporting the sustained maximum Instrument power specified in [**Redacted**] .

 

b) The Spacecraft Bus shall [**Redacted**]

3.1.3.1.4    Command and Telemetry Interfaces

The Spacecraft Bus shall provide the following command and telemetry interfaces to the Instrument, all of which shall be cross-strapped between the primary and redundant Spacecraft Bus electronics and primary and redundant Instrument electronics:

[**Redacted**]

 

 

 

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3.1.3.1.4.1    Instrument Commanding

Using the specified data interfaces, the Spacecraft Bus shall forward commands to the Instrument, [**Redacted**] as documented in the Spacecraft Bus to Instrument ICDs.

3.1.3.1.4.2    Image Start and Stop Commands

The commands for image [**Redacted**] shall be issued from the Spacecraft Bus [**Redacted**] .

3.1.3.1.4.3    Image Duration

 

a) The minimum Image duration possible shall be no more than [**Redacted**] .

 

b) There shall be [**Redacted**] .

 

c) Image durations shall be commandable in [**Redacted**] .

[**Redacted**]

3.1.3.1.4.4    Instrument Telemetry

Using the specified data interfaces, the Spacecraft Bus shall receive telemetry from the Instrument as documented in the Spacecraft Bus to Instrument ICDs. The following rules shall be applied to Instrument telemetry:

[**Redacted**]

3.1.3.1.4.5    [**Redacted**]

The Spacecraft Bus shall provide a [**Redacted**] as follows:

[**Redacted**]

3.1.3.1.5    Image Data Interfaces

The Spacecraft Bus shall provide image data interfaces [**Redacted**]

3.1.3.1.5.1    General Interface Definition

The Spacecraft Bus to Instrument data interface shall be as follows:

[**Redacted**]

3.1.3.1.5.2    Maximizing Storage and Downlink Efficiency

The Spacecraft Bus to Instrument data interface shall be capable of supporting the following Instrument configurations and shall ensure [**Redacted**]

3.1.3.1.6    EOA Thermal Control Interfaces

[**Redacted**]

3.1.3.1.6.1    [**Redacted**]

[**Redacted**]

3.1.3.1.6.2    [**Redacted**]

[**Redacted**]

3.1.3.1.6.3    [**Redacted**]

[**Redacted**]

 

 

 

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3.1.3.1.7    [**Redacted**]

The [**Redacted**] system will be provided to the SSI [**Redacted**] . The Spacecraft Bus shall interface to the [**Redacted**] system as specified in [**Redacted**] .

3.1.3.2    MGB

The MGB will be provided to the SSI [**Redacted**] . The SSI shall meet the MGB requirements specified in the MGB Requirements Documents and Interface Control Documents.

 

3.2 Satellite Characteristics

This Section defines the characteristics of the Satellite required to support the mission with respect to performance, physical characteristics, reliability, availability, and environmental conditions. The SSI shall derive and otherwise define lower level requirements necessary to implement the requirements of this specification, including those that are passed to the Instrument Contractor via the Spacecraft Bus to Instrument ICD, the Environmental Design and Test Specification, and other relevant documents.

 

3.2.1 Performance

3.2.1.1    General Mission Requirements

3.2.1.1.1    Mission Life

The Satellite shall meet all on-orbit performance requirements for a Mission Life of [**Redacted**] . The end of this period is defined as End of Life (EOL).

[**Redacted**]

3.2.1.1.2    Orbits

3.2.1.1.2.1    General Orbit Compatibility

The Satellite shall be capable of operating at any equatorial altitude between [**Redacted**]

3.2.1.1.2.2    Reserved

3.2.1.1.2.3    Mission Orbit

The Mission Orbit shall be defined as:

[**Redacted**]

3.2.1.1.2.4    Reserved

3.2.1.1.2.5    Insertion Orbit and Dispersions

The Satellite shall be compatible with being inserted directly into any of the orbits defined under General Orbit Compatibility, [**Redacted**]

3.2.1.2    Satellite Operating Modes

3.2.1.2.1    Normal Operating Modes

The Satellite shall, at a minimum, provide the operating modes defined in Table 3-1 Normal Operating Modes, with the following additional requirements:

[**Redacted**]

 

 

 

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Table 3-1 Normal Operating Modes

 

Mode

  

Basic Satellite State

  

Satellite Pointing

Cruise Mode

 

   [**Redacted**]    [**Redacted**]

[**Redacted**]

 

      [**Redacted**]

[**Redacted**]

 

   [**Redacted**]    [**Redacted**]
[**Redacted**]       [**Redacted**]

3.2.1.2.2    Special / Contingency Modes

The Satellite shall, at a minimum, provide the modes defined in [**Redacted**] , with the following additional requirements:

[**Redacted**]

Table 3-2 Special / Contingency Modes

 

Mode

 

Basic Satellite State

 

Satellite Pointing

[**Redacted**]

 

  [**Redacted**]   [**Redacted**]

[**Redacted**]

 

  [**Redacted**]   [**Redacted**]
[**Redacted**]   [**Redacted**]  

 

 

 

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Table 3-3 Simultaneous Operations

 

Simultaneous
Operations

 

Normal Operating Modes

 

Special / Contingency Modes

 

[**Redacted**]

 

[**Redacted**]

 

[**Redacted**]

 

[**Redacted**]

 

[**Redacted**]

 

[**Redacted**]

 

[**Redacted**]

 

[**Redacted**]

Recording Image Data

      [**Redacted**]   [**Redacted**]        

Recording Ancillary Data

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]      

Transmitting recorded Image and Ancillary Data

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]      

Recording Satellite state of health data

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]  

Transmitting stored state-of-health data

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]  

Transmitting real-time state-of-health data

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]  

Preserving stored Image and Ancillary Data

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]  

Preserving stored state-of-health data

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]   [**Redacted**]

Receiving and executing real-time commands

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]

Receiving and storing stored commands

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]  

Executing stored commands

  [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]  

[**Redacted**]

3.2.1.2.3    Intermediate and Transitional Modes

Additional intermediate and transitional modes may be defined for the Satellite and Spacecraft Bus. [**Redacted**]

3.2.1.3    Pre-Launch Operations

3.2.1.3.1    Ground Storage

The Satellite shall be capable of being stored under proper conditions for up to [**Redacted**] without the need for refurbishment.

3.2.1.3.2    Launch Delay

 

a) The Satellite shall be capable of remaining loaded with propellant for a minimum of [**Redacted**] prior to launch, while maintaining safety and status monitoring.

 

b) The Satellite shall be capable of launch for up to [**Redacted**] following the integration of the Satellite to the Launch Vehicle without the need for demate, while maintaining safety and status monitoring.

 

c) The Satellite shall be designed to permit [**Redacted**] .

 

 

 

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3.2.1.4    Early Orbit Operations

3.2.1.4.1    Autonomous Operations After Separation

Following the separation event, the Satellite shall autonomously:

[**Redacted**]

3.2.1.4.2    First [**Redacted**]

Following the Autonomous Operations after Separation, the Satellite shall pose no constraints on operation such that:

[**Redacted**]

3.2.1.4.3    Commissioning

The Satellite shall pose no constraints on operation such that total Satellite on-orbit performance can be fully verified as specified in the Statement of Work.

3.2.1.5    Mission Operations

3.2.1.5.1    Viewing Angles

Viewing angles referred to in the [**Redacted**] and elsewhere in this specification shall be as defined below.

[**Redacted**]

3.2.1.5.1.1    Nominal Field of Regard

The Nominal Field of Regard shall be defined as a [**Redacted**]

3.2.1.5.1.2    Maximum Field of Regard

The Maximum Field of Regard shall be defined as a [**Redacted**]

3.2.1.5.1.3    [**Redacted**]

[**Redacted**]

3.2.1.5.1.4    [**Redacted**]

[**Redacted**]

3.2.1.5.1.5    Instrument Operating Modes

The Satellite shall allow operation of the Instrument in the modes specified in [**Redacted**]

3.2.1.5.2    Imaging and Downlink Operations

The Satellite shall be capable of performing the imaging and downlink operations specified below assuming [**Redacted**]

3.2.1.5.2.1    [**Redacted**]

[**Redacted 1 Page**]

3.2.1.5.2.2    Wideband and Narrowband Downlinks

It shall be possible to perform both Wideband and Narrowband downlinks as follows:

[**Redacted**]

3.2.1.5.2.3     Instrument Mass Properties for [**Redacted**]

For purposes of verifying the Satellite’s ability to perform the DIS, [ **Redacted**]

 

 

 

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3.2.1.5.2.4    [**Redacted**]

[**Redacted**]

3.2.1.5.3    Stereo Imaging

 

a) The Satellite shall be capable of collecting the stereo imagery [**Redacted**]

 

b) The Satellite shall be capable of collecting stereo imagery [**Redacted**]

3.2.1.5.4    Off-Nadir Imaging

The Satellite shall be capable of supporting off-nadir image collections as follows:

[**Redacted**]

3.2.1.5.5    Special Imaging

3.2.1.5.5.1    Minimum Capabilities

[**Redacted**]

3.2.1.5.5.2    [**Redacted**]

[**Redacted**]

3.2.1.5.6    [**Redacted**]

[**Redacted**]

3.2.1.6    Instrument Requirements

3.2.1.6.1    Integrated Bus/Instrument Performance Effects

The SSI shall perform appropriate integrated Satellite-level analyses and design work in order to ensure the Satellite meets the following performance requirements. LOS motion shall be calculated using an Instrument Finite Element Model (FEM) provided by the Instrument Contractor as defined under Applicable Documents, which shall be assumed to meet the following requirements:

[**Redacted**]

3.2.1.6.1.1    [**Redacted**]

[**Redacted**]

3.2.1.6.1.2    [**Redacted**]

[**Redacted**]

3.2.1.6.2    [**Redacted**]

[**Redated**]

3.2.1.6.2.1    [**Redated**]

[**Redacted**]

 

 

 

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3.2.1.6.2.2    [**Redacted**]

[**Redacted**]

3.2.1.6.3    [**Redacted**]

[**Redacted**]

3.2.1.6.3.1    [**Redacted**]

[**Redacted**]

3.2.1.6.3.2    [**Redacted**]

[**Redacted**]

3.2.1.6.3.3    [**Redacted**]

[**Redacted**]

3.2.1.6.3.4    [**Redacted**]

[**Redacted**]

3.2.1.6.3.4.1    [**Redacted**]

[**Redacted**]

3.2.1.6.3.4.2    [**Redacted**]

[**Redacted**]

3.2.1.6.3.4.3    [**Redacted**]

[**Redacted**]

3.2.1.6.3.5    [**Redacted**]

[**Redacted**]

3.2.1.6.3.5.1    [**Redacted**]

[**Redacted**]

3.2.1.6.3.5.2    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.6.3.6    [**Redacted**]

[**Redacted**]

3.2.1.6.4    Instrument Cleanliness

[**Redacted**]

3.2.1.6.4.1    [**Redacted**]

[**Redacted**]

3.2.1.6.4.2    [**Redacted**]

[**Redacted**]

3.2.1.7    Bus Subsystem Requirements

In addition to supporting all subsystem-level requirements derived from the Satellite-level requirements specified in the above sections, Spacecraft Bus subsystems shall meet the specific requirements contained within this section.

3.2.1.7.1    [ **Redacted** ]

3.2.1.7.1.1    [**Redacted**]

[**Redacted**]

3.2.1.7.1.2    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.1    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.2    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.3    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.7.1.3.4    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.5    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.6    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.7    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.8    [**Redacted**]

[**Redacted**]

3.2.1.7.1.4    [**Redacted**]

3.2.1.7.1.4.1    [**Redacted**]

[**Redacted**]

3.2.1.7.1.4.2    [**Redacted**]

[**Redacted**]

3.2.1.7.1.4.3    [**Redacted**]

[**Redacted**]

3.2.1.7.1.4.4    [**Redacted**]

[**Redacted**]

3.2.1.7.2    ADCS

3.2.1.7.2.1    [**Redacted**]

[**Redacted**]

3.2.1.7.2.2    [**Redacted**]

3.2.1.7.2.2.1    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.7.2.2.2    [**Redacted**]

[**Redacted**]

3.2.1.7.2.2.3    [**Redacted**]

[**Redacted**]

3.2.1.7.2.2.4    [**Redacted**]

[**Redacted**]

3.2.1.7.2.2.5    [**Redacted**]

[**Redacted**]

3.2.1.7.2.3    [**Redacted**]

[**Redacted**]

3.2.1.7.2.4    [**Redacted**]

3.2.1.7.2.4.1    [**Redacted**]

[**Redacted**]

3.2.1.7.2.4.2    [**Redacted**]

[**Redacted**]

3.2.1.7.2.5    [**Redacted**]

3.2.1.7.2.6    [**Redacted**]

[**Redacted**]

3.2.1.7.2.7    [**Redacted**]

[**Redacted**]

3.2.1.7.2.8    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.7.2.9.1    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.2    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.3    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.4    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.5    [**Redacted**]

[**Redacted**]

3.2.1.7.2.10    [**Redacted**]

[**Redacted**]

3.2.1.7.2.11    Solar Arrays

In all modes of operation except Launch Mode, the ADCS shall be capable of pointing the Solar Array as follows:

[**Redacted**]

3.2.1.7.2.12    Wideband Antenna

While in Cruise Mode, Earth or Fixed Frame Imaging Mode, or maneuvering to/from Images, the ADCS shall be capable of pointing the Wideband Antenna as follows:

[**Redacted**]

3.2.1.7.3    Propulsion

3.2.1.7.3.1    Minimum Delta-V Capability

The Propulsion subsystem shall provide at least [**Redacted**]

3.2.1.7.3.2    Propellant Budget

The SSI shall develop and maintain a [**Redacted**]

3.2.1.7.3.3    Inefficiencies of Operation

The propellant budget shall, at a minimum, account for the following inefficiencies of operation:

[**Redacted**]

 

 

 

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3.2.1.7.3.4    Thruster Orientation

[**Redacted**]

3.2.1.7.3.5    [**Redacted**]

[**Redacted**]

3.2.1.7.4    Flight Software

3.2.1.7.4.1    [**Redacted**]

The Flight Software shall provide the capability to [**Redacted**].

3.2.1.7.4.2    Modularity

The design of the Satellite flight software shall be [**Redacted**] .

3.2.1.7.4.2.1    Module Size

The patching or replacing of any single Satellite flight software module shall not require more than [**Redacted**] or the [**Redacted**] shall be uploadable in no more than [**Redacted**] split across multiple contacts [**Redacted**].

3.2.1.7.4.3    Parameterization

The design of the Satellite flight software shall incorporate parameterization to support operational flexibility and command versatility.

[**Redacted**]

3.2.1.7.4.3.1    Parameter Range and Resolution

Parameters shall have enough range and resolution to permit operation of the Satellite to the requirements of this specification without having to patch the Satellite Flight software.

3.2.1.7.4.3.2    [**Redacted**]

[**Redacted**]

3.2.1.7.4.4    [**Redacted**]

[**Redacted**]

3.2.1.7.4.4.1    [**Redacted**]

[**Redacted**]

3.2.1.7.4.4.2    [**Redacted**]

[**Redacted**]

3.2.1.7.4.5    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.7.4.6    [**Redacted**]

[**Redacted**]

3.2.1.7.4.7    [**Redacted**]

[**Redacted**]

3.2.1.7.4.7.1    [**Redacted**]

[**Redacted**]

3.2.1.7.4.8    [**Redacted**]

[**Redacted**]

3.2.1.7.4.9    [**Redacted**]

[**Redacted**]

3.2.1.7.4.10    [**Redacted**]

[**Redacted**]

3.2.1.7.4.11    [**Redacted**]

[**Redacted**]

3.2.1.7.5    C&DH

3.2.1.7.5.1    Commands

3.2.1.7.5.1.1    Command Formats

Commands shall be formatted as specified in the [**Redacted**] .

3.2.1.7.5.1.2    Command Length

Commands shall be [**Redacted**] to assure compatibility with [**Redacted**] with [**Redacted**] and [**Redacted**] .

3.2.1.7.5.1.3    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.4    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.5    [**Redacted**]

[**Redacted**]

 

 

 

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WorldView-3 Satellite Specification

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3.2.1.7.5.1.6    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.7    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.8    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.9    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.10    Unique Satellite Identification

The Satellite identification used for command verification and acceptance shall be unique for each redundancy string and shall be different than IDs used on previous DigitalGlobe satellites.

[**Redacted**]

3.2.1.7.5.2    State-of-Health Telemetry

3.2.1.7.5.2.1    Telemetry Content

The C&DH subsystem shall collect and format housekeeping telemetry for the Spacecraft Bus and Instrument sufficient to provide the following capabilities on the ground:

[**Redacted**]

3.2.1.7.5.2.2    Telemetry Format

The C&DH subsystem shall format and transmit the [**Redacted**] as follows:

[**Redacted**]

3.2.1.7.5.2.3    [**Redacted**]

[**Redacted**]

3.2.1.7.5.2.4    [**Redacted**]

[**Redacted**]

3.2.1.7.5.2.5    [**Redacted**]

[**Redacted**]

 

 

 

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WorldView-3 Satellite Specification

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3.2.1.7.5.2.6    Unique Satellite Identification

All telemetry data shall periodically include a Satellite identification that is different than IDs used on previous DigitalGlobe satellites.

[**Redacted**]

3.2.1.7.5.2.7    Storage Capacity

The C&DH subsystem shall be capable of storing at least 36 hours of telemetry at an average rate of [**Redacted**] .

[**Redacted**]

3.2.1.7.5.2.8    [**Redacted**]

[**Redacted**]

3.2.1.7.5.2.9    [**Redacted**]

[**Redacted**]

3.2.1.7.5.3    [**Redacted**]

[**Redacted**]

3.2.1.7.5.4    Ancillary Data

During normal operations, the C&DH subsystem shall collect Ancillary Data from Bus and Instrument equipment and forward it [**Redacted**]

3.2.1.7.5.4.1    Standard Content

The standard content of the two Ancillary Data streams shall be as defined in [**Redacted**] .

[**Redacted**]

 

 

 

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WorldView-3 Satellite Specification

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Table 3-4 Standard Ancillary Data Content

 

Data Type

  

Description

  

Frequency

  

Minimum Rate

Continuous Ancillary Data Stream

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]

[**Redacted**]

Image Ancillary Data Stream

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

3.2.1.7.5.4.2    Format

The C&DH subsystem shall format the [**Redacted**]

3.2.1.7.5.4.3    Redefinable Content

It shall be possible to independently re-define the content of [**Redacted**] , subject to data bandwidth constraints.

[**Redacted**]

3.2.1.7.5.4.4    [**Redacted**]

[**Redacted**]

3.2.1.7.5.4.5    Data Transfer

The C&DH subsystem shall transfer the Ancillary Data to the MDR as follows:

[**Redacted**]

3.2.1.7.5.4.6    [**Redacted**]

[**Redacted**]

3.2.1.7.5.4.7    [**Redacted**]

[**Redacted**]

 

 

 

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WorldView-3 Satellite Specification

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3.2.1.7.5.5    Command & Telemetry Protocol

The satellite shall meet the requirements for the satellite command and telemetry protocol as specified in the [**Redacted**]

3.2.1.7.6    Narrowband Communications

3.2.1.7.6.1    Command Uplink

3.2.1.7.6.1.1    Uplink Bit Rate

The Command Uplink shall operate at one of two selectable rates, including all headers and other formatting, as follows:

[**Redacted**]

3.2.1.7.6.1.2    Bit Error Rate

The Command Uplink shall provide a bit error rate not to exceed [**Redacted**] .

3.2.1.7.6.1.3    Availability

The Command Uplink shall provide an availability of at least [**Redacted**] .

3.2.1.7.6.1.4    Elevation Angle

The Command Uplink shall operate at elevation angles of [**Redacted**] .

3.2.1.7.6.1.5    Link Margin

The Command Uplink shall meet all performance and functional requirements specified herein at EOL with a link margin of at least [**Redacted**] .

3.2.1.7.6.1.6    [**Redacted**]

[**Redacted**]

3.2.1.7.6.1.7    Modulation

The Command Uplink shall be modulated using [**Redacted**] .

3.2.1.7.6.1.8    Radio Frequency

The nominal Command Uplink carrier frequency shall be [**Redacted**] .

3.2.1.7.6.1.9    Antenna Coverage

Command Uplink antenna coverage shall be provided as follows:

[**Redacted**]

c) Provides realistic allowances for blockages by the Instrument.

3.2.1.7.6.1.10    Antenna Polarization

The Command Uplink antenna shall use [**Redacted**] .

Rationale/Info: To ensure compatibility with existing RGT equipment.

3.2.1.7.6.1.11    Idle Patterns

[**Redacted**]

3.2.1.7.6.2    Telemetry Downlink

3.2.1.7.6.2.1    [**Redacted**] Telemetry Bit Rate

The Telemetry Downlink shall be at the following selectable rates, including all header and other formatting required to structure the commands:

[**Redacted**]

 

 

 

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WorldView-3 Satellite Specification

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3.2.1.7.6.2.2    [**Redacted**] Telemetry Bit Rate

The Telemetry Downlink shall be at a rate of [**Redacted**] .

3.2.1.7.6.2.3    Bit Error Rate

The Telemetry Downlink shall provide a bit error rate not to exceed [**Redacted**] .

3.2.1.7.6.2.4    Availability

The Telemetry Downlink shall provide an availability of at least [**Redacted**] .

3.2.1.7.6.2.5    Elevation Angle

The Telemetry Downlink shall operate at elevation angles of [**Redacted**] .

3.2.1.7.6.2.6    Link Margin

The Telemetry Downlink shall meet all performance and functional requirements specified herein at EOL with a link margin of at least [**Redacted**] .

3.2.1.7.6.2.7    [**Redacted**]

[**Redacted**]

3.2.1.7.6.2.8    [**Redacted**]

[**Redacted**]

3.2.1.7.6.2.9    Modulation

 

a) The Telemetry Downlink shall use [**Redacted**] modulation as specified in the [**Redacted**] .

 

b) Any processing of the original data stream before transmission shall result in a [**Redacted**] .

3.2.1.7.6.2.10    Radio Frequency

The nominal Telemetry Downlink carrier frequency shall be [**Redacted**] .

3.2.1.7.6.2.11    Antenna Coverage: Special / Contingency Modes

 

a) Telemetry Downlink antenna coverage shall support all RF performance requirements specified herein (e.g. all downlink rates, both real-time and stored telemetry, BER, availability, elevation angle, etc.) with a [**Redacted**] when transmitting within [**Redacted**] .

 

b) A minimum elevation angle up to [**Redacted**] shall be permitted.

 

c) It shall be permissible to require ground commands in order to [**Redacted**] for operation in this mode, for example to switch from [**Redacted**] to [**Redacted**]

3.2.1.7.6.2.12    Antenna Coverage: Normal Operating Modes

Telemetry Downlink antenna coverage shall support all RF performance requirements specified herein (e.g. all downlink rates, BER, link margin, etc.) as follows:

[**Redacted**]

3.2.1.7.6.2.13    Antenna Polarization

The Telemetry Downlink antenna shall use [**Redacted**]

 

 

 

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WorldView-3 Satellite Specification

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3.2.1.7.6.2.14    Adjustable RF Output Power

The Telemetry Downlink shall provide the capability to adjust RF output power levels by ground command (real-time or stored), in increments sufficient to meet the link margin and interference limits specified in Sections 3.2.1.7.6.2.6 Link Margin and 3.1.2.1 Non-interference with Outside Systems, at any altitude over the range specified in Section 3.2.1.1.2.1 General Orbit Compatibility.

[**Redacted**]

3.2.1.7.7    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.1    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.2    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.3    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.4    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.5    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.6    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.7    [**Redacted**]

[**Redacted**]

 

 

 

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WorldView-3 Satellite Specification

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3.2.1.7.7.1.8    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.9    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.10    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.11    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.12    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.13    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.14    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.15    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.16    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.17    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2    [**Redacted**]

[**Redacted**]

 

 

 

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WorldView-3 Satellite Specification

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3.2.1.7.7.2.1    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.2    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.3    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.4    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.5    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.6    [**Redacted**]

3.2.1.7.7.2.7    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.8    [**Redacted**]

3.2.1.7.7.2.9    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.10    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.11    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.12    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.13    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.7.7.2.14    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.15    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.16    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.17    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.18    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.19    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.20    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.21    [**Redacted**]

[**Redacted**]

3.2.1.7.8    EPDS

3.2.1.7.8.1    Functional Requirements

The EPDS shall perform the following functions under the Conditions and Operational Scenarios specified below:

 

a) Provide sufficient power to all Spacecraft Bus and Instrument equipment to

[**Redacted**]

3.2.1.7.8.2    Realistic Worst Case Conditions

EPDS performance shall be evaluated under realistic worst-case conditions [**Redacted**], including, but not limited to:

[**Redacted**]

3.2.1.7.8.3    Operational Scenarios

EPDS performance shall be evaluated using the following operational scenarios for the range of orbits specified in Section 3.2.1.1.2.1 General Orbit Compatibility. For requirements verification, it is acceptable to perform in-depth analysis [**Redacted**]

 

 

 

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3.2.1.7.8.4    Instrument Power

The EPDS shall provide power to the Instrument as specified in Section 3.1.3.1.3 Power Interfaces.

3.2.1.7.8.5    [**Redacted**]

[**Redacted**]

3.2.1.7.8.6    [**Redacted**]

[**Redacted**]

3.2.1.7.8.7    [**Redacted**]

[**Redacted**]

3.2.1.7.8.8    [**Redacted**]

[**Redacted**]

3.2.1.7.9    Structures and Mechanisms

3.2.1.7.9.1    Functional Requirements

The Structure shall perform the following functions:

 

a) Support all Bus and Instrument equipment through all mission phases, including pre-launch, launch, initialization, normal operations, and EOL disposal.

 

b) [**Redacted**]

3.2.1.7.9.2    Factors and Margins of Safety

[**Redacted**]

3.2.1.7.9.3    Mechanisms

3.2.1.7.9.3.1    [**Redacted**]

[**Redacted**]

3.2.1.7.9.3.2    Accessibility

Deployment devices shall be accessible with minimum disturbance to the relative position of the mechanisms or their thermal control hardware.

3.2.1.7.9.3.3    Thermal Constraints

There shall be no thermal constraints against the operation of any mechanism at any time during the Satellite Mission Life such that:

[**Redacted**]

3.2.1.7.9.3.4    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.7.9.3.5    [**Redacted**]

[**Redacted**]

3.2.1.7.10    Thermal Control

3.2.1.7.10.1    Functional Requirements

The Thermal Control subsystem shall autonomously perform the following functions under the Conditions and Operational Scenarios specified below:

[**Redacted**]

3.2.1.7.10.2    Realistic Worst Case Conditions

Thermal Control Subsystem performance shall be evaluated under realistic worst-case conditions (i.e. precluding combinations of conditions that can not physically occur), including, but not limited to:

[**Redacted**]

3.2.1.7.10.3    Operational Scenarios

The Thermal Control Subsystem performance shall be evaluated using the following operational scenarios for the range of orbits specified in Section 3.2.1.1.2.1 General Orbit Compatibility. For requirements verification, it is acceptable to perform in-depth analysis [**Redacted**]

3.2.1.7.10.4    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.1    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.2    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.3    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.4    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.5    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.7.10.4.6    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.7    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.8    [**Redacted**]

3.2.1.7.10.4.9    [**Redacted**]

[**Redacted**]

3.2.1.7.10.5    [**Redacted**]

[**Redacted**]

3.2.1.7.11     Direct Tasking

The Satellite shall provide Direct Tasking capabilities as specified below, with the following definitions of key terms:

[**Redacted**]

3.2.1.7.11.1    [**Redacted**]

[**Redacted**]

3.2.1.7.11.1.1    [**Redacted**]

[**Redacted**]

3.2.1.7.11.1.2    [**Redacted**]

[**Redacted**]

3.2.1.7.11.1.3    [**Redacted**]

[**Redacted**]

3.2.1.7.11.1.4    [**Redacted**]

[**Redacted**]

3.2.1.7.11.1.5    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.7.11.1.6    [**Redacted**]

[**Redacted**]

3.2.1.7.11.1.7    [**Redacted**]

[**Redacted**]

3.2.1.7.11.2    [**Redacted**]

[**Redacted**]

3.2.1.7.11.2.1    [**Redacted**]

[**Redacted**]

3.2.1.7.11.2.2    [**Redacted**]

[**Redacted**]

3.2.1.7.11.2.3    [**Redacted**]

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3.2.1.7.11.2.4    [**Redacted**]

[**Redacted**]

3.2.1.7.11.2.5    [**Redacted**]

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3.2.1.7.11.3    [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.1    [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.2    [**Redacted**]

[**Redacted**]

 

 

 

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3.2.1.7.11.3.3    [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.4    [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.5    [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.6    [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.7    [**Redacted**]

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3.2.1.7.11.3.8    [**Redacted**]

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3.2.1.7.11.3.9    [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.10    [**Redacted**]

[**Redacted**]

3.2.1.7.11.4    [**Redacted**]

[**Redacted**]

3.2.1.7.11.4.1    [**Redacted**]

[**Redacted**]

3.2.1.7.11.4.2    [**Redacted**]

[**Redacted**]

 

 

 

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   38


LOGO   

WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

3.2.1.7.11.4.3    [**Redacted**]

[**Redacted**]

3.2.1.7.11.4.4    [**Redacted**]

[**Redacted**]

3.2.1.7.11.4.5    [**Redacted**]

[**Redacted**]

3.2.1.7.11.4.6    [**Redacted**]

[**Redacted**]

3.2.1.7.11.4.7    [**Redacted**]

[**Redacted**]

3.2.1.7.11.4.8    [**Redacted**]

[**Redacted**]

3.2.1.7.11.4.9    [**Redacted**]

[**Redacted**]

3.2.1.7.11.5    [**Redacted**]

3.2.1.7.11.5.1    [**Redacted**]

[**Redacted**]

3.2.1.7.11.5.2    [**Redacted**]

[**Redacted**]

3.2.1.7.11.5.3    [**Redacted**]

[**Redacted**]

3.2.1.7.11.5.4    [**Redacted**]

[**Redacted**]

3.2.1.7.11.5.5    [**Redacted**]

[**Redacted**]

3.2.1.7.11.5.6    [**Redacted**]

[**Redacted**]

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

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   39


LOGO   

WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

3.2.1.7.11.5.7    [**Redacted**]

[**Redacted**]

3.2.2    Physical Characteristics

3.2.2.1    Size Constraints

The size of the integrated Satellite shall be compatible with the specified Launch Vehicles and Shipping Constraints.

3.2.2.2    Mass Constraints

The total Satellite mass (including all parts of the Launch Vehicle adapter / separation mechanism that remain with the Satellite after separation) shall not exceed the limits established by the [**Redacted**] and the [**Redacted**] .

[**Redacted**]

3.2.2.3    Shipping Constraints

The Satellite and associated Ground Support Equipment (GSE), including the shipping container, shall be designed to allow transportation to the Launch Site via the [**Redacted**] or by [**Redacted**] and [**Redacted**] .

3.2.3    Reliability

3.2.3.1    End of Life Ps

[**Redacted**]

3.2.3.2    [**Redacted**]

[**Redacted]

3.2.3.3    [**Redacted**]

[**Redacted**]

3.2.3.4    Cycle-Limited Items

Items whose life is limited by the total number of operating cycles shall meet all on-orbit performance requirements after operating for [**Redacted**] the predicted number of cycles, including all cycles incurred during both the Mission Life and during ground testing. Cycle-limited items shall include at a minimum:

[**Redacted**]

3.2.3.4.1    [**Redacted**]

[**Redacted**]

3.2.3.4.2    [**Redacted**]

[**Redacted**]

 

 

 

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DigitalGlobe Proprietary and Confidential

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   40


LOGO   

WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

3.2.4    Availability and Maintainability

3.2.4.1    Fault Recovery Timeline

The Satellite equipment provided by the SSI shall be designed to allow recovery from any fault conditions and single event upsets or latch-ups within [**Redacted**] of ground operator intervention, with the exception of [**Redacted**] , which shall take no longer than [**Redacted**]

3.2.4.2    Environmental Conditions

The Satellite shall meet all functional and performance requirements after exposure to the following environments.

3.2.4.2.1    Launch Induced Environments

[**Redacted**]

3.2.4.2.2    On-Orbit Environments

On-orbit environments shall be consistent with operation in the Mission Orbit for the Mission Life and shall include, at a minimum:

[**Redacted**]

3.2.4.2.3    Pre-Launch Environments

Except for any specific testing aimed at verifying the design margins, the Satellite shall not be subjected to any environments that exceed the launch and on-orbit environments. This includes integration and test activities, transportation, launch site processing, and the period the Satellite is within the Launch Vehicle Fairing prior to launch.

3.3    Satellite Design and Construction

3.3.1    General

The Satellite Design and Construction shall be performed per standard SSI practices in accordance with the Environmental Design and Test Specification and the DigitalGlobe Space Segment Specification Addendum, including at a minimum the following items:

[**Redacted**]

3.3.2    SEUs

[**Redacted**]

3.3.3    Immunity to Latch-Up

[**Redacted**]

3.3.4    Cleanliness and Contamination Control

[**Redacted**]

 

 

 

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   41


LOGO   

WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 4.0: 2 Feb 2011

 

 

3.3.4.1     [**Redacted**]

[**Redacted**]

3.3.4.2     [**Redacted**]

[**Redacted**]

3.3.4.3     [**Redacted**]

[**Redacted**]

3.3.4.4     [**Redacted**]

[**Redacted**]

3.3.5     Safety

The Satellite shall be designed to allow for safe handling, operation, transportation, fuel loading and pressurization through all mission phases. It shall comply with the specific requirements of [**Redacted**] , including at a minimum:

[**Redacted**]

3.3.6     [**Redacted**]

[**Redacted**]

 

4. VERIFICATION

Requirements verification shall be performed per standard SSI practices, in accordance with the DigitalGlobe Space Segment Specification Addendum and the Statement of Work.

 

5. QUALITY ASSURANCE

Quality Assurance shall be performed per standard SSI practices, in accordance with the DigitalGlobe Space Segment Specification Addendum and the Statement of Work.

 

 

 

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   42


Attachment 3

WorldView 3 Payment Milestone Schedule, Rev 1.0

Dated 11 February 2011

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


WorldView 3 Payment Milestone Schedule

Exhibit 3 to WV3 Satellite Agreement # 60150

 

Item
#

   Invoice Date   

Line
Item

  

Description

   Completed    Milestone
Value
   Cumulative
Milestones
   Termination
Liability
1    [**Redacted**]       Milestone 1 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]            
2    [**Redacted**]       Milestone 2 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
3    [**Redacted**]       Milestone 3 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
4    [**Redacted**]       Milestone 4 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
5    [**Redacted**]       Milestone 5 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
6    [**Redacted**]       Milestone 6 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
7    [**Redacted**]       Milestone 7 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
8    [**Redacted**]       Milestone 8 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
9    [**Redacted**]       Milestone 9 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
10    [**Redacted**]       Milestone 10 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      


11    [**Redacted**]       Milestone 11 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
12    [**Redacted**]       Milestone 12 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
13    [**Redacted**]       Milestone 13 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
14    [**Redacted**]       Milestone 14 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
15    [**Redacted**]       Milestone 15 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
      e    [**Redacted**]    [**Redacted**]      
16    [**Redacted**]       Milestone 16 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
17    [**Redacted**]       Milestone 17 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
18    [**Redacted**]       Milestone 18 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
19    [**Redacted**]       Milestone 19 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      


20    [**Redacted**]       Milestone 20 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
21    [**Redacted**]       Milestone 21 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
22    [**Redacted**]       Milestone 22 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
23    [**Redacted**]       Milestone 23 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
24    [**Redacted**]       Milestone 24 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
25    [**Redacted**]       Milestone 25 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
26    [**Redacted**]       Milestone 26 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
27    [**Redacted**]       Milestone 27 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
28    [**Redacted**]       Milestone 28 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      


29    [**Redacted**]       Milestone 29 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
30    [**Redacted**]       Milestone 30 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
31    [**Redacted**]       Milestone 31 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
32    [**Redacted**]       Milestone 32 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
33    [**Redacted**]       Milestone 33 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
34    [**Redacted**]       Milestone 34 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
35    [**Redacted**]       Milestone 35 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
36    [**Redacted**]       Milestone 36 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
37    [**Redacted**]       Milestone 37 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      
38    [**Redacted**]       Milestone 38 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]    [**Redacted**]      
      b    [**Redacted**]    [**Redacted**]      
      c    [**Redacted**]    [**Redacted**]      
      d    [**Redacted**]    [**Redacted**]      


39    [**Redacted**]       Milestone 39 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
      b    [**Redacted**]      [**Redacted**]         
      c    [**Redacted**]      [**Redacted**]         
      d    [**Redacted**]      [**Redacted**]         
40    [**Redacted**]       Milestone 40 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
      b    [**Redacted**]      [**Redacted**]         
      c    [**Redacted**]      [**Redacted**]         
      d    [**Redacted**]      [**Redacted**]         
41    [**Redacted**]       Milestone 41 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
      b    [**Redacted**]      [**Redacted**]         
      c    [**Redacted**]      [**Redacted**]         
42    [**Redacted**]       Milestone 42 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
      b    [**Redacted**]      [**Redacted**]         
      c    [**Redacted**]      [**Redacted**]         
43    [**Redacted**]       Milestone 43 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
      b    [**Redacted**]      [**Redacted**]         
      c    [**Redacted**]      [**Redacted**]         
      d    [**Redacted**]      [**Redacted**]         
44    [**Redacted**]       Milestone 44 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
      b    [**Redacted**]      [**Redacted**]         
45    [**Redacted**]       Milestone 45 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
      b    [**Redacted**]      [**Redacted**]         
46    [**Redacted**]       Milestone 46 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
      b    [**Redacted**]      [**Redacted**]         
      c    [**Redacted**]      [**Redacted**]         
      d    [**Redacted**]      [**Redacted**]         
47    [**Redacted**]       Milestone 47 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
48    [**Redacted**]       Milestone 48 Total Value      [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]      [**Redacted**]         
      b    [**Redacted**]      [**Redacted**]         
      c    [**Redacted**]      [**Redacted**]         
         TOTALS                $ 184,242,399       $ 184,242,399       $ 180,575,000   


Attachment 4

WV3 Spacecraft Simulator Specification, Initial Release

Dated 20 December 2010

[**Redacted**]

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

Exhibit 10.5.2

FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

Amendment No. 3

To the

WorldView 3 Satellite Purchase Agreement 1460150

This Amendment No. 3 (“Amendment”) to WorldView 3 Satellite Purchase Agreement #60150 (the “Agreement”) is entered into by and between DigitalGlobe, Inc. (“DigitalGlobe”), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, CO 80503; and Ball Aerospace & Technologies Corp., a Delaware corporation with its principal offices located at 1600 Commerce Street, Boulder, CO 80301 (“BATC”). As used in this Agreement, “Party” means either DigitalGlobe or BATC, as appropriate, and “Parties” means DigitalGlobe and BATC.

WHEREAS, DigitalGlobe and BATC entered into the WorldView 3 Satellite Purchase Agreement #60150 (“Agreement”) on September 1, 2010;

Now, THEREFORE, the parties hereby agree to amend the Agreement to incorporate the following Engineering Change Proposals (“ECP”):

 

1. ECP 008: Document Updates

This change updates two specifications currently under contract. In addition the Payment Milestone Schedule, Exhibit 3, has been updated.

Therefore, this Amendment updates the following documents which are provided as Attachments 1-3 to the Agreement.

a. Exhibit 1 to the Agreement, titled “Statement of Work for the WorldView 3 Satellite -10329656, Rev 1.0,” and dated 7 February 2011, is replaced in its entirety by the updated version “Statement of Work for the WorldView 3 Satellite —10329656, Rev 2.0,” dated 5 May 2011, included as Attachment 1 to this Amendment; and

b. Exhibit 2 to the Agreement, titled “DigitalGlobe WorldView 3 Satellite Specification — 10329655, Rev 4.0,” and dated 2 February 2011, is replaced in its entirety by the updated version “DigitalGlobe WorldView 3 Satellite Specification — 10329655, Rev 5.0”, dated 2 May 2011, included as Attachment 2 to this Amendment; and

c. Exhibit 3 to the Agreement, titled “WorldView 3 Payment Milestone Schedule — 10329669, Rev 1.0” and dated 11 February 2011, is replaced in its entirety by the updated version “WorldView 3 Payment Milestone Schedule, Rev — 10329669, Rev 2.1,” dated 13 May 2011, included as Attachment 3 to this Amendment.

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document


2. ECP 009: Change of launch vehicle from Delta 11 to Atlas V

DigitalGlobe has changed the baseline WV3 launch vehicle from a Delta 11 to an Atlas V 401. This requires BATC to perform additional analyses to show compatibility with an Atlas V 401 launch vehicle. The following assumptions listed in BATC’s Firm Fixed Price proposal letter dated 18 April 2011 are valid:

[**Redacted**]

Rev 2.0 of the Statement of Work (SOW) and Rev 5.0 of the Satellite Specification contain the updates to reflect this new work.

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**] .

 

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of tins document.


SUMMARY

The value for these ECPs is $575,000, outlined in the following table:

 

Change #

  

Change Description

   $  

008

  

Document Updates

     [**Redacted**]   

009

  

[**Redacted**]

     [**Redacted**]   
     

 

 

 
  

TOTAL

   $ 575,000.00   
     

 

 

 

Contract Value Summary

 

Previous Contract Value

   $ 184,242,399.00   

ECPs

   $ 575,000.00   

New Contract Value

   $ 184,817,399.00   

Unless otherwise expressly provided herein, all other terms and conditions of the Agreement shall remain in full force and effect.

This Amendment No. 3 is hereby executed and agreed to by DigitalGlobe and BATC and shall be binding and effective as of the last date executed below.

 

Ball Aerospace & Technologies Corp.       DigitalGlobe, Inc.
[**Redacted**]   

 

     

/s/ Neal T. Anderson

Signature       Signature
[**Redacted**]   

 

Name       Name: Neal T. Anderson
[**Redacted**]   

 

Title       Title: Vice President, Tech Dev

17 May 2011

     

19 May 2011

 

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document


Attachment 1

Statement of Work for the WorldView 3 Satellite, Rev 2.0

Dated 5 May 2011


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

 

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   WV3 Satellite Statement of Work   
   Doc Number 10329656

 

 

Exhibit 1 to Agreement 60150

Statement of Work

for the WorldView 3

Satellite

 

 

 

  Document Number    10329656
  Release Date:    April 14, 2011
  Issue/Revision:    Release 2.0
  Prepared by:    Brian Uzzle
  Approved by    Steve Linn

RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION

This document contains information proprietary and confidential to DigitalGlobe Incorporated, to its subsidiaries, or to a third party to whom DigitalGlobe Incorporated may have a legal obligation to protect such information from unauthorized disclosure, use or duplication. Any disclosure, use or duplication of this document or of any of the information contained herein for other than the specific purpose for which it was disclosed is expressly prohibited, except as DigitalGlobe Incorporated may otherwise agree to in writing. This document may only be used for the purpose for which it is provided. All copies of this document are the sole property of DigitalGlobe and will be returned promptly upon request.

 

 

 

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Change Record

 

Issue

  

Date

  

Section(s)

  

Description of Change

Initial    20 Aug 2010       Initial Release
Rev 1    7 Feb 2011    2.1    Updated references for Satellite Specification, Satellite Simulator Specification, and Instrument Specification
      3.1.b    Updated dates for Satellite Simulator releases and number of deliveries
      3.1.n    Added deliverable item [**Redacted**]
      3.1.o    Added deliverable item [**Redacted**] .
      13.8.1    Clarified WV3 simulator changes versus WV2 simulator [**Redacted**] .
      Attachment 1    Updated release dates for Satellite Simulator (LM-8), Satellite Simulator Documentation (LM-9), and Satellite Simulator Source Code (LM-10).
      Attachment 1    Updated [**Redacted**] (CFHW-1)
Rev 2    14 Apr 2011    10.2.2    Updated [**Redacted**] , to be consistent with the date in Attachment 1 (CFHW-2)
     

1.2, 2.1,

4.5.3.2.F,

[**Redacted**] ,

11.4, 12.1,

12.2, 12.3,

Attachment 2

  

Changed launch vehicle baseline from Delta-2 to Atlas V.

Changed number of TIMs from 8 to 20.

Changed SLRR from [**Redacted**] to [**Redacted**] .

      3.1(b)    Updated delivery date for Simulator [**Redacted**] per Ball’s request.

 

 

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Issue

  

Date

  

Section(s)

  

Description of Change

        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        

 

 

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1.0 Introduction

This Statement of Work defines those tasks to be performed by BATC, the Space Segment Integrator, in defining; designing, producing, testing, verifying, and preparing for launch; the DigitalGlobe WorldView 3 Satellite. BATC has the overall responsibility for Satellite performance, as defined in the WV3 Satellite Specification, provided the DG-furnished Instrument meets its interfaces and specifications as defined in Paragraph 2.2. Within this role, BATC has the responsibility to work with DigitalGlobe to define requirements, allocate budgets, analyze performance, execute trade studies, interact with other vendors, define configurations(s), conform to existing Instrument interfaces, assess and mitigate risks, prepare various programmatic documentation, and interact with all participating organizations via meetings, teleconferences, and reviews as defined herein.

BATC shall provide integrating services as defined herein and the hardware and software, exclusive of Customer Furnished Equipment, that comprise the WV3 Satellite.

This document also defines the scope of work required from DigitalGlobe and associated subcontractors in order for BATC to execute this contract successfully.

Associate contractors under contract to DigitalGlobe shall provide the Instrument and Launch services. However, BATC shall fully support defining, documenting, and verifying Satellite(s) to LV and MGB interfaces and integration procedures. BATC shall insure that the Satellite will withstand all launch environments.

 

1.1 Definitions

Agreement: Satellite Purchase Agreement #60150 by and between DigitalGlobe, Inc. and Ball Aerospace and Technologies Corp., dated August 27, 2010, as amended.

Authorization to Proceed (ATP): Effective date of work commencement per the Agreement.

Satellite: The complete space-borne infrastructure required to perform the mission of providing radiometrically and geometrically correct imagery of the Earth. The Satellite consists of the Instrument and the Spacecraft Bus.

Instrument: The Instrument is that part of the Satellite that collects light photons using appropriate mirrors and structure, [**Redacted**] . It also may be designated the Electro-Optical Assembly (EOA). The instrument includes it’s own thermal control system. However, the instrument focus mechanism depends upon drive electronics to be provided by BATC per this Statement of Work. Also, the instrument stimulation lamp depends upon drive electronics to be provided by BATC per this Statement of Work.

Telescope: That part of the Instrument that collects and focuses light onto a focal plane. [**Redacted**] It also may be designated the Optical Telescope Unit (OTU).

Sensor Subsystem (SSS): That part of the Instrument that converts photons to analog voltage signals, [**Redacted**] , and digitizes [**Redacted**] those signals.

Solid State Recorder: The subsystem that accepts digital data from the SSS and Ancillary Data from the spacecraft bus, provides storage, [**Redacted**] and outputs that data to the wideband transmitter(s).

 

 

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Spacecraft Bus: The Bus is that part of the Satellite that provides the support infrastructure so the Instrument can function.

[**Redacted**]

MGB: “MGB” is a meaningless three letter designation for an additional subsystem being installed on the WV3 satellite. The MGB subsystem consists of three components. The first is a Sensor Unit (SU) which will attach to the aperture end of the OBA. The second is the Interface Adaptor Unit (IAU) which will mount to the spacecraft bus. The third is an inter-connect cable which connects the first two units.

Initial Acceptance: Occurs upon successful completion of the Satellite Pre-Ship Review as defined in paragraph 4.5.3.2.e

Final Acceptance: Occurs following satellite fueling operations and completion of the Satellite Launch Readiness Review as defined in paragraph 4.5.3.2.f

Transfer of Title: Occurs as defined in the Satellite Purchase Agreement paragraph 8.

 

1.2 Program Overview

Under this Scope of Work, DigitalGlobe will procure one satellite to support the EnhancedView program and future commercial operations. DigitalGlobe shall provide the Instrument as Customer Furnished Equipment via a procurement contract with ITT. DigitalGlobe shall provide the “MGB” subsystem. As on the WV2 program, BATC shall deliver a WorldView 2 like stimulation lamp that will be incorporated into the ITT provided instrument. BATC shall also incorporate into the Bus, an instrument focus mechanism electronics capability.

DigitalGlobe shall provide the Launch Services via a procurement contract with Lockheed Martin-Commercial Launch Services. Lockheed Martin-Commercial Launch Services has in-turn subcontracted with United Launch Alliance to provide the Atlas V launch vehicle and associated launch services. BATC can assume an Atlas V launch vehicle and a launch from Vandenberg Air Force Base. BATC shall assume satellite processing at Vandenberg AFB will occur in either the Astrotech Payload Processing facility or the Spaceport Systems International Processing Facility.

 

 

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2.0 Documents

 

2.1 Applicable Documents

This Statement-of-Work identifies applicable documents. These documents provide detailed requirements regarding Satellite performance, interfaces, and/or standardized design, fabrication, and testing processes/procedures. BATC and DigitalGlobe will perform the defined work according to these standardized processes/procedures such that the delivered products meet the performance and ICD requirements.

In the event of any conflict between these documents, the following order of precedence shall prevail: a) Agreement Terms & Conditions; b) Statement of Work; c) Satellite Specification; d) Other Applicable documents.

 

DigitalGlobe Produced or Provided Documents   

WV3 Satellite Specification

   [**Redacted**]

WV3 Spacecraft Simulator Specification

   [**Redacted**]

WV3 Command & Telemetry Handbook Specification

   [**Redacted**]

WV3 Maneuver Planner Specification

   [**Redacted**]

MGB Data Protection Plan for BATC

   [**Redacted**]

Stim Lamp and Stim Lamp Electronics Specification

   [**Redacted**]

[**Redacted**] Focus Mechanism Electronics Specification

   [**Redacted**]

Star Tracker Simulation Specification

   [**Redacted**]

IRU Simulator Specification

   [**Redacted**]

SSR to DPU Cable Design and Build Documentation

   [**Redacted**]
BATC Produced Documents   

BATC Product Assurance Plan

   [**Redacted**]

BATC Supplier Product Assurance Plan

   [**Redacted**]

BATC Document Control Procedure

   [**Redacted**]

BATC Configuration and Data Management Plan

   [**Redacted**]
Associated Contractor Produced Documents   

Astrotech Vandenberg Facility Accommodations Manual

   [**Redacted**]

Spaceport Systems International, Vandenberg Facility Accommodation Manual

   [**Redacted**]

Atlas V Launch Services User’s Guide

   [**Redacted**]

 

 

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2.2 Reference Documents

The following documents provide the baseline instrument definition. DigitalGlobe shall provide an instrument that is compliant with these documents.

 

DigitalGlobe Produced or Provided Documents   

Instrument Specification

   [**Redacted**]

Instrument Finite Element Model

   [**Redacted**]

 

 

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3.0 Contract Deliverables

 

3.1 Deliverable Items

 

  a. WV3 Satellite: Initial Acceptance: [**Redacted**] . Final Acceptance: [**Redacted**] Delivery shall be adjusted for Excusable Delay or failure of customer to [**Redacted**] to the extent that these delays affect the Delivery Date.

 

  b. WV3 Satellite Simulator

Initial release: [**Redacted**]

Simulator Delivery [**Redacted**]

Functional and performance signoff: [**Redacted**]

On orbit performance/tuning update: [**Redacted**]

 

  c. [**Redacted**]

 

  d. [**Redacted**]

 

  e. [**Redacted**]

 

  f. [**Redacted**]

 

  g. [**Redacted**]

 

  h. [**Redacted**]

 

  i. [**Redacted**]

 

  j. [**Redacted**]

 

  k. [**Redacted**]

 

  l. [**Redacted**]

 

  m. [**Redacted**]

 

  n. [**Redacted**]

 

  o. [**Redacted**]

 

3.2 Deliverable Data

Reference Attachment 1: Contractor Data Items List (CDIL)

 

3.3 Deliverable Services

 

  a. Storage and Delivery (Section 11.0)

 

  b. Launch Support (Section 12.0)

 

  c. Mission, Commissioning, & Readiness Support (Section 13.0)

 

 

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4.0 Program Management

 

4.1 Program Philosophy

Emphasis throughout all phases and functions of the project shall be to produce a reliable Satellite that meets the performance requirements on the contracted schedule. [**Redacted**]

 

4.2. BATC Organization (CDIL PM-1)

A dedicated Program Manager shall be appointed by BATC prior to the start of the contract. The Program Manager shall lead all of the Contractor’s activities under the contract.

A diagram illustrating the Program Management Structure shall be provided to DigitalGlobe. (CDIL PM-1) This diagram(s) shall indicate job titles and names of the program management team.

The Program Manager shall coordinate changes to contract conditions, price, timescale, deliverables, services or performance levels, unless a specific alternate has been appointed to deal with any of these matters. All changes to the contract documents shall require the written agreement of BATC contracts representative.

BATC shall also appoint a different and dedicated individual to be a single point of contact for each of the following:

 

  a. Program technical management (Satellite System Engineer)

 

  b. Instrument System Engineer

 

  c. Project Engineer Quality Assurance (PEQA)

 

  d. Program Integration and Test management

BATC shall appoint a different individual to be a single point of contact for each of the following:

 

  e. Various Bus Subsystem Lead Engineers

 

  f. Launch Vehicle Integration Engineer

 

  g. Program Contract Management

These individuals are key personnel and, if performing well, should remain unchanged for the duration of the program.

BATC shall appoint a Satellite Simulator Project Lead. This individual will be the technical lead for the Satellite Simulator development effort and will be responsible for meeting its technical and schedule guidelines established herein.

 

4.3 DigitalGlobe Management

DigitalGlobe will appoint a Program Manager who as an individual shall act as DigitalGlobe’s primary point of contact on all program management matters. As required, according to the activity and phase of the contract, the Program Manager will nominate specific individuals to interface directly with BATC.

The DigitalGlobe Program Manager shall coordinate changes to contract conditions, price, timescale, deliverables, services or performance levels, unless a specific alternate has been appointed to deal with any of these matters. All changes to the contract documents shall require the written agreement of the DigitalGlobe contracts representative.

 

 

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DigitalGlobe will also appoint a responsible individual(s) to be a single point of contact for each of the following.

[**Redacted**]

BATC shall permit direct engineering interactions between these DG individuals and their BATC counterparts.

 

4.4 Space Segment Master Program Schedule (MPS) (CDIL PM-2)

BATC shall develop maintain, and provide a Master Program Schedule (MPS) for the entire program including hardware, software, analyses, data item deliverables, and subcontractor activities for all phases of the program including design, integration, test, and shipment through final acceptance.

 

4.4.1 General

The MPS shall consist of a computer supported dependency network, each element of which shall represent a single program event. Each event shall be attributed a start and finish date. The network must clearly show the interdependency in terms of both time and function amongst the events.

The MPS shall be the major management tool for planning, monitoring and controlling the program, in terms of:

 

  a. Planning the program, monitoring progress, documenting actual activity accomplishment and actual durations.

 

  b. Predicting future progress.

 

  c. Identification of significant milestones e.g. review meeting.

 

  d. Identification of the time critical path.

 

  e. Reflecting actual progress and changes relative to baseline plan.

 

4.4.2 Required Software

The Contractor shall create and maintain the network using Microsoft Project (Version 2003). Schedules of a detailed nature shall be provided electronically on a monthly basis. A hardcopy shall also be provided on request.

 

4.4.3 MPS Construction

1.1.1.1    Content

The network shall be constructed against the following major classifications:

 

  a. Deliverable hardware down to component level

 

  b. Software development activities

 

  c. Facilities required to support the production of any of the deliverables

 

  d. Other events/items required to support the production of the deliverables or services. e.g. test aids, test software prototypes, etc.

 

  e. Customer Furnished Equipment required from DigitalGlobe

 

 

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Individual items in each class shall be considered to consist of a number of generic events. These events shall typically consist of such activities as:

 

  a. Plan

 

  b. Design & develop

 

  c. Manufacture

 

  d. Assemble

 

  e. Integrate

 

  f. Test

 

  g. Deliver

 

  h. Reviews

However steps may be omitted or added given unit specific circumstances.

1.1.1.2    Unique Identifiers

The MPS shall include a unique identifying number for each task. This will more easily allow DigitalGlobe to combine certain tasks into a DigitalGlobe Master Schedule. Unique identifiers will not be deleted, reused, or re-assigned to other tasks.

 

4.4.4 Reports

The MPS shall be capable of generating a number of different types of reports upon demand. All events and milestones shall be coded to permit a variety of sort options to be exercised without program modification. Both GANTT and network form shall be supported.

 

4.5 Meetings & Reviews

BATC shall support the meetings and reviews listed in the following paragraphs.

 

4.5.1 Weekly Status Meeting

BATC Program Manager shall support a weekly meeting/telecon with the DigitalGlobe Program Manager to review program status including schedule, technical, risk register, action item list, and subcontracts.

 

4.5.2 Monthly Program Status Review

BATC Program Manager shall support a monthly Program Status Review with DigitalGlobe.

 

4.5.3 Program Reviews

1.1.1.3    List of Formal Reviews

BATC will host and conduct formal reviews at the following program milestones. BATC shall prepare charts, viewgraphs, analysis results, trade study results, etc. in the quantity and quality typical of aerospace industries reviews.

 

  a. Satellite Requirements Review (SRR) (CDIL D-34) ) Only changes between WV2 and WV3 must be reviewed.

 

  b. Delta - Preliminary Design Review (PDR) (CDIL D-30) Only changes between WV2 and WV3 must be reviewed.

 

  c. Delta-Critical Design Review (CDR) (CDIL D-31) Only changes between WV2 and WV3 must be reviewed.

 

 

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  d. Spacecraft Bus Complete/Instrument Integration Readiness Review (IRR) (CDIL – PT-8)

 

  e. Satellite Environmental Testing Readiness Review (CDIL – PT-9)

 

  f. Satellite Pre-Ship Review (CDIL PT-10)

 

  g. Launch Readiness Review (CDIL LM-14)

1.1.1.4    4.5.3.2    Content of Reviews

 

  A. PDR and CDR: BATC shall conduct “delta” reviews. These reviews will document the design changes between WV2 and WV3. These design reviews (PDR and CDR) shall include information and documentation typical of aerospace industry reviews, such as:

 

  1. Satellite mechanical configuration including stowed and deployed views

 

  2. Satellite mechanical configuration including [**Redacted**]

 

  3. Satellite electrical/electronic design, including system block diagram and redundancy scheme

 

  4. Satellite software design

 

  5. Satellite Operating Modes

 

  6. Satellite Fault Detection and Safing

 

  7. Satellite Budgets and Margins

 

  A. Performance relative to specifications

 

  B. Mass

 

  C. Power

 

  D. Thermal

 

  E. Consumables

 

  F. Attitude control: stability, pointing and knowledge

 

  G. RF links

 

  H. Satellite resources: relays, telemetry stream, CPU throughput, processor memory

 

  I. MTF

 

  J. Reliability: Ps, critical items list, cycle-limited items, FMECA

 

 

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  B. Spacecraft Bus Complete/Instrument Integration Readiness Review: BATC shall host this review. The purpose is to ensure the readiness to begin Instrument integration. This review will cover information including:

 

  1. Instrument Integration procedure and hardware status

 

  2. Status of all Certification Logs for all Ball built hardware that will be integrated to the Bus. Ball shall provide rationale and recovery plan for all certification logs that are open, even though the hardware is complete and ready for integration.

 

  3. TAR and HAR status from the Bus Integration and Test phase

 

  4. Test Team Personnel status, certifications, and time-sharing with other programs

 

  5. Facility status

 

  6. Satellite configuration review

 

  7. Other issues that may impact the timely and successful completion of Instrument integration.

 

  8. The Spacecraft Bus shall be deemed complete and ready for Instrument integration when: [**Redacted**]

 

  C. Satellite Environmental Testing Readiness Review: BATC shall host this review. The purpose is to ensure the readiness to begin satellite level environmental testing which includes but is not limited to: TVAC, EMI/EMC, Vibration, Shock, and Acoustic. This review will cover information including:

[**Redacted**]

 

  D. Satellite Pre-Ship Review: BATC shall host this review. The purpose is to ensure the readiness to ship the satellite to the launch site. This review shall be held after completion of all significant testing and all post-test reviews. The purpose shall be to review the results of the entire Integration & Test program, and demonstrate compliance to the satellite specification., and provide for satellite preliminary acceptance.

The Pre-ship Review shall be deemed satisfactory and the satellite preliminary acceptance by DigitalGlobe complete when the:

[**Redacted**]

 

  F. Satellite Launch Readiness Review: BATC shall conduct a Satellite Launch Readiness Review (SLRR) on or about [**Redacted**] . (Note, the Launch Services Provider, Lockheed Martin/ULA also has a review called the Launch Readiness Review. However, that review encompasses the satellite, launch vehicle, weather, and range support.) This SOW paragraph is only concerned with the readiness to launch the satellite. BATC shall review the results of the launch site Integration & Test activities, review any updates to the Verification Matrix, and provide for satellite final acceptance.

 

 

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The SLRR shall be deemed satisfactory and the satellite final acceptance by DigitalGlobe complete when the:

[**Redacted**]

 

4.5.4 Component/Subsystem Design Review Listing (CDIL PM-3)

BATC shall prepare a summary listing of all planned component (box level) and subsystem design reviews. This listing shall include BATC and vendor provided hardware, and BATC provided software including the satellite simulator and maneuver planner software. This listing shall define the meeting format and required attendance. BATC shall provide a minimum of 10 days advance notice to DigitalGlobe for the following major reviews:

 

  a. System/Subsystem & Component PDRs

 

  b. System/Subsystem & Component CDRs

DigitalGlobe attendance and participation, including support consultants, shall be allowed, but not required at all reviews. The review activity will not be repeated if DigitalGlobe fails to attend.

 

4.5.5 Component/Subsystem Test Readiness / Data Review Listing (CDIL PM-4)

BATC shall prepare a summary listing of all planned component (box level) and subsystem qualification and acceptance test reviews. This listing shall include BATC provided and vendor provided hardware, and BATC provided software. This listing shall define the meeting format and required attendance. BATC shall inform DigitalGlobe of upcoming reviews in a timely manner.

DigitalGlobe attendance and participation shall be allowed, but not required at all reviews. The review activity will not be repeated if DigitalGlobe fails to attend.

 

4.5.6 DigitalGlobe Meetings

DigitalGlobe will arrange separate contracts for the:

 

  a. Launch Vehicle Segment (LV)

 

  b. Instrument

 

  c. Launch and Mission insurance

A series of technical interchange and review meetings will be held with these contractors jointly and separately, as required. BATC shall provide representation at these meetings as needed to resolve interface issues.

In the case of the insurance (c), BATC will provide inputs to formal presentations and support meetings to be held at the DigitalGlobe facility. DigitalGlobe will be responsible for responses to action items using information made available or provided by BATC during the course of the program.

 

 

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4.6 Documentation Management

 

4.6.1 Access to Program Technical Data

DigitalGlobe will have access rights to all program technical data that BATC generates and Subcontractor data to which BATC has legal and contractual rights. Program technical data may include Engineering Reports, drawings, software source code, and other tools used in the development of the spacecraft and analysis of requirements.

 

4.6.2 Objective

BATC shall establish a control and monitoring process relating to all deliverable documentation and other technical and test data for the complete program. The program shall account for the following:

 

  a. Preparation, review, and formal release as required

 

  b. Changes

 

  c. Storage, backup, and retrieval

 

  d. Distribution

 

Note:   BATC shall include the DigitalGlobe Satellite Integration and Test Point-of-Contact on the distribution list of all relevant WV3 Engineering Reports. (“Relevant” in this clause refers to all ERs containing design information, analyses, test data, etc that affect the performance and/or operations of the satellite. It does not include ERs that contain BATC proprietary cost data.)

 

  e. DigitalGlobe access to all BATC documentation prepared on the project

 

  f. Long term storage for the purpose of through-life product support

As a primary supporting management tool, BATC shall use a secure project server. All data items except memory intensive drawings, test data, production logs, and QA data shall be maintained electronically on the project server. The project shall use the Microsoft Office software suite for word processing, spreadsheets, presentations, and documentation databases.

 

4.6.3 Documentation Listing (CDIL PM-5)

BATC shall develop and maintain a Documentation Listing that identifies all deliverable reports, analyses, drawings, software items, etc., that are developed on the project. The Documentation Listing shall include a naming convention that uniquely identifies the documents for electronic access where applicable. The List shall also indicate spacecraft name, a short title/description of the document, subsystem affected, the latest revision number and date, planned completion date, and status information. The List shall indicate those WV1 and WV2 documents that are also applicable to WV3. Document updates are required to reflect content changes. Document updates are not required if the sole purpose is to reflect applicability to WV3.

 

4.6.4 Documentation Delivery

The Contractor shall deliver document in native formats, e.g. Microsoft Word, Excel, etc., as opposed to PDF except as noted below. DigitalGlobe will identify the delivery location, such as a Microsoft Office Sharepoint Server (MOSS) internet site, and provide Contractor with username and password-controlled access. Documents shall be submitted or made available to DigitalGlobe according to the dates indicated in the list provided in Attachment 1.

 

 

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In the case of deliverables generated in Microsoft Office, such as Word, Excel, PowerPoint, etc; BATC shall populate the document property fields with the following minimum information: Title, Subject, Author, and key words.

In the case of deliverables that are not generated in MicroSoft Office, such as BATC drawings, .pdf is acceptable and BATC shall populate the property fields of drawings after they are converted to .pdf format.

 

4.7 Action Item Tracking (CDIL PM-6)

BATC shall maintain an Action Item List indicating all significant action items, including those of BATC as well as those of other organizations that relate to interactions with BATC. The Action Item List will be developed and maintained in a format that allows sorting by subsystem, originating party, receiving party, originating date, and closing date. BATC shall be responsible for ensuring closure of those items relating to BATC interactions and interfaces.

 

4.8 Financial Management

BATC shall define a standard set of formats for reporting program financial payment and billing status and shall submit them on a monthly basis. This shall consist of the following:

 

4.8.1 Historical Record of Payments (CDIL PM-7)

This shall consist of a record of the individual payments made, updated on a monthly basis. This record shall be cross-referenced to the payment schedule incorporated in the contract. Payments made in support of contract amendments shall be separately reported and cross-referenced to the payment schedule incorporated in the amendment.

 

4.8.2 Payments Forecast (CDIL PM-7)

This shall consist of a forecast of the future invoices and shall be cross-referenced to the payment schedule incorporated in the contract. Payment milestone forecasts shall be consistent with program progress reported on the Master Program Schedule. NOTE: Record of Payments and Payment Forecast are delivered as a single CDIL item.

 

4.9 Contract Change Control

These are considered to be of three types only:

 

  a. Contract Amendments

 

  b. Waivers: A written authorization granted after contract award to accept an item, that during production, or after having been submitted for inspection or acceptance, is found to depart from contract or specified configuration requirements. Waivers are intended only as one-time departures from an established configuration for specified items or lots and are not intended to be repeatedly used in place of formal engineering changes.

 

  c. Deviations: A written authorization, granted after contract award and prior to the manufacture of the item, to depart from a particular performance or design requirement of a contract, specification, or referenced document, for a specific number of units or a specified period of time. Deviations are intended only as one-time departures from an established configuration for specified items or lots and are not intended to be repeatedly used in place of formal engineering changes.

 

 

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BATC shall devise a system to control, monitor, and notify DigitalGlobe of these changes. The control system shall include provision for:

 

  a. A unique numbering scheme to track the changes through to completion.

 

  b. Impact upon contract obligation: - price, performance and delivery schedule, with specific identification of the item(s) of hardware, software or documentation affected.

 

  c. Notification of timescale for acceptance or rejection for each change, typically 10 business days.

 

 

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5.0 Design

 

5.1 General

BATC shall perform the necessary trade studies, preliminary design, and detailed design of the Satellite, exclusive of the Customer Furnished Equipment as defined in Section 10, in accordance with the applicable documents. BATC shall design and procure the Ground Support Equipment necessary to support Satellite Integration and Test activities, except for items defined in Section 10.0. Design activities shall be featured in the program master schedule.

 

5.2 Working Groups and Trade Studies

 

5.2.1 Working Groups

[**Redacted**]

 

5.2.2 Trade Studies

Reserved.

 

5.3 Satellite Design Data

The satellite shall be designed such that the environmental design criteria of the Instrument as defined in the documents of paragraph 2.2 are not exceeded, and the structural, electrical, and thermal characteristics, as defined in the documents of paragraph 2.2, of the Instrument are accommodated.

DigitalGlobe shall provide information required to update the budgets for the Customer Furnished Equipment, consistent with paragraph 2.2.

 

5.3.1 Satellite to Instrument Interface Control Document(s) (CDIL D-1)

BATC shall produce and maintain the Satellite to Instrument ICD(s). The ICD(s) will address all interface issues including but not limited to: power, commanding, telemetry, mass and mass properties, mechanical envelope and mounting, thermal, fields-of-view, vibration and jitter isolation/management, and accommodation of bus components on the Instrument.

 

5.3.2 Satellite to Ground Terminal Narrowband Link ICD (CDIL D-2)

BATC shall produce and maintain the Satellite to Ground Station Narrowband Link ICD. This link will address both the command uplink and telemetry downlink.

 

5.3.3 Satellite to Ground Terminal Wideband Link ICD (CDIL D-3)

BATC shall produce and maintain the Satellite to Ground Terminal Wideband Link ICD.

 

 

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5.3.4 Satellite Environmental Design and Test Specification (EDTS) (CDIL D-4)

BATC shall prepare and maintain the EDTS, or equivalent document defining the component environmental design and test requirements. Electromagnetic Interference Design and Testing shall be in accordance with the standards specified in Satellite Specification.

 

5.3.5 Contamination Control Plan(s) (CDIL D-5)

[**Redacted**]

 

5.3.6 Satellite Level Requirements Verification/Compliance Matrix (CDIL D-6)

BATC shall produce a satellite level RVCM. The RVCM will include requirements from the Satellite Specification and the Instrument Specification if applicable. BATC shall update/maintain the Satellite RVCM to reflect changes to these parent specifications. DigitalGlobe shall have review and approval authority over changes to the RVCM. BATC shall include the following information in the RVCM

 

  a. Source of requirement (Parent specification document and paragraph number, i.e. satellite spec, instrument spec, etc)

 

  b. Specification paragraph

 

  c. Paragraph title

 

  d. Summary description of requirement

 

  e. Column indicating status of compliance

 

  f. Summary description of performance

 

  g. Responsible organization

 

  h. Verification Point [**Redacted**]

 

  i. Verification Method [**Redacted**]

 

  j. Verification Source Document indicating applicable paragraph, test sheet, etc.

 

  k. Comments, if required.

 

  l. Other information at BATC’s option

 

5.3.7 Box Level Requirements Verification/Compliance Matrix (CDIL D-7)

BATC shall flow down requirements from the Satellite Specification to box level requirements. BATC shall develop performance requirements for each box level component on the Satellite excluding CFE. For this paragraph, “box level component” also includes all components that are not really “box” like. These include but may not be limited to:

[**Redacted**]

BATC shall use the Box Level RVCM as an input into the box level performance test procedures. BATC shall demonstrate compliance to the box level RVCM.

 

5.3.8 Drawings (CDIL D-8)

A complete file of BATC drawings prepared for the WV3 program, will be maintained on file in electronic and hardcopy form, where appropriate. Electronic transfer to DigitalGlobe will constitute delivery.

 

 

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5.3.9 Performance Compliance and Risk Management

1.1.1.5    5.3.9.1    Performance Compliance (CDIL D-9)

The contractor shall supply at PDR a Performance Compliance Matrix identifying the performance estimate, allocated uncertainty (and/or contingency as appropriate) and resulting Total Performance (where Total Performance = performance estimate + uncertainty) for the following list. The Performance Compliance Matrix shall be updated and provided with each Quarterly Review following the PDR.

[**Redacted**]

DigitalGlobe shall provide performance information required to update the budgets for any of the Customer Furnished Equipment, in accordance with the documents in Paragraph 2.2.

1.1.1.6    5.3.9.2    Risk Management Report (CDIL D-10)

BATC and DigitalGlobe shall jointly develop and maintain a Risk Status Report. This report highlights known program risks, assigns risk levels, and documents mitigation strategies and status. BATC shall supply at PDR an initial Risk Status Report covering the system elements to be provided by this SOW. BATC shall updated the Risk Status Report monthly following the PDR.

 

5.3.10 Subsystem Description Documents (CDIL D-11)

BATC shall prepare Subsystem Description Documents for each satellite subsystem.

The Subsystem Description Documents will include as a minimum, unless provided in other deliverable documents, and referenced in the SDD:

 

a. Subsystem Overview including a detailed block diagram

 

b. Functionality and major performance characteristics of each Subsystem Component

 

c. Redundancy

[**Redacted**]

 

d. [**Redacted**]

 

e. [**Redacted**]

 

f. [**Redacted**]

 

g. Subsystem schematic including power, power returns, commands, and telemetry. This schematic shall be updated to reflect Engineering Change Orders.

 

h. Expected nominal operating methods and telemetry limits

[**Redacted**]

 

i. Operational constraints

[**Redacted**]

 

j. Fault Protection

[**Redacted**]

j.2 List the information available to the operator to reconstruct or identity the fault.

 

k. Interfaces between subsystem components

 

l. Major interfaces with other subsystems

The Subsystem Description Documents shall be delivered at CDR + 4 months. If changes require an update to the document, those updates shall be provided at approximately Launch – 4 months and again at Launch + 4 months. The subsystem schematic (item e.) shall be updated as required throughout the program to reflect Engineering Change Orders.

 

 

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5.3.11    Analysis and reports

 

BATC shall perform the following analyses. Updates shall be provided when changes significantly invalidate previous results.

 

  a. (1) Integrated Spacecraft Bus/Instrument thermal analyses, including summary of temperature predictions for unit level components under various operational modes and (2) unit-level thermal analysis [**Redacted**] . (CDIL D-12)

 

  b. Integrated Spacecraft Bus/Instrument structural analysis including [**Redacted**] . (CDIL D-13)

 

  c. Control system analysis including [**Redacted**]. (CDIL D-14)

 

  d. System Level Failure Modes and Effects and Criticality Analysis (FMECA). [**Redacted**] (CDIL D-15)

 

  e. Satellite Reliability Analysis BATC shall calculate satellite reliability using it’s standard process. [**Redacted**] (CDIL D-16)

 

  f. Satellite Life Prediction Data. DigitalGlobe needs to continually assess expected satellite life based upon actual on-orbit operational parameters. BATC shall provide all backup data used by BATC for sizing and life predictions. BATC does not need to produce a life expectancy analysis. DigitalGlobe will use the provided data and make our own Life Prediction. BATC can provide the life prediction data in one summary package, or in other CDILs.

 

  g. Flight Battery Life Prediction Analysis. BATC shall produce a life expectancy analysis for the satellite battery. The battery life prediction shall account for ground handling and will include a family of curves based upon pertinent on-orbit variables including but not necessarily limited to temperature and depth-of-discharge. (CDIL D-35)

 

  h. Satellite Imaging Performance (CDIL D-17)

BATC shall perform a comprehensive analysis regarding imaging performance. This is a comprehensive look at the numerous subsystem and trans-subsystem performance measures that affect imaging. The list includes but is not limited to:

[**Redacted**]

5.3.12    Other Interface Control Documents

BATC shall provide inputs, review, and verify BATC side of the following ICDs.

 

  a. Satellite to Launch Vehicle ICD

In the event that the ICDs require revision, the changes will be discussed between the affected parties to determine the most cost and schedule efficient manner to implement the change. If applicable, any impact will be covered under changes provision of the Contract.

5.3.13    Critical Items list (CDIL D-18)

BATC shall maintain a Critical Items List summarizing all known single point failures on the Satellite and any special efforts required to mitigate risk associated with them. It shall also contain any items requiring special handling due to a high potential of damage, mission criticality, or safety concerns.

 

 

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5.3.14    Component Heritage Summary (CDIL D-19)

The Component Heritage Summary will consist of a listing of all Satellite units by subsystem summarizing:

 

  a. Unit name

 

  b. Development / qualification history (e.g. engineering model, qual, protoflight)

 

  c. Previous flight heritage

 

  d. Modifications to previous uses

 

  e. Any significant known anomalies on flight units

5.3.15    Engineering Reports (CDIL D-20)

A complete file of all relevant Engineering Reports prepared on the WV3 program funding shall be maintained on file in electronic and hardcopy form where appropriate. Electronic transfer to DigitalGlobe will constitute delivery and shall occur within 5 business days of the ER release date. ERs delivered as a separate CDIL do not need to be delivered twice – once per this paragraph and again per the relevant CDIL paragraph. Those ERs need only be delivered once per the relevant CDIL paragraph.

(“Relevant” in this clause refers to all ERs containing design information, analyses, test data, etc that affect the performance and/or operations of the satellite. It does not include ERs that contain BATC proprietary cost data.)

5.3.16    Flight Software Source Code (CDIL D-21)

Per the terms of the software license agreement set forth in the Agreement, BATC shall grant to DigitalGlobe a limited license to use the flight software code. A copy of the flight software code, as identified below, shall be provided to DigitalGlobe on suitable media. Other elements of the software, as identified below, shall be placed in escrow per the Agreement.

[**Redacted**]

For units that are subcontracted by BATC, software and firmware shall be delivered if delivered to BATC and BATC has the right to deliver it to DigitalGlobe.

5.3.17    Composite Grounding Design (CDIL D-22)

[**Redacted**]

5.3.18    Structural, Power, Thermal, and Reliability Analytical Models (CDIL D-23)

BATC shall provide the analytical models used to predict the integrated spacecraft and instrument Structural [**Redacted**] , Power, and Thermal performance.

Satellite thermal performance modeling shall use the instrument thermal model provided by ITT. BATC shall use the integrated Satellite model to:

 

  a. Verify thermal interface requirements documented in the Spacecraft Bus to Instrument ICD are being met. Although BATC shall not be held contractually responsible for non-compliances on the ITT side of the interfaces, any such non-compliances revealed by Satellite thermal modeling shall be reported to DigitalGlobe.

 

 

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  b. Verify the Bus meets all of its requirements when modeled as a complete Satellite, for example unit temperatures and line of sight stability. BATC shall deliver line of sight motion vs. time profiles to DigitalGlobe (for incorporation into system geolocation budgets).

 

  c. Develop predicted temperature vs. time profiles of key instrument nodes as coordinated with ITT through the established ICD process. BATC shall deliver these temperature profiles to DigitalGlobe and forward a copy to ITT (so that ITT can verify the instrument meets its requirements).

BATC shall also provide the spacecraft bus reliability model down to the component and/or card level. Electronic transfer to DigitalGlobe will constitute delivery.

5.3.19     Coordinate Transformation Document (CDIL D-24)

BATC shall provide the documentation of all coordinate reference frames used in the satellite system including their reference points within the spacecraft. Nominal values for all transformations shall be provided. Reference frames requiring on-orbit calibration shall be noted. The document shall be updated with best-estimates from pre-launch calibrations and measurements.

5.3.20     Flight Software Users Manual (CDIL D-25)

BATC shall provide documentation of the flight software to include flowchart of routines/modules, structure and calling sequences, commands, telemetry, database constants and uploadable parameters, address tables, and log file definitions and locations.

5.3.21     Component Acceptance Data Package (CDIL D-26)

BATC shall provide or make available data acceptance packages for all major components.

5.3.22     [**Redacted**]

[**Redacted**]

5.3.23     Instrument/Sensor Boresight Stability Data (CDIL D-28)

[**Redacted**]

5.3.24     Position and Attitude Accuracy (CDIL D-29)

BATC shall provide detailed analysis and test data showing compliance with position and attitude accuracy requirements.

5.3.25     Satellite to MGB Interface Control Document(s) (CDIL D-32)

BATC shall produce and maintain the Satellite to MGB ICD(s). The ICD will address all interface issues including but not limited to: power, commanding, telemetry, mass and mass properties, mechanical envelope and mounting, thermal, fields-of-view, vibration and jitter isolation/management.

 

 

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5.3.26     DigitalGlobe to BATC Electrical GSE Interface Control Document (CDIL D-33)

BATC shall produce and maintain an ICD for the STOC-to-NarrowBand Rack interface. This includes but is not limited to: grounding, commanding, telemetry, data formats, etc.

 

 

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6.0 Product Assurance

 

6.1 Product Assurance Plan

The Contractor and its subcontractors shall have an established quality control system that meets the requirements of BATC’s Product Assurance Plan and BATC’s Supplier Product Assurance Plan

 

6.2 BATC Parts Control Board (PCB)

The Parts Control Board (PCB) shall be constructed as follows: A PCB will be established. The responsibility of this PCB is to ensure each EEE part was evaluated for performance relative to the requirements. With the exception of System Safety, the PCB will also be used as the forum to discuss other Systems Assurance/Product Assurance issues i.e., Materials and Processes, Reliability, etc. The PCB is responsible for the review and disposition of any noncompliance with BATC’s Product Assurance Plan.

The PCB consists of:

 

  a. BATC Product Assurance Manager (Chairman)

 

  b. BATC WV3 Product Assurance Specialist or designated alternate

 

  c. Designated technical specialist from the hardware/software product team as needed

 

  d. Other necessary disciplines as needed

 

  e. DigitalGlobe Designated Representative(s). (The DigitalGlobe member is a non-voting adjunct member).

 

6.2.1 Subcontractor Parts Control Board (PCB)

Subcontractor PCBs shall be established as necessary to implement BATC’s supplied Product Assurance Plan. It is BATC’s responsibility to verify compliance.

 

6.2.2 PCB Meetings

PCB meeting shall be convened as needed. BATC shall notify DigitalGlobe of upcoming meetings at least 2 working days in advance. DigitalGlobe attendance is optional BATC shall maintain meeting minutes to document all decisions and will provide a copy of the minutes to DigitalGlobe within 5 working days.

The minutes may be informal and in most cases shall be delivered to DigitalGlobe electronically via e-mail.

Minimal PCB approval/disposition signatures include BATC PAM and BATC WorldView Product Assurance Specialist or his designated alternate. Once the PCB approves a part, the Parts Engineer will indicate approval on the Advanced or Program Parts List (A/PPL).

 

 

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6.3 Parts and Materials

 

6.3.1 Electrical, Electronic, and Electro-mechanical Parts (EEE)Parts Listing (CDIL QA-1)

BATC shall prepare, maintain, and deliver a EEE Parts Listing for all satellite hardware except for Customer Furnished Equipment. This listing shall identify all EEE parts intended to be used by BATC and it’s vendors. For each part, the following minimum information shall be identified: manufacturer, description, lot date code. Parts shall be qualified as compared to BATC product assurance criteria and the Satellite Specification and the Satellite Specification Addendum. BATC’s internal process and format for EEE Parts Listing may be utilized.

The Parts List shall be maintained and reviewed by BATC as necessary, but minimally it shall be updated and provided to DigitalGlobe at the following:

 

  a. Prior to manufacturing for each box/component At this phase, it is acknowledged by DigitalGlobe and BATC that the list may be incomplete due to part shortages.

 

  b. Prior to box/component level Test Readiness Review

 

  c. Prior to the integration of any box/component onto the Bus.

 

6.3.2 Material and Processes Reports (CDIL QA-2)

BATC shall prepare and deliver reports documenting their approval of all materials and processes planned for use on the Bus.

 

6.4 As-Built Configuration and Conformance

 

6.2.1     6.4.1 As-Built Configured Article List (CDIL QA-3)

The as-built configured article status shall be maintained throughout the production program in the certification logs and production orders. At the conclusion of integration, the information shall be used to generate the preliminary As-built Configured Article List. After test and modification (if any) the List shall be finalized and presented.

 

6.2.2     6.4.2 Certificate of Conformance (CDIL QA-4)

A Certificate of Conformance shall be generated and signed off by Product Assurance and Program Management. It details the conformance (and exceptions) to the SOWs, specifications and other contractual documents for the delivered article. This Certificate of Conformance shall be delivered to DigitalGlobe at the Launch Readiness Review.

 

6.5 Product Assurance Reviews (CDIL QA-5)

The plan shall include a program for the periodic audit of portions of the Contractor’s Product Assurance System in each of the below activity areas to confirm conformance to the requirements. These audits will be conducted by the Program Product Assurance engineer. BATC shall inform DigitalGlobe of the audit results.

 

  a. Reliability

 

  b. Parts Procurement

 

 

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  c. Materials and Processes

 

  d. Non-Conforming Material Control

 

  e. Configuration Management

 

  f. Safety

 

6.6 Documentation

Documents shall be submitted or made available to DigitalGlobe as indicated in the list provided in Attachment 1.

 

6.7 Known Non-Compliant Hardware

[**Redacted**]

 

6.8 Military Standard 461

[**Redacted**]

 

 

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7.0 Procurement

 

7.1 General

BATC shall be responsible for the work associated with the procurement of all material and subcontracts required to provide the deliverable items, except for the CFE items identified in Section 10.0. BATC shall procure according to the CSO Supplier Product Assurance Plan. Procurement activities shall be featured in the program master schedule.

 

7.2 Make/Buy Plans (CDIL PT-1)

BATC shall identify Make/Buy plans for all Satellite components.

 

7.3 Encryption/Decryption Devices

[**Redacted**]

 

7.4 Reviews

A series of reviews shall be established with each subcontractor. A schedule of these reviews shall be included in the Review Listings required by paragraph 4.5.3. The reviews will generally be held at the vendor and DigitalGlobe personnel may attend, at their option.

 

7.5 Program Subcontract Status Report (PSSR) (CDIL PT-2)

BATC shall prepare a Program Subcontract Status Report (PSSR) for the program. The PSSR will contain critical status information on each major subcontract (larger than $1M) relative to:

 

   

Design & development

 

   

Procurement and Production

 

   

Assembly

 

   

Integration

 

   

Test, including any anomalies

 

   

Delivery schedule

 

   

Reviews

 

7.6 Documentation

Documents shall be submitted or made available to DigitalGlobe as indicated in the list provided in Attachment 1.

 

7.7 Subcontract Flow-downs

 

7.7.1     Assignment Clause

[**Redacted**]

 

7.7.2     Access

[**Redacted**]

 

 

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8.0 Production Activities

 

8.1 General

BATC shall appoint a Production engineer responsible for ensuring that BATC’s production capabilities match the requirements of the program. With the support of the Program QA engineer, he shall ensure that the production facilities comply with the Product Assurance requirements.

BATC shall be responsible for the work associated with the production of the deliverable items, except for the CFE items identified in Section 10.0. BATC shall be responsible for the production activities associated with integrating the CFE items as defined in Section 10.

Production activities shall be featured in the program master schedule.

 

8.2 Production Process

BATC shall produce the deliverable hardware according to applicable BATC standardized procedures. As a minimum, standardized BATC procedures shall be followed for the following topics:

[**Redacted**]

 

8.3 Access

The production manager shall arrange access for the DigitalGlobe staff to BATC manufacturing areas where manufacturing activities associated with the program are taking place.

 

8.4 Production Documentation

Production orders and Certification Logs shall document the as-built configuration. These logs shall be available on-site for DigitalGlobe review.

 

 

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9.0 Integration and Test Activities

 

9.1 General

For the WV program the Integration and Test activities fall into four logical categories.

 

  a. Box level / Subsystem level testing

 

  b. Bus level integration and testing including integration of the instrument

 

  c. Satellite level testing

 

  d. Mission and Launch Rehearsals

The Integration and Test Manager shall be responsible to ensure that BATC’s integration and test capabilities match the requirements of the program

BATC shall accomplish the work associated with a-d above for all BATC supplied hardware/software. BATC shall accomplish the work associated with b-d above for all CFE.

 

9.2 Box/Subsystem Level Testing

 

9.2.1 General

BATC shall perform all box level testing per environmental design and test specification and the box level Requirements Verification and Compliance Matrix.

 

9.2.2 [**Redacted**]

[**Redacted**]

 

9.3 WV Bus and Satellite Integration and Test Plans (CDIL PT-3)

BATC shall develop a WV Bus and Satellite Integration and Test Plan (Satellite I&T Plan) for the WV3 satellite. The test plans will include all I&T activities starting from the installation of the first component on to the bus structure through launch.

The WV I&T Plan(s) shall:

[**Redacted 4 Pages**]

 

9.4 Post-Shipment Instrument Testing

ITT will perform post-shipment functional testing to verify the Instrument survived shipment without damage. ITT will provide the necessary test equipment for the Instrument.

BATC shall provide:

[**Redacted**]

For schedule purposes the Instrument is not considered delivered to BATC upon arrival at BATC facility. Rather the instrument is considered delivered on the date that the Instrument has completed all necessary post-shipment testing and is ready and available for BATC to integrate to the telescope/bus.

 

 

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9.5 Supporting Documents

BATC shall provide as a minimum the following support documents:

 

  a. All necessary box level test procedures, integration procedures, and system level test procedures. Each procedure shall include a detailed test description explaining the “what, how, and why” of each test.

 

  b. A System Level Test Matrix. The test matrix will identify which System Level Test procedures or portions of those procedures will be accomplished at each test phase. The System Level Test phases include, but are not limited to:

[**Redacted**]

 

9.6 System Test Reports (CDIL PT-5)

[**Redacted**]

 

9.6.1 Content

The report shall include a summary of satellite configuration, test objectives, test results, significant hardware/software anomalies if any, resolution of significant anomalies, and a copy of all telemetry plots or other post-test data. The cognizant test engineer and the appropriate subsystem engineer(s) shall sign the report.

 

9.6.2 Timeliness

BATC shall publish the test reports No Later Than 15 working days after test completion.

 

9.7 Uninterruptible Power Supply (UPS)

[**Redacted**]

 

9.8 DigitalGlobe Integration and Test Engineering Access

 

9.8.1 On-Site and Visiting Engineers

BATC shall provide dedicated cubicle space, furniture, high-speed internet access, and phone lines for three resident DigitalGlobe I&T engineers. These DG on-site engineers will serve as the I&T focal point between DG and BATC. It is anticipated these engineers will be on-site at BATC on a full-time basis. BATC shall provide dedicated cubicle space, furniture, high-speed internet access, and phone lines for one visiting DigitalGlobe engineer.

 

9.8.2 Access to Live Satellite Telemetry

Once power-on bus integration begins, BATC shall provide DG with access to the live satellite telemetry from the cleanroom. DG will provide the necessary hardware to connect the Mission Control Center (MCC) to BATC GSE. DG will man and operate the DG hardware as necessary to flow the telemetry to the MCC. DigitalGlobe access to telemetry will occur on a non-interference basis to BATC test team.

 

 

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9.8.3 Test Observation By Other DG Engineers

BATC shall allow other DG satellite and ground system engineers access to the cleanroom to witness satellite testing. BATC is not obligated to coordinate, inform, or schedule testing according to DG engineer availability.

 

9.8.4 Access to Command and Telemetry Log Files (CDIL PT-6)

BATC shall deliver an archive of all command and telemetry files from satellite integration and test in an electronic format. BATC shall deliver an update weekly. Electronic transfer to the DG server shall constitute delivery. BATC shall maintain information about which command and telemetry database was used in delivered files as well as which test procedures were run in each file.

 

9.9 Test Reviews

The status of the Satellite shall be reviewed during the test phases of the program. See paragraph 4.5.3.2 for the list of reviews and required content.

 

9.10 Optional Testing

The following is a list of optional tests to be performed or supported by BATC. These are tests DigitalGlobe may choose to have BATC perform if the schedule permits. BATC should not show these tests in the baseline schedule. In each case after a test option is exercised by DigitalGlobe, BATC has 30 calendar days to prepare for the test. BATC shall provide a separate option price prior to the start of I&T for each of these tests.

[**Redacted**]

 

 

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10.0 Customer Furnished Equipment and Services

 

10.1 General

DigitalGlobe has contracts with vendors other than BATC who are responsible for providing portions of the overall system. DigitalGlobe has the responsibility for monitoring, administering, and verifying performance of those subcontracts. This section defines the items and support requirements that DigitalGlobe is responsible for securing and providing to BATC via these other subcontractors. This section also defines the equipment that DigitalGlobe is responsible for providing directly.

The delivery of all items shall be per Attachment 2: Customer Furnished Equipment list. DigitalGlobe will also arrange for the return of loaned equipment, if required, at no cost to BATC. CFE items shall be featured in the program master schedule. Unless otherwise explicitly provided to the contrary in Attachment 2, title to all equipment identified in this Section 10.0 shall remain in DigitalGlobe.

 

10.2 Flight Equipment

[**Redacted**]

 

10.2.1    [**Redacted**]

[**Redacted**]

 

10.2.2    [**Redacted**]

[**Redacted**]

 

10.2.3    [**Redacted**]

[**Redacted**]

 

10.2.4    [**Redacted**]

[**Redacted**]

 

10.2.5    [**Redacted**]

[**Redacted**]

 

10.2.6    [**Redacted**]

[**Redacted**]

 

10.3 Simulators (CSIM-1)

[**Redacted**]

 

 

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10.4 Launch Vehicle Interfaces

 

10.4.1     Launch Vehicle Interface

DigitalGlobe shall provide a launch vehicle interface adapter to BATC (CLSE-1). BATC shall use this for a fit check and for a separation test as described in paragraph 9.3.e. DigitalGlobe shall provide a match drill template to BATC (CLSE-2).

 

10.4.2    Launch Vehicle Separation Connectors (CLSE-3)

DigitalGlobe shall provide the flight satellite/launch vehicle separation connectors.

 

10.5 Ground Support Equipment

 

10.5.1    Wideband Link RGT Equipment

DigitalGlobe will provide a set of RGT ground equipment for capturing Instrument data in the cleanroom. Nominally, this will include the following equipment and documentation:

[**Redacted**]

 

10.5.2    Narrowband Link RGT Equipment (CGSE-5)

DigitalGlobe will provide a set of RGT ground equipment for processing the S-band uplink and X-band narrowband downlink in the cleanroom. The capability to bypass the RF sections and operate at a baseband Satellite interface shall be provided by BATC. This may include elements of the Mission Control Center [**Redacted**] as dictated by the architecture of the ground system. DigitalGlobe shall deliver to BATC operating documentation and interface details one month prior to delivery.

This equipment shall include: [**Redacted**]

 

10.5.3     Special Test Equipment

DigitalGlobe shall provide special WB Link / WB receiver test equipment for WB link development and testing. This will include:

[**Redacted**]

 

10.5.4    Mission Control Center (CGSE-11)

DigitalGlobe will provide portions of the Mission Control Center (MCC) and software as required to support the Satellite Integration and Test Plan, via data links between the MCC in Longmont, CO and BATC. BATC shall be responsible for work on the Satellite required to resolve problems associated with the Satellite performance and function. All work associated with resolution of DigitalGlobe provided ground equipment and interfaces shall be at DigitalGlobe expense.

 

10.5.5     [**Redacted**]

[**Redacted**]

 

 

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10.5.6     [**Redacted**]

[**Redacted**]

 

10.5.7     [**Redacted**]

[**Redacted**]

 

10.5.8     MGB Test Equipment (CGSE-15)

DigitalGlobe shall provide a signal generator, up-converter, feedhorn, and control computer.

 

10.6 Launch Vehicle Data (CLD-1 and CLD-2)

DigitalGlobe shall provide a preliminary and final Coupled Loads Analysis (CLA) to BATC from the Launch Services contractor.

 

10.7 Instrument Data

DigitalGlobe shall provide the WV3 instrument data and models, as specified in Paragraph 2.2, to support satellite level analysis and modeling for the areas listed below. BATC shall be responsible for additional data to support the provisions of this document and the spacecraft specification.

 

10.7.1     Instrument Structural Analysis Data (CID-1)

DigitalGlobe shall provide the WV3 instrument structural data and model.

 

10.7.2     Instrument Thermal Analysis Data (CID-2)

DigitalGlobe shall provide WV3 instrument thermal data and model.

 

 

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11.0 Storage and Delivery

 

11.1 General

BATC shall be responsible for storage, if required, and delivery of the WV3 Satellite in accordance with the following paragraphs.

 

11.2 Satellite Pre-Shipment Storage

In the event that the Satellite is completed prior to the contractually scheduled delivery date, BATC shall provide, at their cost, suitable environmentally controlled storage including temperature and humidity monitoring and recording.

If shipment is delayed due to BATC beyond the contractually scheduled delivery date and the Satellite is complete, and such delay by BATC has caused a loss of available launch opportunity, the Satellite shall be placed in storage at BATC’s expense.

If shipment is delayed due to DigitalGlobe beyond the contractually scheduled delivery date and the Satellite is complete, the Satellite shall be placed in storage at DigitalGlobe’s expense.

 

11.3 Pre-Shipment Re-Test

Subject to the length of the storage period, appropriate maintenance and power up of those units sensitive to inactivity shall be undertaken. Any items exhibiting signs of deterioration shall be subject to appropriate follow up action according to the circumstances. All instances shall be reported to DigitalGlobe.

A thorough re-test is required should the storage exceed [**Redacted**] . Details shall be provided in the test requirements document. Appropriate follow up action shall be taken, according to the circumstances, should any problems be detected.

The re-test costs shall be at BATC expense if delay and retest were caused by BATC. The re-test costs shall be at DigitalGlobe’s expense if delay and retest were caused by DigitalGlobe.

 

11.4 Satellite Shipping and Delivery

[**Redacted**]

BATC shall provide shipping from BATC plant to the launch site. BATC shall pack the Satellite and ground support equipment in suitable containers for shipment to the launch site. BATC shall unpack the Satellite and ground support equipment at the payload processing facility at the launch site.

BATC shall provide insurance and security for the satellite and ground support equipment during shipment to the launch site.

BATC shall pack the ground support equipment for return to BATC plant and provide shipping.

BATC shall provide insurance for the ground support equipment during shipment back to BATC plant.

The transportation environment shall be enveloped by the requirements in the Launch Vehicle and Instrument ICD and performance specification. BATC shall be responsible for ensuring the Satellite compatibility with the requirements. BATC shall be responsible for verifying all environmental requirements are met including temperature, humidity, and shock monitoring.

 

 

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11.5 Satellite Launch Site Storage

BATC shall provide volumetric storage and access requirements to DigitalGlobe for shipping containers required at the launch site. The baseline program assumes no Satellite storage requirements at the launch site. However, if the launch should be delayed once the Satellite has been shipped, BATC shall provide, at DigitalGlobe expense, the support necessary to maintain, store, and retest the Satellite.

 

 

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12.0 Launch Support Services

BATC shall provide launch support services as defined in the following paragraphs.

 

12.1 General

[**Redacted**] DigitalGlobe will be responsible for overall coordination of launch activities. BATC shall support this activity as defined in this section of the SOW.

The Satellite shall be compatible with U.S. launch safety requirements. BATC shall generate a WV3 Missile System Pre-launch Safety Package (MSPSP) (CDIL LM-1) to document hazardous items or operations and planned safety procedures for the Satellite.

BATC shall support the safety review processes of the Launch Services Contractor and the Launch site.

 

12.2 Requirement Definition

BATC shall support the generation and maintenance of the Launch Vehicle ICD as defined in paragraph 5.3.12. BATC shall supply the following information and any other information normally required by the Atlas V Launch Services User’s Guide to DigitalGlobe and the Launch Services contractor:

 

  a. Launch vehicle interface details and requirements.

 

  b. Requirements for launch site support and services including space, power, environment, contamination control, lifting/moving, telecommunications, etc.

 

  c. Statement of compliance with launch site safety requirements.

 

  d. Environmental requirements pre and post installation on launch vehicle.

 

  e. Verification of applicable portions of the Satellite to Launch Vehicle ICD.

 

  f. Launch Site Procedures.

BATC shall, by means of drawings, analysis, or test, be responsible for specifically confirming Satellite compatibility with the launch vehicle requirements defined in the ICD. BATC shall prepare a RVCM, as defined in paragraph 5.3.6, for those portions of the ICD for which it has responsibility.

 

12.3 Technical Interchange Meetings

BATC shall support up to twenty Technical Interchange Meetings (TIM) with the launch organization . [**Redacted**] In addition, BATC will support informal meetings and teleconferences at DigitalGlobe’s Colorado facilities and BATC facility as required resolving interface and infrastructure issues.

 

12.4 FEM and CLA-to-Design Load Comparisons (CDIL LM-2)

BATC shall provide preliminary Finite Element Models (FEM) and final FEMs for the WV3 Satellite for the purposes of performing coupled loads analyses. DigitalGlobe is responsible for obtaining valid CLA results from the launch service contractor and delivering those to BATC. BATC shall then compare the results of the coupled loads analyses to the design loads used in spacecraft bus and Instrument structural analysis to confirm that the resulting loads are within the design requirements as specified in the respective ICDs. The deliverables are as follows:

[**Redacted**]

 

 

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12.5 Export Regulations

All contractors on this program are anticipated to be U.S. companies including the launch service contractor. Therefore we anticipate no exports of hardware, software, or technology to foreign companies. However, if that situation changes, DigitalGlobe shall be the single point of contact for all export issues. Therefore:

BATC shall provide information directly to DigitalGlobe and DigitalGlobe will be responsible for obtaining and documenting all export approvals for all documentation transmitted to the launch vehicle agencies.

DigitalGlobe will be responsible for all work associated with compliance to export regulations including licensing, security, customs, document approval, transportation, etc. for documents/data channeled through DigitalGlobe.

It is understood that the Department of State International Traffic in Arms regulations (CFR 22 Part 120 through 130) strictly apply to any data or hardware covered under this SOW.

 

12.6 Adapter Fit-Check

BATC shall perform a launch vehicle interface check on the satellite as defined in the Test Plan. DigitalGlobe will arrange for the launch services contractor to provide the adapter, interface portions of the separation system, and GSE. If required, DigitalGlobe will also arrange for support from the launch services contractor at no cost to BATC.

 

12.7 Launch Site Infrastructure

DigitalGlobe shall arrange for and provide all launch site infrastructure necessary for satellite testing and pre-launch processing. This includes lease of a satellite processing facility.

 

12.8 Launch Site Operations

BATC shall support the launch operations campaign including provision of the test equipment and labor required to perform the launch site unpacking, Satellite checkout as defined by the WV I&T Plan, fueling, final mating to launch vehicle, launch, and repacking for return to BATC plant. Delays associated with BATC performance shall be at BATC expense. Any other delays shall be at DigitalGlobe expense. BATC will be responsible to support meetings for the purpose of coordinating launch site operations including joint operations with the launch services contractor. All efforts associated with reprocessing due to a cancelled or aborted launch shall be at DigitalGlobe expense.

 

12.9 Fueling

BATC shall prepare a fueling plan and the procedures required for fueling the Satellite using an appropriate fueling cart. BATC shall prepare the fueling equipment for hydrazine loading operations and package for shipment to the launch site. BATC shall be responsible for a single fuel loading operation unless multiple fuelings are required due to reasons under BATC’s control.

 

 

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BATC shall provide all required consumables, propellant, safety training, and safety equipment including SCAPE gear required to effectively and safely perform satellite fueling operations. DigitalGlobe shall arrange for disposal of all hazardous wastes and any excess materials through its Launch Services provider.

BATC shall provide support to the launch vehicle/range contractor as required to respond to range specific requirements as they pertain to the handling of the hydrazine operations.

 

 

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13.0 Mission Preparation and On-Orbit Commissioning

BATC shall assist with Mission preparation and On-orbit Commissioning by performing the following tasks and engineering services.

 

13.1 Training (CDIL LM-3)

13.1.1    Training Materials

BATC shall develop a training package for each satellite subsystem including the operation of the Instrument to address specifically the changes between WV-2 and WV3. The training package will be based on the Subsystem Description Documents (Paragraph 5.3.10) and include the same minimum information.

The training packages will be delivered on both paper and electronic media.

13.1.2    Training Sessions

For each subsystem, a cognizant BATC subsystem engineer shall present the training materials from paragraph 13.1.1. DigitalGlobe will provide the conference room and necessary projectors to support the presentation. DigitalGlobe reserves the right to videotape the training sessions for the purpose of training future DigitalGlobe personnel.

 

13.2 Command and Telemetry Handbook (CDIL LM-4)

BATC shall prepare a command and telemetry handbook. This document shall provide a definitive listing of all satellite telemetry and commands with a full description for each. The handbook shall meet the requirements identified in WV159.

 

13.3 Bus Subsystem Calibration Tools (CDIL LM-5)

BATC shall provide the subsystem calibration tools necessary for on-orbit calibration activities. Depending upon the final satellite design, these tools include but may not be limited to:

[**Redacted**]

 

13.4 DigitalGlobe Procedure Development Support

DigitalGlobe will generate the on-orbit procedures for the WV3 satellite(s). BATC shall understand the DigitalGlobe Concept-of-Operations and assist the procedure development. BATC shall review DigitalGlobe developed procedures for technical, operational, and safety concerns. [**Redacted**]

 

13.5 Commissioning Plan (CDIL LM-6)

DigitalGlobe shall generate the Commissioning Plan for the WV3 satellite. BATC shall assist the commissioning plan development. This includes assisting with the definition of the nominal sequence of events, required prerequisites, allowed out-of-sequence events, and required technical support for each event. DigitalGlobe will provide information about ground contacts, mission control center operations, and other necessary ground information used to create the commissioning plan(s).

 

 

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The Commissioning Plan shall include subsystem initialization, calibration, and demonstration of performance requirements including, but not limited to, the following:

[**Redacted**]

 

13.6 Anomaly Preparations

DigitalGlobe will generate anomaly resolution flow-charts. BATC shall assist with the anomaly flow-chart development including defining the probable anomalies and proper recovery actions/sequences. BATC shall review DigitalGlobe anomaly resolution flow-charts for technical, operational, and safety concerns.

 

13.7 Satellite Commissioning

 

13.7.1     Launch and Early Operations (LEOP) Phase

DigitalGlobe shall direct Satellite Launch and Early Operations. BATC shall provide a dedicated engineer for all satellite subsystems except for the Instrument subsystem. This support will run 24 hours per day for up to 7 days at the DigitalGlobe Mission Control Center in Longmont, CO.

 

13.7.2     Verification and Calibration (V&C) Phase

DigitalGlobe shall conduct the Verification and Calibration activities necessary to achieve Full Operational Capability (FOC). This includes but is not limited to satellite calibration activities such as star tracker and gyroscope calibrations.

Barring anomalies, V&C activities will nominally occur between 0600 and 1800 hours seven days per week. V&C activities will nominally require 30 days. BATC shall provide a dedicated engineer for all satellite subsystems except for the Instrument subsystem.

BATC shall also provide off-hour, on-call engineering support during V&C. A 30 minute or less call-back response is required.

 

1.1.1.7    13.7.2.1        Commissioning Reports (CDIL LM-7)

BATC shall produce a Commissioning Report. The report will document spacecraft bus Beginning-of-Life (BOL) performance and will update End-of-Life (EOL) performance predictions for all subsystems for which it has responsibility. At a minimum the report shall include:

 

  a. An explanation of significant deviations from performance metrics as identified in the satellite specification. The explanation shall include the reasons for the performance delta and the anticipated effects, if any, on the subsystem or satellite.

 

  b. An explanation of any known component or sub-component failures encountered during the LEOP or V&C Phases. The explanation shall include the possible causes of the failure, workarounds, updated reliability analysis for the component, subsystem, and satellite, and any impacts to DigitalGlobe’s concept of operation.

 

 

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13.8 Satellite Simulator

BATC shall provide a high fidelity dynamic satellite simulator. The simulator shall simulate satellite responses to stimuli. BATC shall provide sufficient documentation to accurately capture the design, functionality, capabilities, limitations, maintenance, extension, and operation of the simulator.

 

13.8.1     Satellite Simulator (CDIL LM-8)

BATC shall deliver a high fidelity satellite simulator per the requirements document [**Redacted**] . [**Redacted**] BATC and DigitalGlobe shall mutually agree upon a computer hardware and operating system, called the computing platform, for use in simulator functional and performance acceptance testing. BATC shall execute spacecraft simulator acceptance testing on the identified platform. DigitalGlobe shall execute the simulator testing on the same platform.

The satellite simulator does not need to include the MGB subsystem.

 

13.8.2     Documentation (CDIL LM-9)

BATC shall provide a Users manual with sufficient detail to:

 

   

Develop simulation scenarios including all configuration files, scripts, procedures, ephemeris, initial conditions, etc

 

   

Start-up, shut-down, and operate the simulation console and all simulator components

 

   

Control the simulation in real-time by setting/adjusting variables

 

   

Inspect low level model telemetry through the simulation console and simulator components directly

 

   

Save, modify, and load simulator state files used to start, pause, resume, and diagnose simulation scenarios

 

   

Understand all log files and log entries

 

   

Understand and recover from all error conditions

 

   

Extend, modify, maintain, build and release the simulator.

 

   

Incorporate a new flight software release into the simulator

In this context, “maintain” refers to the functions required to upgrade to new versions of commercial products such as MatLab or Simulink, alter configuration files, or otherwise customize the implementation.

 

13.8.3     Source Code (CDIL LM-10)

Per the terms of the software license agreement set forth in the Agreement, BATC shall provide all BATC developed bus simulator software components in source format (non binary). Source code shall be delivered in originating and native format. BATC does not need to provide development tools or COTS software, but BATC shall provide COTS software tool configuration including supplier, part number, and revision levels of tools used (e.g. compilers, linkers, and other development tools) and all reasonable data/information necessary for DigitalGlobe to enhance, modify, compile, and deploy the simulator.

 

 

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13.8.4     Delivery Schedule

BATC shall provide the simulator, manuals, and source code per Attachment 1. BATC shall deliver an updated simulator based upon LEOP/commissioning on-orbit performance. At a minimum, the following subsystem models will be updated: thermal, power, and ADCS models.

 

13.8.5     Technical Interchange Meetings and Design Reviews

BATC shall include DigitalGlobe in technical interchange meetings and design reviews such that DigitalGlobe can explain the intent behind various simulator requirements. BATC and DigitalGlobe shall refine high level requirements to detailed requirements during technical interchange meetings. BATC shall hold preliminary and critical design reviews for the Satellite Simulator. BATC shall hold intermediate Technical Interchange Meetings for the following modules at a minimum: the console, sensor and actuator models, redundancy modeling, fault modeling, thermal modeling, and power modeling.

 

13.9 Maneuver Planners

[**Redacted**]

 

13.9.1    [**Redacted**]

[**Redacted**]

 

13.9.2     [**Redacted**]

[**Redacted**]

 

13.9.3     [**Redacted**]

[**Redacted**]

 

13.10    Software Test Bench

BATC shall maintain a test bench suitable for the development and troubleshooting of the satellite computer Flight Software. The bench will include at a minimum:

[**Redacted**]

 

13.11    Ground Stations

DigitalGlobe is responsible for all Ground Station equipment. DigitalGlobe operators will be the lead operators of the Ground Segment.1

 

13.12    Telemetry Packet Creation and Mapping Tools (CDIL LM-15)

BATC shall provide the documentation, software, and training necessary for making changes to the telemetry received from the satellite. This includes changes to both telemetry packets and the mapping of those packets into various telemetry streams under CCSDS Grade C protocol.

 

 

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Initial delivery shall coincide with initial delivery of the Command & Telemetry Handbook (C&TH). BATC shall update if necessary at a. launch minus 6 months, b. final pre-launch C&TH delivery, and c. launch plus 6 months. Training shall occur coincident with Training Sessions specified in section 13.1 with delta training, if needed, at the final pre-launch C&TH delivery.

 

13.13    Telemetry Monitor and Response (CDIL LM-16)

BATC shall provide the documentation, software, and training necessary for making changes to flight software telemetry monitors and response actions on the satellite. This includes creation of new telemetry monitors and response actions, and changes to existing monitors and response actions.

Initial delivery shall coincide with initial delivery of the Command & Telemetry Handbook (C&TH). BATC shall update if necessary at a. launch minus 6 months, b. final pre-launch C&TH delivery, and c. launch plus 6 months. Training shall occur coincident with Training Sessions specified in section 13.1 with delta training, if needed, at the final pre-launch C&TH delivery.

 

14.0 Communications Flexibility and TT&C Definition

BATC shall work with DigitalGlobe to set/finalize satellite ID’s by CDR.

 

15.0 Facilities

BATC shall provide all facilities necessary to perform the scope of this SOW.

 

 

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ATTACHMENT 1        CONTRACT DATA ITEMS LIST

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

PROGRAM MANAGEMENT

PM-1    Program Management Structure   

4.2

   [**Redacted**]    As req’d   
PM-2    Master Program Schedule   

4.4

   [**Redacted**]    monthly   
PM-3    Component/Subsystem Design Review Listing   

4.5.4

   [**Redacted**]    As req’d   
PM-4    Component/Subsystem Test Readiness / Data Review Listing   

4.5.5

   [**Redacted**]    As req’d   
PM-5    Documentation Listing   

4.6.3

   [**Redacted**]   

No later than

Bi-monthly

  
PM-6    Action Item List   

4.7

   [**Redacted**]    As req’d   
PM-7    Historical Record of Payments & Payments Forecast   

4.8.1 & 4.8.2

   [**Redacted**]    monthly   

DESIGN

              
D-1    Satellite to Instrument ICD   

5.3.1

   [**Redacted**]    As req’d   
D-2    Satellite to Ground Station Narrowband ICD   

5.3.2

   [**Redacted**]    As req’d   
D-3    Satellite to Ground Station Wideband Link ICD   

5.3.3

   [**Redacted**]    As req’d   
D-4    Satellite Environmental Design and Test Specification   

5.3.4

   [**Redacted**]    As req’d   
D-5    Contamination Control Plan   

5.3.5

   [**Redacted**]    As req’d   
D-6    Satellite Level Requirements Verification/Compliance Matrix   

5.3.6

   [**Redacted**]    As req’d   
D-7    Box Level Requirements Verification/Compliance Matrix   

5.3.7

   [**Redacted**]    As req’d   
D-8    Drawings   

5.3.8

   [**Redacted**]    with EOs   
D-9    Performance Compliance Matrix   

5.3.9.1

   [**Redacted**]    Quarterly   
D-10    Risk Management Report   

5.3.9.2

   [**Redacted**]    Monthly   

 

 

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Attch 1 - 1


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Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

D-11    Subsystem Description Docs   

5.3.10

   [**Redacted**]   

Launch – 4 m;

Launch + 4 m

   Updates only as required
D-12    Thermal Analysis and Reports   

5.3.11.a

   [**Redacted**]    As req’d   
D-13    Structural Analysis   

5.3.11.b

   [**Redacted**]    As req’d   
D-14    Control System Analysis   

5.3.11.c

   [**Redacted**]    As req’d   
D-15    Failure Modes and Effects and Criticality Analysis (FMECA)   

5.3.11.d

   [**Redacted**]    As req’d   
D-16    Satellite Reliability Analysis   

5.3.11.e

   [**Redacted**]    As req’d   
D-17    Satellite Imaging Performance   

5.3.11.h

   [**Redacted**]    As req’d   
D-18    Critical Items List   

5.3.13

   [**Redacted**]    As req’d   
D-19    Component Heritage Summary   

5.3.14

   [**Redacted**]    As req’d   
D-20    System Engineering Reports   

5.3.16

   [**Redacted**]      
D-21    Flight Software Code   

5.3.16

   [**Redacted**]   

As req’d Final

@ PSR

  
D-22    Composite Grounding Design   

5.3.17

   [**Redacted**]    As req’d   
D-23    Structural, Power, Thermal, and Reliability Analytical Models   

5.3.18

   [**Redacted**]    L+3 m   
D-24    Coordinate Transformation Document   

5.3.19

   [**Redacted**]    L – 4m   
D-25    Flight Software Users Manual   

5.3.20

   [**Redacted**]    As req’d   
D-26    Component Acceptance Data Package   

5.3.21

   [**Redacted**]    As req’d   
D-27    Jitter Analysis and Test Data   

5.3.22

   [**Redacted**]    As req’d   
D-28    Telescope Boresight Stability Data   

5.3.23

   [**Redacted**]    As req’d   
D-29    Position and Attitude Accuracy   

5.3.24

   [**Redacted**]    As req’d   
D-30    PDR Data Package   

4.5.3

   [**Redacted**]    As req’d   
D-31    CDR Data Package   

4.5.3

   [**Redacted**]    As req’d   
D-32    Satellite to MGB ICD   

5.3.25

   [**Redacted**]    As req’d   

 

 

ITAR Controlled Document - DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

Attch 1 - 2


LOGO    WV3 Satellite Statement of Work   
   Doc Number 10329656

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

D-33    Electrical GSE ICD   

5.3.26

   [**Redacted**]    As req’d   
D-34    Satellite Requirements Review   

4.5.3.1

   [**Redacted**]      
D-35    Battery Life Prediction   

5.3.11.g

   [**Redacted**]    L+ 1m   
PRODUCT ASSURANCE            
QA-1    EEE Parts List   

6.2.1

   [**Redacted**]      
QA-2    Material Identification and Use Listing   

6.2.2

   [**Redacted**]    See para 6.3.2   
QA-3    As built configured article list   

6.3.1

   [**Redacted**]    At Launch Readiness Review   
QA-4    Certification of Conformance   

6.3.2

   [**Redacted**]      
QA-5    Product Assurance Reviews   

6.4

   [**Redacted**]      
PROCUREMENT, PRODUCTION & TEST         
PT-1    Make / Buy Plans   

7.2

   [**Redacted**]    As req’d   
PT-2    Program Subcontract Status Report   

7.5

   [**Redacted**]    monthly   
PT-3    WV I&T Plan   

9.3

   [**Redacted**]    As req’d   
PT-4    Battery Maintenance Plan   

9.3.d

   [**Redacted**]    As req’d   
PT-5    System Test Reports   

9.6

   [**Redacted**]      
PT-6    I&T Command and Telemetry Log Files   

9.8.4

   [**Redacted**]    weekly   
PT-7    Reserved   

Na

   [**Redacted**]      
PT-8    Instrument Integration Readiness Review Data Package   

4.5.3

   [**Redacted**]      
PT-9    Satellite Environmental Testing Readiness Review Data Package   

4.5.3

   [**Redacted**]      
PT-10    Pre-Ship Review Data Package   

4.5.3

   [**Redacted**]      
LAUNCH AND MISSION         
LM-1    Missile Systems Pre-Launch Safety Package (MSPSP)   

12.1

   [**Redacted**]   

L-52 wks TBD

L-26 wks TBD

  
LM-2    Preliminary WV3 FEM   

12.4.a

   [**Redacted**]      
   Preliminary CLA-to-WV3 Design Loads Comparison   

12.4.b

   [**Redacted**]      

 

 

ITAR Controlled Document - DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

Attch 1 - 3


LOGO

   WV3 Satellite Statement of Work   
   Doc Number 10329656

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

   Final WV3 FEM   

12.4.c

   [**Redacted**]      
   Final CLA-to-WV3 Design Loads Comparison   

12.4.d

   [**Redacted**]      
LM-3    Training Materials and sessions   

13.1.1

   [**Redacted**]    As revised   
LM-4    Command &Telemetry Handbook   

13.2

   [**Redacted**]    As revised   
LM-5    Calibration Tools   

13.3

   [**Redacted**]   

As revised

& L+3 m

  
LM-6    Commissioning Plan   

13.5

   [**Redacted**]    As revised   
LM-7    Commissioning Report   

13.7.2.1

   [**Redacted**]      
LM-8    Satellite Simulator   

13.8.1

   [**Redacted**]    See Para 3.1.b   
LM-9    Satellite Simulator Documentation   

13.8.2

   [**Redacted**]    With LM-8   
LM-10    Satellite Simulator Source Code   

13.8.3

   [**Redacted**]    With LM-8   
LM-11    High Fidelity Maneuver Planner   

13.9.1

   [**Redacted**]      
LM-12    Peak Estimator Algorithm   

13.9.2

   [**Redacted**]      
LM-13    Integrative Maneuver Model   

3

   [**Redacted**]      
LM-14    Satellite Launch Readiness Review Data Package   

4.5.3

   [**Redacted**]      
LM-15    Telemetry Packet Creation and Mapping Tools   

13.12

   [**Redacted**]    See 13.12   
LM-16    Telemetry Monitor and Response   

13.13

   [**Redacted**]    See 13.13   

All items are provided for DigitalGlobe information only. Approvals are not required except for ICDs, changes to ICDs, and as otherwise noted.

ATP +1m is 1 month after Authorization to Proceed.

 

 

ITAR Controlled Document - DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

Attch 1 - 4


LOGO

   WV3 Satellite Statement of Work   
   Doc Number 10329656
  

 

 

ATTACHMENT 2 CUSTOMER FURNISHED EQUIPMENT LIST

 

Item

  

Title

   SOW
Ref
  

Date

  

Comment

FLIGHT HARDWARE
CFHW-1    [**Redacted**]    10.2.1    [**Redacted**]   
CFHW-2    [**Redacted**]    10.2.2    [**Redacted**]    Flight and corresponding ground keys.
CFHW-3    [**Redacted**]    10.2.3    [**Redacted**]   
CFHW-4    [**Redacted**]    10.2.4    [**Redacted**]   
CFHW-5    [**Redacted**]    10.2.5    [**Redacted**]   
CFHW-6    [**Redacted**]    10.2.6    [**Redacted**]   
[**Redacted**]
CSIM-1    [**Redacted**]    10.3    [**Redacted**]    Remains the property of DG
[**Redacted**]
CLSE-1    [**Redacted**]    10.4.1    [**Redacted**]   
CLSE-2    [**Redacted**]    10.4.1    [**Redacted**]   
CLSE-3    [**Redacted**]    10.4.2    [**Redacted**]   
[**Redacted**]
CGSE-1    [**Redacted**]    10.5.1.a    [**Redacted**]    Remains the property of DG
CGSE-2    [**Redacted**]    10.5.1.b    [**Redacted**]    Remains the property of DG
CGSE-3    [**Redacted**]    10.5.1.c    [**Redacted**]    Remains the property of DG
CGSE-4    [**Redacted**]    10.5.1.d    [**Redacted**]    Remains the property of DG
CGSE-5    [**Redacted**]    10.5.2.    [**Redacted**]    Remains the property of DG
CGSE-6    [**Redacted**]    10.5.2.0    [**Redacted**]    Remains the property of DG
CGSE-7    [**Redacted**]    10.5.2.0    [**Redacted**]    Remains the property of DG
CGSE-8    [**Redacted**]    10.5.3.a    [**Redacted**]    Remains the property of DG
CGSE-9    [**Redacted**]    10.5.3.b    [**Redacted**]    Remains the property of DG
CGSE-10    [**Redacted**]    10.5.3.c    [**Redacted**]    Remains the property of DG
CGSE-11    [**Redacted**]    10.5.4    [**Redacted**]    Remains the property of DG

 

 

ITAR Controlled Document - DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

Attch 1 - 5


LOGO

   WV3 Satellite Statement of Work   
   Doc Number 10329656
  

 

Item

  

Title

   SOW
Ref
  

Date

  

Comment

CGSE-12    [**Redacted**]    10.5.5    [**Redacted**]    Remains the property of DG
CGSE-13    [**Redacted**]    10.5.6    [**Redacted**]    Remains the property of DG
CGSE-14    [**Redacted**]    10.5.7    [**Redacted**]    Remains the property of DG
CGSE-15    [**Redacted**]    10.5.8    [**Redacted**]    Remains the property of DG
LAUNCH VEHICLE DATA ITEM
CLD-1    WV3 Preliminary CLA    10.6    [**Redacted**]   
CLD-2    WV3 Final CLA    10.6    [**Redacted**]   
INSTRUMENT DATA ITEM
CID-1    WV3 Instrument Structural Data    10.7.1    [**Redacted**]   
CID-2    WV3 Instrument Thermal Data    10.7.2    [**Redacted**]   

DigitalGlobe will provide this equipment in accordance with the requirements of the Agreement.

 

 

ITAR Controlled Document - DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

Attch 1 - 6


Attachment 2

Specifications for the WorldView 3 Satellite, Rev 5.0

Dated 2 May 2011


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

 

LOGO

  Exhibit 2 to Contract 60150

 

 

WorldView-3 Satellite

Specification

 

 

 

  Document #    10329655
  Revision #    5.0
  Release Date    2 May 2011
  Prepared by    George Hunyadi
  Approved by    Keith Constantinides

This Document Is ITAR Controlled

This document contains Technical Data as defined and controlled under the International Traffic In Arms Regulations (ITAR). Transfer of this data by any means to a foreign person, whether in the United States or abroad, without an export license or other approval from the U.S. Department of State is prohibited.

RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION

This document contains information proprietary and confidential to DigitalGlobe , to its subsidiaries, or to a third party to whom DigitalGlobe may have a legal obligation to protect such information from unauthorized disclosure, use or duplication. Any disclosure, use or duplication of this document or of any of the information contained herein for other than the specific purpose for which it was disclosed is expressly prohibited, except as DigitalGlobe may otherwise agree to in writing. This document may only be used for the purpose for which it is provided. All copies of this document are the sole property of DigitalGlobe and will be returned promptly upon request.


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

Change Record

 

Revision

   Date   

Sections

  

Description of Change

1.0    20 Aug 2010    All    Initial Release
[**Redacted**]         
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

  i


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

Table of Contents

 

1.   

 

SCOPE

     6   
     1.1      

 

Purpose

     6   
     1.2      

 

System Overview

     6   
     1.3      

 

Document Overview

     6   
2.   

 

APPLICABLE DOCUMENTS

     7   
     2.1      

 

Government Documents

     7   
        2.1.1      

 

[**Redacted**]

     7   
        2.1.2      

 

[**Redacted**]

     7   
     2.2      

 

Non-Government Documents

     7   
        2.2.1      

 

[**Redacted**]

     7   
        2.2.2      

 

[**Redacted**]

     7   
        2.2.3      

 

[**Redacted**]

     7   
     2.3      

 

Reference Documents

     7   
3.   

 

REQUIREMENTS

     7   
     3.1      

 

Satellite Definition

     8   
        3.1.1      

 

Satellite Diagrams

     8   
           3.1.1.1      

 

Component Tree

     8   
           3.1.1.2      

 

Coordinate System

     8   
        3.1.2      

 

Satellite Interfaces

     8   
           3.1.2.1      

 

Non-interference with Outside Systems

     8   
              3.1.2.1.1      

[**Redacted**

     8   
              3.1.2.1.2      

[**Redacted**]

     8   
              3.1.2.1.3      

[**Redacted**]

     8   
           3.1.2.2      

 

Satellite-Global Positioning System Interfaces

     8   
              3.1.2.2.1      

Compatibility

     8   
           3.1.2.3      

 

Satellite-Ground Interfaces

     9   
              3.1.2.3.1      

Compatibility

     9   
              3.1.2.3.2      

Remote Ground Terminal Locations

     9   
              3.1.2.3.3      

Command Uplink

     9   
              3.1.2.3.4      

Narrowband Telemetry Downlink

     9   
              3.1.2.3.5      

Wideband Data Downlink

     9   
           3.1.2.4      

 

Satellite-Launch Vehicle Interfaces

     10   
              3.1.2.4.1      

Compatibility

     10   
              3.1.2.4.2      

[**Redacted**]

     10   
              3.1.2.4.3      

Umbilical

     10   
        3.1.3      

 

Customer Furnished Equipment

     10   
           3.1.3.1      

 

Instrument

     10   
              3.1.3.1.1      

Physical, Structural and Mechanical Requirements

     10   
              3.1.3.1.2      

Thermal Interfaces

     11   
              3.1.3.1.3      

Power Interfaces

     11   
              3.1.3.1.4      

Command and Telemetry Interfaces

     11   
              3.1.3.1.5      

Image Data Interfaces

     12   
              3.1.3.1.6      

EOA Thermal Control Interfaces

     12   
              3.1.3.1.7      

[**Redacted**]

     13   
           3.1.3.2      

 

MGB

     13   

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

  ii


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

     3.2      

Satellite Characteristics

     13   
      3.2.1   

 

Performance

     13   
           3.2.1.1     

General Mission Requirements

     13   
           3.2.1.1.1   

Mission Life

     13   
           3.2.1.1.2   

Orbits

     13   
           3.2.1.2     

Satellite Operating Modes

     13   
           3.2.1.2.1   

Normal Operating Modes

     13   
           3.2.1.2.2   

Special / Contingency Modes

     14   
           3.2.1.2.3   

Intermediate and Transitional Modes

     15   
           3.2.1.3     

Pre-Launch Operations

     15   
           3.2.1.3.1   

Ground Storage

     15   
           3.2.1.3.2   

Launch Delay

     15   
           3.2.1.4     

Early Orbit Operations

     16   
           3.2.1.4.1   

Autonomous Operations After Separation

     16   
           3.2.1.4.2   

First [**Redacted**]

     16   
           3.2.1.4.3   

Commissioning

     16   
           3.2.1.5     

Mission Operations

     16   
           3.2.1.5.1   

Viewing Angles

     16   
           3.2.1.5.2   

Imaging and Downlink Operations

     16   
           3.2.1.5.3   

Stereo Imaging

     17   
           3.2.1.5.4   

Off-Nadir Imaging

     17   
           3.2.1.5.5   

[**Redacted**]

     17   
           3.2.1.5.6   

[**Redacted**]

     17   
           3.2.1.6     

Instrument Requirements

     17   
           3.2.1.6.1   

Integrated Bus/Instrument Performance Effects

     17   
           3.2.1.6.2   

[**Redacted**]

     17   
           3.2.1.6.3   

[**Redacted**]

     18   
           3.2.1.6.4   

Instrument Cleanliness

     19   
           3.2.1.7     

Bus Subsystem Requirements

     19   
           3.2.1.7.1   

[**Redacted**]

     19   
           3.2.1.7.2   

ADCS

     20   
           3.2.1.7.3   

Propulsion

     22   
           3.2.1.7.4   

Flight Software

     23   
           3.2.1.7.5   

C&DH

     24   
           3.2.1.7.6   

Narrowband Communications

     28   
           3.2.1.7.7   

[**Redacted**]

     30   
           3.2.1.7.8   

EPDS

     33   
           3.2.1.7.9   

Structures and Mechanisms

     34   
           3.2.1.7.10   

Thermal Control

     35   
           3.2.1.7.11   

Direct Tasking

     36   
      3.2.2   

 

Physical Characteristics

     40   
           3.2.2.1     

Size Constraints

     40   
           3.2.2.2     

Mass Constraints

     40   
           3.2.2.3     

Shipping Constraints

     40   
      3.2.3   

 

Reliability

     40   
           3.2.3.1     

End of Life Ps

     40   

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

  iii


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

           3.2.3.2      

 

[**Redacted**]

     40   
           3.2.3.3      

 

[**Redacted**]

     40   
           3.2.3.4      

 

Cycle-Limited Items

     40   
              3.2.3.4.1      

[**Redacted**]

     40   
              3.2.3.4.2      

[**Redacted**]

     40   
        3.2.4      

 

Availability and Maintainability

     41   
           3.2.4.1      

 

Fault Recovery Timeline

     41   
           3.2.4.2      

 

Environmental Conditions

     41   
              3.2.4.2.1      

Launch Induced Environments

     41   
              3.2.4.2.2      

On-Orbit Environments

     41   
              3.2.4.2.3      

Pre-Launch Environments

     41   
   3.3   

 

Satellite Design and Construction

     41   
        3.3.1      

 

General

     41   
        3.3.2      

 

SEUs

     41   
        3.3.3      

 

Immunity to Latch-Up

     41   
        3.3.4      

 

Cleanliness and Contamination Control

     41   
           3.3.4.1      

 

[**Redacted**]

     41   
           3.3.4.2      

 

[**Redacted**]

     42   
           3.3.4.3      

 

[**Redacted**]

     42   
           3.3.4.4      

 

[**Redacted**]

     42   
        3.3.5      

 

Safety

     42   
        3.3.6      

 

[**Redacted**]

     42   
4.   

VERIFICATION

     42   
5.   

QUALITY ASSURANCE

     42   

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

  iv


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

List of Tables

[**Redacted**]

List of Figures

[**Redacted**]

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

  v


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

2. SCOPE

 

2.1 Purpose

This document describes the requirements for design and implementation of the DigitalGlobe WorldView-3 Satellite, being constructed to support DigitalGlobe commercial imaging operations.

 

2.2 System Overview

Ball Aerospace & Technology Corporation (BATC) is providing the integrated WorldView-3 imaging satellite to DigitalGlobe, Inc. As the Space Segment Integrator (SSI), BATC is manufacturing a Spacecraft Bus that can accommodate the panchromatic + multi-spectral WorldView-3 Instrument. This will be the same Bus design as used for predecessor WorldView Satellites. The Instrument is being supplied by ITT Industries Space Systems Division (ITT) to DigitalGlobe, with miscellaneous support units / functions provided by BATC. All ITT equipment will be provided as Customer Furnished Equipment (CFE) to BATC for Satellite integration. As the SSI, BATC will then perform Satellite level testing, prepare the Satellite for launch, and support on-orbit checkout of the Satellite.

The Satellite will be in a sun-synchronous orbit at an altitude between 450 and 830 km with a descending equator crossing time between 10:00 AM and 2:00 PM. [**Redacted**] Image data is recorded by the Spacecraft Bus and is normally downlinked to DigitalGlobe ground stations. However, direct downlink to user sites may also be performed in certain circumstances. Direct downlink is via the normal wideband downlink.

A key feature of the WordView-3 Satellite is Direct Tasking, where imaging and downlink parameters are directly uplinked from a customer’s ground station to the satellite, and image data is directly downlinked to a customer’s ground station, on the same and/or successive passes. Direct Tasking supports an expanded customer base and fulfills these customers’ desires to compress the overall planning-tasking-collection-downlink timeline and to not expose their task list to outside parties (including DigitalGlobe) prior to image collection. Full command authority is maintained by DigitalGlobe, with key commands needed to initiate the image and downlink operations uploaded from DigitalGlobe ground stations.

 

2.3 Document Overview

This document specifies functional, performance and interface requirements for the integrated Satellite and the Spacecraft Bus, including external Satellite interfaces, Instrument-Bus interfaces and Instrument integration, Bus and Satellite test, launch, and operational requirements. Separate Interface Control Documents (ICDs) detail the specifics of the Instrument-Bus interfaces and Integration and Test processes. Satisfaction of the Satellite-level requirements contained in this specification assume the Instrument provided as CFE meets its requirements, which are documented separately. As the SSI, BATC will refer to the separate Instrument Specifications as necessary to maintain the Spacecraft Bus to Instrument ICDs and develop an integration and test plan sufficient to ensure the integrated Satellite meets its system-level functional and performance requirements.

This specification may contain requirements that have not been fully defined. These open requirements are indicated by a TBR, and/or TBD:

TBR – To Be Resolved: Indicates parameters that exist, but may change after discussions with Contractor and others (e.g.: DigitalGlobe).

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

  6


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

TBD – To Be Determined: Indicates parameters that have not yet been determined.

 

3. APPLICABLE DOCUMENTS

This document is the Satellite Specification. This specification defines the technical requirements called out in the Contract and a Statement of Work (SOW). The Contract and SOW define schedule requirements, deliverable items and programmatics. However, in the event of a conflict between a specific requirement herein and documents, then the Contract, the Statement of Work, this document, and Applicable documents shall govern in this order. If the revision is not specifically noted, the latest revision of each document applies.

At contract signing, the Environmental Design and Test Specification and Interface Control Documents from predecessor DigitalGlobe WorldView satellite programs listed below shall be considered the baseline release for WV-3. It is anticipated that the WV-3 versions of these documents will require few modifications from the predecessor baselines, with changes focused in a few key areas as driven by WV-3 unique requirements (for example enhanced Instrument thermal control and updated power values). The first release of the WV-3 version of each document shall supersede the predecessor version, which shall no longer be considered an Applicable Document.

Although the Satellite Integrating Contractor physically maintains many of these ICDs, their development is inherently a cooperative process. Accordingly, the latest released ICD revision shall always apply, where release is predicated on mutual agreement between all involved parties; for example the Instrument to Spacecraft ICD requires consensus between the Satellite Integrating Contractor, the Instrument Contractor, and DigitalGlobe.

 

3.1 Government Documents

 

3.1.1 [**Redacted**]

 

3.1.2 [**Redacted**}

 

3.2 Non-Government Documents

 

3.2.1 [**Redacted**]

 

3.2.2 [**Redacted**]

 

3.2.3 [**Redacted**]

 

3.3 Reference Documents

[**Redacted**]

 

4. REQUIREMENTS

Remarks contained as Rationale/Info shall NOT be considered a formal part of this specification and are provided for reference only.

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

  7


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

[**Redacted**]

 

4.1 Satellite Definition

This Section defines fundamental terminology and identifies the basic Satellite functions along with the provider of each function. It also provides external interface requirements and internal interface requirements for the equipment to be provided [**Redacted**] to the SSI.

 

4.1.1 Satellite Diagrams

4.1.1.1    Component Tree

[**Redacted**] defines the major elements, subsystems, assemblies and units/functions of the Satellite and shows how they are allocated between DigitalGlobe’s contractors. The figure also indicates items that are delivered to the SSI [**Redacted 1 Page**].

4.1.1.2    Coordinate System

The base coordinate system used for all major Satellite element and segment mechanical interfaces shall be as shown in [**Redacted**] , for example, Instrument to Spacecraft Bus and Satellite to Launch Vehicle.

Other coordinate systems may be used as appropriate within elements and/or subsystems; [**Redacted**] . The relationships between the base coordinate system and other coordinate systems shall be explicitly shown in the appropriate documents (drawings, interface control documents, etc.).

[**Redacted**]

 

4.1.2 Satellite Interfaces

4.1.2.1    Non-interference with Outside Systems

4.1.2.1.1    [**Redacted**]

The Satellite shall not interfere with [**Redacted**].

4.1.2.1.2    [**Redacted**]

During normal operations, RF emissions from the Satellite shall not exceed the limits specified in the [**Redacted**] .

4.1.2.1.3    [**Redacted**]

All RF emissions shall use the frequency allocation of [**Redacted**] , with out-of-band emissions compliant with [**Redacted**].

4.1.2.2    Satellite-Global Positioning System Interfaces

4.1.2.2.1     Compatibility

The Spacecraft Bus shall be compatible with standard GPS interfaces as defined in [**Redacted**] .

 

 

 

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4.1.2.3    Satellite-Ground Interfaces

The following paragraphs define high-level requirements for Satellite-Ground compatibility; detailed interface requirements shall be defined in the Narrowband and Wideband Satellite-Ground ICD.

[**Redacted**]

4.1.2.3.1     Compatibility

The Satellite Narrowband and Wideband Communications Subsystems shall be compatible with [**Redacted**] .

4.1.2.3.2     Remote Ground Terminal Locations

Remote Ground Terminals (RGTs) will be located as follows:

[**Redacted**]

4.1.2.3.3     Command Uplink

4.1.2.3.3.1     Effective Isotropic Radiated Power

The minimum Effective Isotropic Radiated Power (EIRP) of the command uplink antenna will be [**Redacted** ].

4.1.2.3.3.2     Axial Ratio

The command uplink antenna will transmit using [**Redacted**] .

4.1.2.3.4     Narrowband Telemetry Downlink

4.1.2.3.4.1     Figure of Merit (G/T)

The minimum G/T of the Narrowband receive antenna will be as follows across the frequency range of [**Redacted**] under all conditions, for the RGT locations defined in Section 3.1.2.3.2 Remote Ground Terminal Locations. These values include the effects of antenna pointing error and atmospheric conditions.

[**Redacted**]

4.1.2.3.4.2     Axial Ratio

The Narrowband receive antenna will receive using [**Redacted**] .

4.1.2.3.4.3 Implementation Loss

The demodulator implementation loss for the Narrowband telemetry receiver will be [**Redacted**] .

4.1.2.3.5     Wideband Data Downlink

4.1.2.3.5.1     Figure of Merit (G/T)

The minimum G/T of the Wideband receive antenna will be as follows across the frequency range of [**Redacted**] under all conditions, for the RGT locations defined in Section 3.1.2.3.2 Remote Ground Terminal Locations. These values include the effects of antenna pointing error and atmospheric conditions.

[**Redacted**]

4.1.2.3.5.2     Axial Ratio

The Wideband receive antenna will receive using [**Redacted**] .

 

 

 

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4.1.2.3.5.3     Implementation Loss

The demodulator implementation loss for the wideband telemetry receiver will be [**Redacted**] .

4.1.2.4    Satellite-Launch Vehicle Interfaces

The following paragraphs define high-level requirements for Satellite – Launch Vehicle compatibility; detailed interface requirements shall be defined in the Mission Specification.

4.1.2.4.1     Compatibility

The Satellite design shall be compatible with the [**Redacted**]

4.1.2.4.2    [**Redacted**]

The Satellite shall accommodate [**Redacted**].

4.1.2.4.3     Umbilical

The Satellite shall accommodate an umbilical to support all required functions for launch mode, including at a minimum the following critical electrical functions:

[**Redacted**]

 

4.1.3 Customer Furnished Equipment

4.1.3.1    Instrument

The Instrument will be provided to the SSI [**Redacted**] . The SSI shall provide interfaces as specified herein, with detailed interface requirements provided in accordance with the [**Redacted**] .

4.1.3.1.1     Physical, Structural and Mechanical Requirements

4.1.3.1.1.1     Configuration

The Spacecraft Bus shall accommodate the following major Instrument assemblies and/or units:

[**Redacted**]

4.1.3.1.1.2     Size

The Spacecraft Bus shall be capable of supporting the Instrument assemblies/units as specified in the Spacecraft Bus to Instrument ICDs.

4.1.3.1.1.3     Mass Properties

[**Redacted**]

4.1.3.1.1.4     EOA-Mounted Spacecraft Bus Equipment

The SSI shall provide the following equipment to be mounted on the EOA:

[**Redacted**]

4.1.3.1.1.5     EOA Fields of View

The Spacecraft Bus shall provide the Instrument with [**Redacted**] .

4.1.3.1.1.6     EOA Purge Fitting

The Satellite shall be configured to provide a purge fitting [**Redacted**] .

 

 

 

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4.1.3.1.1.7     Assembly, Integration and Test

 

a) To the maximum extent possible, the Satellite configuration shall permit independent integration of all Instrument assemblies/units and access to internal Instrument test ports and harness connections.

 

b) The Satellite configuration shall allow clear access to Instrument equipment essential to integration and test activities, for example: test ports, purge lines, aperture cover, interface connectors, etc.

4.1.3.1.1.8     EOA Vibration Environment

The SI shall ensure that the [**Redacted**]

4.1.3.1.1.9    [**Redacted**]

The Spacecraft Bus shall provide radiation shielding for the [**Redacted**] .

4.1.3.1.2     Thermal Interfaces

The Spacecraft Bus shall perform the following thermal functions, with interfaces to the Instrument as specified in the Spacecraft Bus to Instrument ICDs:

[**Redacted**]

4.1.3.1.3     Power Interfaces

The Spacecraft Bus shall provide electrical power to the Instrument as specified below, with the breakdown of individual unit powers and other characteristics as specified in the Spacecraft Bus to Instrument ICDs.

4.1.3.1.3.1     Instrument Power Feeds

The Spacecraft Bus shall provide power to all Instrument units as follows:

[**Redacted**]

4.1.3.1.3.2     Voltage

The Spacecraft Bus shall present power at the Instrument interfaces as follows:

[**Redacted**]

4.1.3.1.3.3 [**Redacted**]

[**Redacted**]

4.1.3.1.3.4     Average Operating Power

During normal operations, the Spacecraft Bus shall be able to perform [**Redacted**]

4.1.3.1.3.5     Survival Power

When in Emergency Mode, the Spacecraft Bus shall provide power as specified in [**Redacted**] via the Essential Bus, as specified in Section 3.1.3.1.3.1 Instrument Power Feeds.

4.1.3.1.3.6     Maximum Power

 

a) The Spacecraft Bus shall be capable of supporting the sustained maximum Instrument power specified in [**Redacted**] .

 

b) The Spacecraft Bus shall [**Redacted**]

4.1.3.1.4     Command and Telemetry Interfaces

The Spacecraft Bus shall provide the following command and telemetry interfaces to the Instrument, all of which shall be cross-strapped between the primary and redundant Spacecraft Bus electronics and primary and redundant Instrument electronics:

[**Redacted**]

 

 

 

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4.1.3.1.4.1     Instrument Commanding

Using the specified data interfaces, the Spacecraft Bus shall forward commands to the Instrument, [**Redacted**] as documented in the Spacecraft Bus to Instrument ICDs.

4.1.3.1.4.2     Image Start and Stop Commands

The commands for image [**Redacted**] shall be issued from the Spacecraft Bus [**Redacted**] .

4.1.3.1.4.3     Image Duration

 

a) The minimum Image duration possible shall be no more than [**Redacted**] .

 

b) There shall be [**Redacted**] .

 

c) Image durations shall be commandable in [**Redacted**] .

[**Redacted**]

4.1.3.1.4.4     Instrument Telemetry

Using the specified data interfaces, the Spacecraft Bus shall receive telemetry from the Instrument as documented in the Spacecraft Bus to Instrument ICDs. The following rules shall be applied to Instrument telemetry:

[**Redacted**]

4.1.3.1.4.5    [**Redacted**]

The Spacecraft Bus shall provide a [**Redacted**] as follows:

[**Redacted**]

4.1.3.1.5     Image Data Interfaces

The Spacecraft Bus shall provide image data interfaces [**Redacted**]

4.1.3.1.5.1     General Interface Definition

The Spacecraft Bus to Instrument data interface shall be as follows:

[**Redacted**]

4.1.3.1.5.2     Maximizing Storage and Downlink Efficiency

The Spacecraft Bus to Instrument data interface shall be capable of supporting the following Instrument configurations and shall ensure [**Redacted**]

4.1.3.1.6     EOA Thermal Control Interfaces

[**Redacted**]

4.1.3.1.6.1    [**Redacted**]

[**Redacted**]

4.1.3.1.6.2    [**Redacted**]

[**Redacted**]

4.1.3.1.6.3    [**Redacted**]

[**Redacted**]

 

 

 

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4.1.3.1.7    [**Redacted**]

The [**Redacted**] system will be provided to the SSI [**Redacted**] . The Spacecraft Bus shall interface to the [**Redacted**] system as specified in [**Redacted**] .

4.1.3.2    MGB

The MGB will be provided to the SSI [**Redacted**] . The SSI shall meet the MGB requirements specified in the MGB Requirements Documents and Interface Control Documents.

 

4.2 Satellite Characteristics

This Section defines the characteristics of the Satellite required to support the mission with respect to performance, physical characteristics, reliability, availability, and environmental conditions. The SSI shall derive and otherwise define lower level requirements necessary to implement the requirements of this specification, including those that are passed to the Instrument Contractor via the Spacecraft Bus to Instrument ICD, the Environmental Design and Test Specification, and other relevant documents.

 

4.2.1 Performance

4.2.1.1    General Mission Requirements

4.2.1.1.1     Mission Life

The Satellite shall meet all on-orbit performance requirements for a Mission Life of [**Redacted**] . The end of this period is defined as End of Life (EOL).

[**Redacted**]

4.2.1.1.2     Orbits

4.2.1.1.2.1     General Orbit Compatibility

The Satellite shall be capable of operating at any equatorial altitude between [ **Redacted**]

4.2.1.1.2.2     Reserved

4.2.1.1.2.3     Mission Orbit

The Mission Orbit shall be defined as:

[**Redacted**]

4.2.1.1.2.4     Reserved

4.2.1.1.2.5     Insertion Orbit and Dispersions

The Satellite shall be compatible with being inserted directly into any of the orbits defined under General Orbit Compatibility, [**Redacted**]

4.2.1.2    Satellite Operating Modes

4.2.1.2.1     Normal Operating Modes

The Satellite shall, at a minimum, provide the operating modes defined in Table 4-1 Normal Operating Modes, with the following additional requirements:

[**Redacted**]

 

 

 

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Table 4-1 Normal Operating Modes

 

Mode

  

Basic Satellite State

  

Satellite Pointing

Cruise Mode

 

   [**Redacted**]    [**Redacted**]

[**Redacted**]

 

      [**Redacted**]

[**Redacted**]

 

   [**Redacted**]    [**Redacted**]
[**Redacted**]       [**Redacted**]

4.2.1.2.2     Special / Contingency Modes

The Satellite shall, at a minimum, provide the modes defined in [**Redacted**] , with the following additional requirements:

[**Redacted**]

Table 4-2 Special / Contingency Modes

 

Mode

  

Basic Satellite State

  

Satellite Pointing

[**Redacted**]

 

   [**Redacted**]    [**Redacted**]

[**Redacted**]

 

   [**Redacted**]    [**Redacted**]
[**Redacted**]    [**Redacted**]   

 

 

 

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Table 4-3 Simultaneous Operations

 

Simultaneous
Operations

  

Normal Operating Modes

   Special / Contingency Modes
  

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]

Recording Image Data

         [**Redacted**]    [**Redacted**]            

Recording Ancillary Data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]         

Transmitting recorded Image and Ancillary Data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]         

Recording Satellite state of health data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]   

Transmitting stored state-of-health data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]   

Transmitting real-time state-of-health data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]   

Preserving stored Image and Ancillary Data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]   

Preserving stored state-of-health data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]    [**Redacted**]

Receiving and executing real-time commands

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]

Receiving and storing stored commands

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]   

Executing stored commands

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]   

[**Redacted**]

4.2.1.2.3     Intermediate and Transitional Modes

Additional intermediate and transitional modes may be defined for the Satellite and Spacecraft Bus. [**Redacted**]

4.2.1.3    Pre-Launch Operations

4.2.1.3.1     Ground Storage

The Satellite shall be capable of being stored under proper conditions for up to [**Redacted**] without the need for refurbishment.

4.2.1.3.2     Launch Delay

 

a) The Satellite shall be capable of remaining loaded with propellant for a minimum of [**Redacted**] prior to launch, while maintaining safety and status monitoring.

 

b) The Satellite shall be capable of launch for up to [**Redacted**] following the integration of the Satellite to the Launch Vehicle without the need for demate, while maintaining safety and status monitoring.

 

c) The Satellite shall be designed to permit [**Redacted**] .

 

 

 

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4.2.1.4    Early Orbit Operations

4.2.1.4.1     Autonomous Operations After Separation

Following the separation event, the Satellite shall autonomously:

[**Redacted**]

4.2.1.4.2     First [**Redacted**]

Following the Autonomous Operations after Separation, the Satellite shall pose no constraints on operation such that:

[**Redacted**]

4.2.1.4.3     Commissioning

The Satellite shall pose no constraints on operation such that total Satellite on-orbit performance can be fully verified as specified in the Statement of Work.

4.2.1.5    Mission Operations

4.2.1.5.1     Viewing Angles

Viewing angles referred to in the [**Redacted**] and elsewhere in this specification shall be as defined below.

[**Redacted**]

4.2.1.5.1.1     Nominal Field of Regard

The Nominal Field of Regard shall be defined as a [**Redacted**]

4.2.1.5.1.2     Maximum Field of Regard

The Maximum Field of Regard shall be defined as a [**Redacted**]

4.2.1.5.1.3    [**Redacted**]

[**Redacted**]

4.2.1.5.1.4    [**Redacted**]

[**Redacted**]

4.2.1.5.1.5     Instrument Operating Modes

The Satellite shall allow operation of the Instrument in the modes specified in [**Redacted**]

4.2.1.5.2     Imaging and Downlink Operations

The Satellite shall be capable of performing the imaging and downlink operations specified below assuming [**Redacted**]

4.2.1.5.2.1    [**Redacted**]

[**Redacted 1 Page**]

4.2.1.5.2.2     Wideband and Narrowband Downlinks

It shall be possible to perform both Wideband and Narrowband downlinks as follows:

[**Redacted**]

4.2.1.5.2.3      Instrument Mass Properties for [**Redacted**]

For purposes of verifying the Satellite’s ability to perform the DIS, [ **Redacted**]

 

 

 

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4.2.1.5.2.4    [**Redacted**]

[**Redacted**]

4.2.1.5.3     Stereo Imaging

 

a) The Satellite shall be capable of collecting the stereo imagery [**Redacted**]

 

b) The Satellite shall be capable of collecting stereo imagery [**Redacted**]

4.2.1.5.4     Off-Nadir Imaging

The Satellite shall be capable of supporting off-nadir image collections as follows:

[**Redacted**]

4.2.1.5.5     Special Imaging

4.2.1.5.5.1     Minimum Capabilities

[**Redacted**]

4.2.1.5.5.2    [**Redacted**]

[**Redacted**]

4.2.1.5.6    [**Redacted**]

[**Redacted**]

4.2.1.6    Instrument Requirements

4.2.1.6.1     Integrated Bus/Instrument Performance Effects

The SSI shall perform appropriate integrated Satellite-level analyses and design work in order to ensure the Satellite meets the following performance requirements. LOS motion shall be calculated using an Instrument Finite Element Model (FEM) provided by the Instrument Contractor as defined under Applicable Documents, which shall be assumed to meet the following requirements:

[**Redacted**]

4.2.1.6.1.1    [**Redacted**]

[**Redacted**]

4.2.1.6.1.2    [**Redacted**]

[**Redacted**]

4.2.1.6.2    [**Redacted**]

[**Redated**]

4.2.1.6.2.1    [**Redated**]

[**Redacted**]

 

 

 

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4.2.1.6.2.2    [**Redacted**]

[**Redacted**]

4.2.1.6.3    [**Redacted**]

[**Redacted**]

4.2.1.6.3.1    [**Redacted**]

[**Redacted**]

4.2.1.6.3.2    [**Redacted**]

[**Redacted**]

4.2.1.6.3.3    [**Redacted**]

[**Redacted**]

4.2.1.6.3.4    [**Redacted**]

[**Redacted**]

4.2.1.6.3.4.1    [**Redacted**]

[**Redacted**]

4.2.1.6.3.4.2    [**Redacted**]

[**Redacted**]

4.2.1.6.3.4.3    [**Redacted**]

[**Redacted**]

4.2.1.6.3.5    [**Redacted**]

[**Redacted**]

4.2.1.6.3.5.1    [**Redacted**]

[**Redacted**]

4.2.1.6.3.5.2    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.6.3.6    [**Redacted**]

[**Redacted**]

4.2.1.6.4     Instrument Cleanliness

[**Redacted**]

4.2.1.6.4.1    [**Redacted**]

[**Redacted**]

4.2.1.6.4.2    [**Redacted**]

[**Redacted**]

4.2.1.7 Bus Subsystem Requirements

In addition to supporting all subsystem-level requirements derived from the Satellite-level requirements specified in the above sections, Spacecraft Bus subsystems shall meet the specific requirements contained within this section.

4.2.1.7.1    [** Redacted **]

4.2.1.7.1.1    [**Redacted**]

[**Redacted**]

4.2.1.7.1.2    [**Redacted**]

[**Redacted**]

4.2.1.7.1.3    [**Redacted**]

[**Redacted**]

4.2.1.7.1.3.1    [**Redacted**]

[**Redacted**]

4.2.1.7.1.3.2    [**Redacted**]

[**Redacted**]

4.2.1.7.1.3.3    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.1.3.4    [**Redacted**]

[**Redacted**]

4.2.1.7.1.3.5    [**Redacted**]

[**Redacted**]

4.2.1.7.1.3.6    [**Redacted**]

[**Redacted**]

4.2.1.7.1.3.7    [**Redacted**]

[**Redacted**]

4.2.1.7.1.3.8    [**Redacted**]

[**Redacted**]

4.2.1.7.1.4    [**Redacted**]

 

4.2.1.7.1.4.1    [**Redacted**]

[**Redacted**]

4.2.1.7.1.4.2    [**Redacted**]

[**Redacted**]

4.2.1.7.1.4.3    [**Redacted**]

[**Redacted**]

4.2.1.7.1.4.4    [**Redacted**]

[**Redacted**]

4.2.1.7.2     ADCS

4.2.1.7.2.1    [**Redacted**]

[**Redacted**]

4.2.1.7.2.2    [**Redacted**]

4.2.1.7.2.2.1    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.2.2.2    [**Redacted**]

[**Redacted**]

4.2.1.7.2.2.3    [**Redacted**]

[**Redacted**]

4.2.1.7.2.2.4    [**Redacted**]

[**Redacted**]

4.2.1.7.2.2.5    [**Redacted**]

[**Redacted**]

4.2.1.7.2.3    [**Redacted**]

[**Redacted**]

4.2.1.7.2.4    [**Redacted**]

4.2.1.7.2.4.1    [**Redacted**]

[**Redacted**]

4.2.1.7.2.4.2    [**Redacted**]

[**Redacted**]

4.2.1.7.2.5     [ **Redacted** ]

4.2.1.7.2.6     [ **Redacted** ]

[**Redacted**]

4.2.1.7.2.7    [**Redacted**]

[**Redacted**]

4.2.1.7.2.8    [**Redacted**]

[**Redacted**]

4.2.1.7.2.9    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.2.9.1    [**Redacted**]

[**Redacted**]

4.2.1.7.2.9.2    [**Redacted**]

[**Redacted**]

4.2.1.7.2.9.3    [**Redacted**]

[**Redacted**]

4.2.1.7.2.9.4    [**Redacted**]

[**Redacted**]

4.2.1.7.2.9.5    [**Redacted**]

[**Redacted**]

4.2.1.7.2.10    [**Redacted**]

[**Redacted**]

4.2.1.7.2.11     Solar Arrays

In all modes of operation except Launch Mode, the ADCS shall be capable of pointing the Solar Array as follows:

[**Redacted**]

4.2.1.7.2.12     Wideband Antenna

While in Cruise Mode, Earth or Fixed Frame Imaging Mode, or maneuvering to/from Images, the ADCS shall be capable of pointing the Wideband Antenna as follows:

[**Redacted**]

4.2.1.7.3     Propulsion

4.2.1.7.3.1     Minimum Delta-V Capability

The Propulsion subsystem shall provide at least [**Redacted**]

4.2.1.7.3.2     Propellant Budget

The SSI shall develop and maintain a [**Redacted**]

4.2.1.7.3.3     Inefficiencies of Operation

The propellant budget shall, at a minimum, account for the following inefficiencies of operation:

[**Redacted**]

 

 

 

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4.2.1.7.3.4     Thruster Orientation

[**Redacted**]

4.2.1.7.3.5    [**Redacted**]

[**Redacted**]

4.2.1.7.4     Flight Software

4.2.1.7.4.1     [**Redacted**]

The Flight Software shall provide the capability to [**Redacted**] .

4.2.1.7.4.2     Modularity

The design of the Satellite flight software shall be [**Redacted**] .

4.2.1.7.4.2.1     Module Size

The patching or replacing of any single Satellite flight software module shall not require more than [**Redacted**] or the [**Redacted**] shall be uploadable in no more than [**Redacted**] split across multiple contacts [**Redacted**].

4.2.1.7.4.3     Parameterization

The design of the Satellite flight software shall incorporate parameterization to support operational flexibility and command versatility.

[**Redacted**]

4.2.1.7.4.3.1     Parameter Range and Resolution

Parameters shall have enough range and resolution to permit operation of the Satellite to the requirements of this specification without having to patch the Satellite Flight software.

4.2.1.7.4.3.2    [**Redacted**]

[**Redacted**]

4.2.1.7.4.4    [**Redacted**]

[**Redacted**]

4.2.1.7.4.4.1    [**Redacted**]

[**Redacted**]

4.2.1.7.4.4.2    [**Redacted**]

[**Redacted**]

4.2.1.7.4.5    [**Redacted**]

[**Redacted**]

 

 

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4.2.1.7.4.6    [**Redacted**]

[**Redacted**]

4.2.1.7.4.7    [**Redacted**]

[**Redacted**]

4.2.1.7.4.7.1    [**Redacted**]

[**Redacted**]

4.2.1.7.4.8    [**Redacted**]

[**Redacted**]

4.2.1.7.4.9    [**Redacted**]

[**Redacted**]

4.2.1.7.4.10    [**Redacted**]

[**Redacted**]

4.2.1.7.4.11    [**Redacted**]

[**Redacted**]

4.2.1.7.5     C&DH

4.2.1.7.5.1     Commands

4.2.1.7.5.1.1     Command Formats

Commands shall be formatted as specified in the [**Redacted**] .

4.2.1.7.5.1.2     Command Length

Commands shall be [**Redacted**] to assure compatibility with [**Redacted**] with [**Redacted**] and [**Redacted**] .

4.2.1.7.5.1.3    [**Redacted**]

[**Redacted**]

4.2.1.7.5.1.4    [**Redacted**]

[**Redacted**]

4.2.1.7.5.1.5    [**Redacted**]

[**Redacted**]

 

 

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4.2.1.7.5.1.6    [**Redacted**]

[**Redacted**]

4.2.1.7.5.1.7    [**Redacted**]

[**Redacted**]

4.2.1.7.5.1.8    [**Redacted**]

[**Redacted**]

4.2.1.7.5.1.9    [**Redacted**]

[**Redacted**]

4.2.1.7.5.1.10     Unique Satellite Identification

The Satellite identification used for command verification and acceptance shall be unique for each redundancy string and shall be different than IDs used on previous DigitalGlobe satellites.

[**Redacted**]

4.2.1.7.5.2     State-of-Health Telemetry

4.2.1.7.5.2.1     Telemetry Content

The C&DH subsystem shall collect and format housekeeping telemetry for the Spacecraft Bus and Instrument sufficient to provide the following capabilities on the ground:

[**Redacted**]

4.2.1.7.5.2.2     Telemetry Format

The C&DH subsystem shall format and transmit the [**Redacted**] as follows:

[**Redacted**]

4.2.1.7.5.2.3    [**Redacted**]

[**Redacted**]

4.2.1.7.5.2.4    [**Redacted**]

[**Redacted**]

4.2.1.7.5.2.5    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.5.2.6     Unique Satellite Identification

All telemetry data shall periodically include a Satellite identification that is different than IDs used on previous DigitalGlobe satellites.

[**Redacted**]

4.2.1.7.5.2.7     Storage Capacity

The C&DH subsystem shall be capable of storing at least 36 hours of telemetry at an average rate of [**Redacted**] .

[**Redacted**]

4.2.1.7.5.2.8    [**Redacted**]

[**Redacted**]

4.2.1.7.5.2.9    [**Redacted**]

[**Redacted**]

4.2.1.7.5.3    [**Redacted**]

[**Redacted**]

4.2.1.7.5.4     Ancillary Data

During normal operations, the C&DH subsystem shall collect Ancillary Data from Bus and Instrument equipment and forward it [**Redacted**]

4.2.1.7.5.4.1     Standard Content

The standard content of the two Ancillary Data streams shall be as defined in [**Redacted**] .

[**Redacted**]

 

 

 

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Table 4-4 Standard Ancillary Data Content

 

Data Type

  

Description

  

Frequency

  

Minimum Rate

Continuous Ancillary Data Stream

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]
[**Redacted**]
Image Ancillary Data Stream

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

4.2.1.7.5.4.2     Format

The C&DH subsystem shall format the [**Redacted**]

4.2.1.7.5.4.3     Redefinable Content

It shall be possible to independently re-define the content of [**Redacted**] , subject to data bandwidth constraints.

[**Redacted**]

4.2.1.7.5.4.4    [**Redacted**]

[**Redacted**]

4.2.1.7.5.4.5     Data Transfer

The C&DH subsystem shall transfer the Ancillary Data to the MDR as follows:

[**Redacted**]

4.2.1.7.5.4.6    [**Redacted**]

[**Redacted**]

4.2.1.7.5.4.7     [ **Redacted** ]

[**Redacted**]

 

 

 

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4.2.1.7.5.5     Command & Telemetry Protocol

The satellite shall meet the requirements for the satellite command and telemetry protocol as specified in the [**Redacted**]

4.2.1.7.6     Narrowband Communications

4.2.1.7.6.1     Command Uplink

4.2.1.7.6.1.1     Uplink Bit Rate

The Command Uplink shall operate at one of two selectable rates, including all headers and other formatting, as follows:

[**Redacted**]

4.2.1.7.6.1.2     Bit Error Rate

The Command Uplink shall provide a bit error rate not to exceed [**Redacted**] .

4.2.1.7.6.1.3     Availability

The Command Uplink shall provide an availability of at least [**Redacted**] .

4.2.1.7.6.1.4     Elevation Angle

The Command Uplink shall operate at elevation angles of [**Redacted**] .

4.2.1.7.6.1.5     Link Margin

The Command Uplink shall meet all performance and functional requirements specified herein at EOL with a link margin of at least [**Redacted**] .

4.2.1.7.6.1.6    [**Redacted**]

[**Redacted**]

4.2.1.7.6.1.7     Modulation

The Command Uplink shall be modulated using [**Redacted**] .

4.2.1.7.6.1.8     Radio Frequency

The nominal Command Uplink carrier frequency shall be [**Redacted**] .

4.2.1.7.6.1.9     Antenna Coverage

Command Uplink antenna coverage shall be provided as follows:

[**Redacted**]

c) Provides realistic allowances for blockages by the Instrument.

4.2.1.7.6.1.10     Antenna Polarization

The Command Uplink antenna shall use [**Redacted**] .

4.2.1.7.6.1.11     Idle Patterns

[**Redacted**]

4.2.1.7.6.2     Telemetry Downlink

4.2.1.7.6.2.1     [**Redacted**] Telemetry Bit Rate

The Telemetry Downlink shall be at the following selectable rates, including all header and other formatting required to structure the commands:

[**Redacted**]

 

 

 

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4.2.1.7.6.2.2     [**Redacted**] Telemetry Bit Rate

The Telemetry Downlink shall be at a rate of [**Redacted**].

4.2.1.7.6.2.3     Bit Error Rate

The Telemetry Downlink shall provide a bit error rate not to exceed [**Redacted**] .

4.2.1.7.6.2.4     Availability

The Telemetry Downlink shall provide an availability of at least [**Redacted**] .

4.2.1.7.6.2.5     Elevation Angle

The Telemetry Downlink shall operate at elevation angles of [**Redacted**] .

4.2.1.7.6.2.6     Link Margin

The Telemetry Downlink shall meet all performance and functional requirements specified herein at EOL with a link margin of at least [**Redacted**] .

4.2.1.7.6.2.7    [**Redacted**]

[**Redacted**]

4.2.1.7.6.2.8     [ **Redacted** ]

[**Redacted**]

4.2.1.7.6.2.9     Modulation

 

a) The Telemetry Downlink shall use [**Redacted**] modulation as specified in the [**Redacted**] .

 

b) Any processing of the original data stream before transmission shall result in a [**Redacted**] .

4.2.1.7.6.2.10     Radio Frequency

The nominal Telemetry Downlink carrier frequency shall be [**Redacted**] .

4.2.1.7.6.2.11     Antenna Coverage: Special / Contingency Modes

 

a) Telemetry Downlink antenna coverage shall support all RF performance requirements specified herein (e.g. all downlink rates, both real-time and stored telemetry, BER, availability, elevation angle, etc.) with a [**Redacted**] when transmitting within [**Redacted**] .

 

b) A minimum elevation angle up to [**Redacted**] shall be permitted.

 

c) It shall be permissible to require ground commands in order to [**Redacted**] for operation in this mode, for example to switch from [**Redacted**] to [**Redacted**]

4.2.1.7.6.2.12     Antenna Coverage: Normal Operating Modes

Telemetry Downlink antenna coverage shall support all RF performance requirements specified herein (e.g. all downlink rates, BER, link margin, etc.) as follows:

[**Redacted**]

4.2.1.7.6.2.13     Antenna Polarization

The Telemetry Downlink antenna shall use [**Redacted**]

 

 

 

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4.2.1.7.6.2.14     Adjustable RF Output Power

The Telemetry Downlink shall provide the capability to adjust RF output power levels by ground command (real-time or stored), in increments sufficient to meet the link margin and interference limits specified in Sections 3.2.1.7.6.2.6 Link Margin and 3.1.2.1 Non-interference with Outside Systems, at any altitude over the range specified in Section 3.2.1.1.2.1 General Orbit Compatibility.

[**Redacted**]

4.2.1.7.7    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.1    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.2    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.3    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.4    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.5    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.6    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.7    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.7.1.8    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.9    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.10    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.11    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.12     [ **Redacted** ]

[**Redacted**]

4.2.1.7.7.1.13    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.14    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.15    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.16    [**Redacted**]

[**Redacted**]

4.2.1.7.7.1.17    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2     [ **Redacted** ]

[**Redacted**]

 

 

 

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4.2.1.7.7.2.1     [ **Redacted** ]

[**Redacted**]

4.2.1.7.7.2.2     [ **Redacted** ]

[**Redacted**]

4.2.1.7.7.2.3     [ **Redacted** ]

[**Redacted**]

4.2.1.7.7.2.4     [ **Redacted** ]

[**Redacted**]

4.2.1.7.7.2.5    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.6    [**Redacted**]

4.2.1.7.7.2.7    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.8    [**Redacted**]

4.2.1.7.7.2.9    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.10    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.11    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.12    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.13    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.7.2.14    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.15    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.16    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.17    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.18    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.19    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.20    [**Redacted**]

[**Redacted**]

4.2.1.7.7.2.21    [**Redacted**]

[**Redacted**]

4.2.1.7.8     EPDS

4.2.1.7.8.1     Functional Requirements

The EPDS shall perform the following functions under the Conditions and Operational Scenarios specified below:

 

a) Provide sufficient power to all Spacecraft Bus and Instrument equipment to

[**Redacted**]

4.2.1.7.8.2     Realistic Worst Case Conditions

EPDS performance shall be evaluated under realistic worst-case conditions [**Redacted**], including, but not limited to:

[**Redacted**]

4.2.1.7.8.3     Operational Scenarios

EPDS performance shall be evaluated using the following operational scenarios for the range of orbits specified in Section 3.2.1.1.2.1 General Orbit Compatibility. For requirements verification, it is acceptable to perform in-depth analysis [**Redacted**]

 

 

 

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4.2.1.7.8.4     Instrument Power

The EPDS shall provide power to the Instrument as specified in Section 3.1.3.1.3 Power Interfaces.

4.2.1.7.8.5    [**Redacted**]

[**Redacted**]

4.2.1.7.8.6    [**Redacted**]

[**Redacted**]

4.2.1.7.8.7    [**Redacted**]

[**Redacted**]

4.2.1.7.8.8    [**Redacted**]

[**Redacted**]

4.2.1.7.9     Structures and Mechanisms

4.2.1.7.9.1     Functional Requirements

The Structure shall perform the following functions:

 

a) Support all Bus and Instrument equipment through all mission phases, including pre-launch, launch, initialization, normal operations, and EOL disposal.

 

b) [**Redacted**]

4.2.1.7.9.2     Factors and Margins of Safety

[**Redacted**]

4.2.1.7.9.3     Mechanisms

4.2.1.7.9.3.1    [**Redacted**]

[**Redacted**]

4.2.1.7.9.3.2     Accessibility

Deployment devices shall be accessible with minimum disturbance to the relative position of the mechanisms or their thermal control hardware.

4.2.1.7.9.3.3     Thermal Constraints

There shall be no thermal constraints against the operation of any mechanism at any time during the Satellite Mission Life such that:

[**Redacted**]

4.2.1.7.9.3.4    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.9.3.5    [**Redacted**]

[**Redacted**]

4.2.1.7.10     Thermal Control

4.2.1.7.10.1     Functional Requirements

The Thermal Control subsystem shall autonomously perform the following functions under the Conditions and Operational Scenarios specified below:

[**Redacted**]

4.2.1.7.10.2     Realistic Worst Case Conditions

Thermal Control Subsystem performance shall be evaluated under realistic worst-case conditions (i.e. precluding combinations of conditions that can not physically occur), including, but not limited to:

[**Redacted**]

4.2.1.7.10.3     Operational Scenarios

The Thermal Control Subsystem performance shall be evaluated using the following operational scenarios for the range of orbits specified in Section 4.2.1.1.2.1 General Orbit Compatibility. For requirements verification, it is acceptable to perform in-depth analysis [**Redacted**]

4.2.1.7.10.4    [**Redacted**]

[**Redacted**]

4.2.1.7.10.4.1    [**Redacted**]

[**Redacted**]

4.2.1.7.10.4.2    [**Redacted**]

[**Redacted**]

4.2.1.7.10.4.3    [**Redacted**]

[**Redacted**]

4.2.1.7.10.4.4    [**Redacted**]

[**Redacted**]

4.2.1.7.10.4.5    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.10.4.6    [**Redacted**]

[**Redacted**]

4.2.1.7.10.4.7    [**Redacted**]

[**Redacted**]

4.2.1.7.10.4.8    [**Redacted**]

4.2.1.7.10.4.9    [**Redacted**]

[**Redacted**]

4.2.1.7.10.5    [**Redacted**]

[**Redacted**]

4.2.1.7.11     Direct Tasking

The Satellite shall provide Direct Tasking capabilities as specified below, with the following definitions of key terms:

[**Redacted**]

4.2.1.7.11.1    [**Redacted**]

[**Redacted**]

4.2.1.7.11.1.1    [**Redacted**]

[**Redacted**]

4.2.1.7.11.1.2    [**Redacted**]

[**Redacted**]

4.2.1.7.11.1.3    [**Redacted**]

[**Redacted**]

4.2.1.7.11.1.4    [**Redacted**]

[**Redacted**]

4.2.1.7.11.1.5    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.11.1.6    [**Redacted**]

[**Redacted**]

4.2.1.7.11.1.7    [**Redacted**]

[**Redacted**]

4.2.1.7.11.2    [**Redacted**]

[**Redacted**]

4.2.1.7.11.2.1    [**Redacted**]

[**Redacted**]

4.2.1.7.11.2.2    [**Redacted**]

[**Redacted**]

4.2.1.7.11.2.3    [**Redacted**]

[**Redacted**]

4.2.1.7.11.2.4    [**Redacted**]

[**Redacted**]

4.2.1.7.11.2.5    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3.1    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3.2    [**Redacted**]

[**Redacted**]

 

 

 

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4.2.1.7.11.3.3    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3.4    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3.5    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3.6    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3.7    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3.8    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3.9    [**Redacted**]

[**Redacted**]

4.2.1.7.11.3.10    [**Redacted**]

[**Redacted**]

4.2.1.7.11.4    [**Redacted**]

[**Redacted**]

4.2.1.7.11.4.1    [**Redacted**]

[**Redacted**]

4.2.1.7.11.4.2    [**Redacted**]

[**Redacted**]

 

 

 

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  38


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

4.2.1.7.11.4.3    [**Redacted**]

[**Redacted**]

4.2.1.7.11.4.4    [**Redacted**]

[**Redacted**]

4.2.1.7.11.4.5    [**Redacted**]

[**Redacted**]

4.2.1.7.11.4.6    [**Redacted**]

[**Redacted**]

4.2.1.7.11.4.7    [**Redacted**]

[**Redacted**]

4.2.1.7.11.4.8    [**Redacted**]

[**Redacted**]

4.2.1.7.11.4.9    [**Redacted**]

[**Redacted**]

4.2.1.7.11.5    [**Redacted**]

4.2.1.7.11.5.1    [**Redacted**]

[**Redacted**]

4.2.1.7.11.5.2    [**Redacted**]

[**Redacted**]

4.2.1.7.11.5.3    [**Redacted**]

[**Redacted**]

4.2.1.7.11.5.4    [**Redacted**]

[**Redacted**]

4.2.1.7.11.5.5    [**Redacted**]

[**Redacted**]

4.2.1.7.11.5.6    [**Redacted**]

[**Redacted**]

 

 

 

ITAR-Controlled Document

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Use or disclosure of data is subject to the restriction on the title page of this document.

  39


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

4.2.1.7.11.5.7    [**Redacted**]

[**Redacted**]

4.2.2    Physical Characteristics

4.2.2.1    Size Constraints

The size of the integrated Satellite shall be compatible with the specified Launch Vehicles and Shipping Constraints.

4.2.2.2    Mass Constraints

The total Satellite mass (including all parts of the Launch Vehicle adapter / separation mechanism that remain with the Satellite after separation) shall not exceed the limits established by the [**Redacted**] and the [**Redacted**] .

[**Redacted**]

4.2.2.3    Shipping Constraints

The Satellite and associated Ground Support Equipment (GSE), including the shipping container, shall be designed to allow transportation to the Launch Site via the [**Redacted**] or by [**Redacted**] and [**Redacted**] .

4.2.3    Reliability

4.2.3.1    End of Life Ps

[**Redacted**]

4.2.3.2    [**Redacted**]

[**Redacted]

4.2.3.3    [**Redacted**]

[**Redacted**]

4.2.3.4    Cycle-Limited Items

Items whose life is limited by the total number of operating cycles shall meet all on-orbit performance requirements after operating for [**Redacted**] the predicted number of cycles, including all cycles incurred during both the Mission Life and during ground testing. Cycle-limited items shall include at a minimum:

[**Redacted**]

4.2.3.4.1    [**Redacted**]

[**Redacted**]

4.2.3.4.2    [**Redacted**]

[**Redacted**]

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

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  40


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

4.2.4    Availability and Maintainability

4.2.4.1    Fault Recovery Timeline

The Satellite equipment provided by the SSI shall be designed to allow recovery from any fault conditions and single event upsets or latch-ups within [**Redacted**] of ground operator intervention, with the exception of [**Redacted**] , which shall take no longer than [**Redacted**]

4.2.4.2    Environmental Conditions

The Satellite shall meet all functional and performance requirements after exposure to the following environments.

4.2.4.2.1     Launch Induced Environments

[**Redacted**]

4.2.4.2.2     On-Orbit Environments

On-orbit environments shall be consistent with operation in the Mission Orbit for the Mission Life and shall include, at a minimum:

[**Redacted**]

4.2.4.2.3     Pre-Launch Environments

Except for any specific testing aimed at verifying the design margins, the Satellite shall not be subjected to any environments that exceed the launch and on-orbit environments. This includes integration and test activities, transportation, launch site processing, and the period the Satellite is within the Launch Vehicle Fairing prior to launch.

4.3    Satellite Design and Construction

4.3.1    General

The Satellite Design and Construction shall be performed per standard SSI practices in accordance with the Environmental Design and Test Specification and the DigitalGlobe Space Segment Specification Addendum, including at a minimum the following items:

[**Redacted**]

4.3.2    SEUs

[**Redacted**]

4.3.3    Immunity to Latch-Up

[**Redacted**]

4.3.4    Cleanliness and Contamination Control

[**Redacted**]

4.3.4.1    [**Redacted**]

[**Redacted**]

 

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

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  41


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 5.0: 2 May 2011

 

 

4.3.4.2    [**Redacted**]

[**Redacted**]

4.3.4.3    [**Redacted**]

[**Redacted**]

4.3.4.4    [**Redacted**]

[**Redacted**]

4.3.5    Safety

The Satellite shall be designed to allow for safe handling, operation, transportation, fuel loading and pressurization through all mission phases. It shall comply with the specific requirements of [**Redacted**] , including at a minimum:

[**Redacted**]

4.3.6    [**Redacted**]

[**Redacted**]

 

5. VERIFICATION

Requirements verification shall be performed per standard SSI practices, in accordance with the DigitalGlobe Space Segment Specification Addendum and the Statement of Work.

 

6. QUALITY ASSURANCE

Quality Assurance shall be performed per standard SSI practices, in accordance with the DigitalGlobe Space Segment Specification Addendum and the Statement of Work.

 

 

 

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  42


Attachment 3

WorldView 3 Payment Milestone Schedule, Rev 2.1

Dated 13 May 2011


WorldView 3 Payment Milestone Schedule

Exhibit 3 to WV3 Satellite Agreement # 60150

 

Item

#

  

Invoice Date

  

Line
Item

  

Description

   Completed   

Milestone

Value

  

Cumulative
Milestones

  

Termination
Liability

1    [**Redacted**]       Milestone 1 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]            
2    [**Redacted**]       Milestone 2 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
3    [**Redacted**]       Milestone 3 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
4    [**Redacted**]       Milestone 4 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
5    [**Redacted**]       Milestone 5 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
6    [**Redacted**]       Milestone 6 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
7    [**Redacted**]       Milestone 7 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
8    [**Redacted**]       Milestone 8 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
9    [**Redacted**]       Milestone 9 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
10    [**Redacted**]       Milestone 10 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      


11    [**Redacted**]       Milestone 11 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
12    [**Redacted**]       Milestone 12 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
13    [**Redacted**]       Milestone 13 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
14    [**Redacted**]       Milestone 14 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
15    [**Redacted**]       Milestone 15 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
      e    [**Redacted**]       [**Redacted**]      
16    [**Redacted**]       Milestone 16 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
17    [**Redacted**]       Milestone 17 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
18    [**Redacted**]       Milestone 18 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
19    [**Redacted**]       Milestone 19 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      


20    [**Redacted**]       Milestone 20 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
21    [**Redacted**]       Milestone 21 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
22    [**Redacted**]       Milestone 22 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
23    [**Redacted**]       Milestone 23 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
24    [**Redacted**]       Milestone 24 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
25    [**Redacted**]       Milestone 25 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
26    [**Redacted**]       Milestone 26 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
27    [**Redacted**]       Milestone 27 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
28    [**Redacted**]       Milestone 28 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      


29    [**Redacted**]       Milestone 29 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
30    [**Redacted**]       Milestone 30 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
31    [**Redacted**]       Milestone 31 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
32    [**Redacted**]       Milestone 32 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
33    [**Redacted**]       Milestone 33 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
34    [**Redacted**]       Milestone 34 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
35    [**Redacted**]       Milestone 35 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
36    [**Redacted**]       Milestone 36 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
37    [**Redacted**]       Milestone 37 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
      e    [**Redacted**]       [**Redacted**]      
38    [**Redacted**]       Milestone 38 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      


39    [**Redacted**]       Milestone 39 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
      b    [**Redacted**]         [**Redacted**]         
      c    [**Redacted**]         [**Redacted**]         
      d    [**Redacted**]         [**Redacted**]         
40    [**Redacted**]       Milestone 40 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
      b    [**Redacted**]         [**Redacted**]         
      c    [**Redacted**]         [**Redacted**]         
      d    [**Redacted**]         [**Redacted**]         
41    [**Redacted**]       Milestone 41 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
      b    [**Redacted**]         [**Redacted**]         
      c    [**Redacted**]         [**Redacted**]         
42    [**Redacted**]       Milestone 42 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
      b    [**Redacted**]         [**Redacted**]         
      c    [**Redacted**]         [**Redacted**]         
43    [**Redacted**]       Milestone 43 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
      b    [**Redacted**]         [**Redacted**]         
      c    [**Redacted**]         [**Redacted**]         
      d    [**Redacted**]         [**Redacted**]         
44    [**Redacted**]       Milestone 44 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
      b    [**Redacted**]         [**Redacted**]         
45    [**Redacted**]       Milestone 45 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
      b    [**Redacted**]         [**Redacted**]         
46    [**Redacted**]       Milestone 46 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
      b    [**Redacted**]         [**Redacted**]         
      c    [**Redacted**]         [**Redacted**]         
      d    [**Redacted**]         [**Redacted**]         
47    [**Redacted**]       Milestone 47 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
48    [**Redacted**]       Milestone 48 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      a    [**Redacted**]         [**Redacted**]         
      b    [**Redacted**]         [**Redacted**]         
      c    [**Redacted**]         [**Redacted**]         
         TOTALS       $ 184,817,399       $ 184,817,399       $ 180,575,000   

Exhibit 10.5.3

FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

Amendment No. 4

To the

WorldView 3 Satellite Purchase Agreement #60150

This Amendment No. 4 (“Amendment”) to WorldView 3 Satellite Purchase Agreement #60150 (the “Agreement”) is entered into by and between DigitalGlobe, Inc. (“DigitalGlobe”), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, CO 80503; and Ball Aerospace & Technologies Corp., a Delaware corporation with its principal offices located at 1600 Commerce Street, Boulder, CO 80301 (“BATC”). As used in this Agreement, “Party” means either DigitalGlobe or BATC, as appropriate, and “Parties” means DigitalGlobe and BATC.

WHEREAS, DigitalGlobe and BATC entered into the WorldView 3 Satellite Purchase Agreement #60150 (“Agreement”) on September 1, 2010;

Now, THEREFORE, the parties hereby agree to amend the Agreement to incorporate the following Engineering Change Proposals (“ECP”):

 

1. ECP 010: [**Redacted**] .

[**Redacted**]

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**] .

 

2. ECP 011: [**Redacted**] .

[**Redacted**]

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**] .

 

3. ECP 012: Document Updates

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the tide page of this document.


This change updates three specifications currently under contract. In addition the Payment Milestone Schedule, Exhibit 3, has been updated. This change also adds a new specification [**Redacted**] .

Therefore, this Amendment updates and adds the following documents which are provided as Attachments 1-5 to the Agreement.

 

  a. Exhibit 1 to the Agreement, titled “Statement of Work for the WorldView 3 Satellite -10329656, Rev 2.0,” and dated 14 April 2011, is replaced in its entirety by the updated version “Statement of Work for the WorldView 3 Satellite — 10329656, Rev 3.0,” dated 9 September 2011, included as Attachment 1 to this Amendment; and

 

  b. Exhibit 2 to the Agreement, titled “DigitalGlobe WorldView 3 Satellite Specification —10329655, Rev 5.0,” and dated 2 May 2011, is replaced in its entirety by the updated version “DigitalGlobe WorldView 3 Satellite Specification — 10329655, Rev 7.0”, dated 13 September 2011, included as Attachment 2 to this Amendment; and

 

  c. Exhibit 3 to the Agreement, titled “WorldView 3 Payment Milestone Schedule —10329669, Rev 2.1” and dated 13 May 2011, is replaced in its entirety by the updated version “WorldView 3 Payment Milestone Schedule, Rev - 10329669, Rev 3.0,” dated 9 September 2011, included as Attachment 3 to this Amendment; and

 

  d. “WV3 Spacecraft Simulator Specification — 10258368, Initial Release”, and dated 20 December 2010, is replaced in its entirety by the document “WV3 Spacecraft Simulator Specification — 10258368, Rev 1.0”, dated 9 September 2011, included as Attachment 4 to this Amendment; and

 

  e. [**Redacted**] .

SUMMARY

The value for these ECPs is $28,460,000, outlined in the following table:

 

Change #

  

Change Description

   $  
010    [**Redacted**]    $ [**Redacted**]   
011    [**Redacted**]    $ [**Redacted**]   
012    Documentation Updates    $ 0.00   
     

 

 

 
   TOTAL    $ 28,460,000.00   
     

 

 

 

Contract Value Summary

 

Previous Contract Value

   $ 184,817,399.00   

ECPs

   $ 28,460,000.00   
  

 

 

 

New Contract Value

   $ 213,277,399.00   
  

 

 

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


Unless otherwise expressly provided herein, all other terms and conditions of the Agreement shall remain in full force and effect.

This Amendment No. 4 is hereby executed and agreed to by DigitalGlobe and BATC and shall be binding and effective as of the last date executed below.

 

Ball Aerospace & Technologies Corp.    Digital Globe, Inc.
[**Redacted**]   

/s/ Yancey Spruill

   EVP, Chief Financial Officer
September 28, 2011    September 22, 2011


Attachment 1

Statement of Work for the WorldView 3 Satellite, Rev 3.0

Dated 9 Sept 2011


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

 

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   WV3 Satellite Statement of Work_
   Doc Number 10329656

 

 

Exhibit 1 to Agreement 60150

Statement of Work

for the WorldView 3

Satellite

 

 

 

  Document Number   10329656
  Release Date:   Sept 9, 2011
  Issue/Revision:   Release 3.0
  Prepared by:   Brian Uzzle
  Approved by   Steve Linn

RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION

This document contains information proprietary and confidential to DigitalGlobe Incorporated, to its subsidiaries, or to a third party to whom DigitalGlobe Incorporated may have a legal obligation to protect such information from unauthorized disclosure, use or duplication. Any disclosure, use or duplication of this document or of any of the information contained herein for other than the specific purpose for which it was disclosed is expressly prohibited, except as DigitalGlobe Incorporated may otherwise agree to in writing. This document may only be used for the purpose for which it is provided. All copies of this document are the sole property of DigitalGlobe and will be returned promptly upon request.

 

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Change Record

 

Issue

  

Date

  

Section(s)

  

Description of Change

Initial    20 Aug 2010       Initial Release
Rev 1    7 Feb 2011    2.1    Updated references for Satellite Specification, Satellite Simulator Specification, and Instrument Specification
      3.1.b    Updated dates for Satellite Simulator releases and number of deliveries
      3.1.n    Added deliverable item [**Redacted**]
      3.1.o    Added deliverable item [**Redacted**] .
      13.8.1    Clarified WV3 simulator changes versus WV2 simulator [**Redacted**] .
      Attachment 1    Updated release dates for Satellite Simulator (LM-8), Satellite Simulator Documentation (LM-9), and Satellite Simulator Source Code (LM-10).
      Attachment 1    Updated [**Redacted**] (CFHW-1)
Rev 2    14 Apr 2011    10.2.2    Updated [**Redacted**] , to be consistent with the date in Attachment 1 (CFHW-2)
      1.2, 2.1, 4.5.3.2.F, [**Redacted**] , 11.4, 12.1, 12.2, 12.3, Attachment 2   

Changed launch vehicle baseline from Delta-2 to Atlas V.

Changed number of TIMs from 8 to 20.

Changed SLRR from [**Redacted**] to [**Redacted**] .

      3.1(b)    Updated delivery date for Simulator [**Redacted**] per Ball’s request.
Rev 3    9 Sep 2011    1.1    Added definitions for [**Redacted**] .
      2.1    Added [**Redacted**] specification. Updated Satellite Spec and Simulator Spec versions. Changed BATC documents for Configuration and Data Management to current doc numbers and release versions. Updated Spaceport Systems International handbook version.
      3.1.a    Updated delivery date for Satellite, based on [**Redacted**]
      3.1.b    Updated delivery date for Simulator [**Redacted**] (LM-8) to match agreed upon dates.
      3.1.p, 3.1.q    Added deliverable items for [**Redacted**]
      4.2    Added [**Redacted**]
      4.5.3.1    Added [**Redacted**]
      4.5.3.2.F    Added [**Redacted**] specifics
      5.2.2    Added [**Redacted**] .
      5.3.9.1    Added [**Redacted**]
      5.3.11.i-m    Added [**Redacted**]
      6.2.2    Updated PCB Section to reflect virtual nature of PCBs
      9.3.b    Added [**Redacted**]
      9.3.g    Added [**Redacted**]
      10.5.9    Added [**Redacted**]
      13.5.g-l    Added [**Redacted**]
      Attachment 1    Added [**Redacted**] and CGSE-16. Changed [**Redacted**]
      n/a    Added Table of Contents

 

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Issue

  

Date

  

Section(s)

  

Description of Change

        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        

 

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   Doc Number 10329656

 

Issue

  

Date

  

Section(s)

  

Description of Change

        
        
        
        
        
        

 

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Table of Contents

 

1.0   INTRODUCTION      1   
 

1.1

  D EFINITIONS      1   
 

1.2

  P ROGRAM O VERVIEW      2   
2.0   DOCUMENTS      3   
 

2.1

  A PPLICABLE D OCUMENTS      3   
 

2.2

  R EFERENCE D OCUMENTS      4   
3.0   CONTRACT DELIVERABLES      5   
 

3.1

  D ELIVERABLE I TEMS      5   
 

3.2

  D ELIVERABLE D ATA      5   
 

3.3

  D ELIVERABLE S ERVICES      5   
4.0   PROGRAM MANAGEMENT      6   
 

4.1

  P ROGRAM P HILOSOPHY      6   
 

4.2

  BATC O RGANIZATION (CDIL PM-1)      6   
 

4.3

  D IGITAL G LOBE M ANAGEMENT      7   
 

4.4

  S PACE S EGMENT M ASTER P ROGRAM S CHEDULE (MPS) (CDIL PM-2)      7   
    4.4.1   

General

     7   
    4.4.2   

Required Software

     7   
    4.4.3   

MPS Construction

     7   
    4.4.4   

Reports

     8   
 

4.5

  M EETINGS & R EVIEWS      8   
    4.5.1   

Weekly Status Meeting

     8   
    4.5.2   

Monthly Program Status Review

     8   
    4.5.3   

Program Reviews

     8   
    4.5.4   

Component/Subsystem Design Review Listing (CDIL PM-3)

     11   
    4.5.5   

Component/Subsystem Test Readiness / Data Review Listing (CDIL PM-4)

     11   
    4.5.6   

DigitalGlobe Meetings

     11   
 

4.6

  D OCUMENTATION M ANAGEMENT      12   
    4.6.1   

Access to Program Technical Data

     12   
    4.6.2   

Objective

     12   
    4.6.3   

Documentation Listing (CDIL PM-5)

     12   
    4.6.4   

Documentation Delivery

     12   
 

4.7

  A CTION I TEM T RACKING (CDIL PM-6)      13   
 

4.8

  F INANCIAL M ANAGEMENT      13   
    4.8.1   

Historical Record of Payments (CDIL PM-7)

     13   
    4.8.2   

Payments Forecast (CDIL PM-7)

     13   
 

4.9

  C ONTRACT C HANGE C ONTROL      13   
5.0   DESIGN      15   
 

5.1

  G ENERAL      15   
 

5.2

  W ORKING G ROUPS AND T RADE S TUDIES      15   

 

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    5.2.1   

Working Groups

     15   
    5.2.2   

Trade Studies

     15   
 

5.3

 

S ATELLITE D ESIGN D ATA

     15   
    5.3.1   

Satellite to Instrument Interface Control Document(s) (CDIL D-1)

     15   
    5.3.2   

Satellite to Ground Terminal Narrowband Link ICD (CDIL D-2)

     15   
    5.3.3   

Satellite to Ground Terminal Wideband Link ICD (CDIL D-3)

     15   
    5.3.4   

Satellite Environmental Design and Test Specification (EDTS) (CDIL D-4)

     15   
    5.3.5   

Contamination Control Plan(s) (CDIL D-5)

     16   
    5.3.6   

Satellite Level Requirements Verification/Compliance Matrix (CDIL D-6)

     16   
    5.3.7   

Box Level Requirements Verification/Compliance Matrix (CDIL D-7)

     16   
    5.3.8   

Drawings (CDIL D-8)

     16   
    5.3.9   

Performance Compliance and Risk Management

     16   
    5.3.10   

Subsystem Description Documents (CDIL D-11)

     17   
    5.3.11   

Analysis and reports

     17   
    5.3.12   

Other Interface Control Documents

     18   
    5.3.13   

Critical Items list (CDIL D-18)

     18   
    5.3.14   

Component Heritage Summary (CDIL D-19)

     19   
    5.3.15   

Engineering Reports (CDIL D-20)

     19   
    5.3.16   

Flight Software Source Code (CDIL D-21)

     19   
    5.3.17   

Composite Grounding Design (CDIL D-22)

     19   
    5.3.18   

Structural, Power, Thermal, and Reliability Analytical Models (CDIL D-23)

     19   
    5.3.19   

Coordinate Transformation Document (CDIL D-24)

     20   
    5.3.20   

Flight Software Users Manual (CDIL D-25)

     20   
    5.3.21   

Component Acceptance Data Package (CDIL D-26)

     20   
    5.3.22   

Jitter/MTF Analysis and Test Data (CDIL D-27)

     20   
    5.3.23   

Instrument/Sensor Boresight Stability Data (CDIL D-28)

     20   
    5.3.24   

Position and Attitude Accuracy (CDIL D-29)

     20   
    5.3.25   

Satellite to MGB Interface Control Document(s) (CDIL D-32)

     20   
    5.3.26   

DigitalGlobe to BATC Electrical GSE Interface Control Document (CDIL D-33)

     21   
6.0   PRODUCT ASSURANCE      22   
 

6.1

 

P RODUCT A SSURANCE P LAN

     22   
 

6.2

 

BATC P ARTS C ONTROL B OARD (PCB)

     22   
    6.2.1   

Subcontractor Parts Control Board (PCB)

     22   

 

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    6.2.2    PCB Meetings      22   
  6.3   P ARTS AND M ATERIALS      23   
    6.3.1    Electrical, Electronic, and Electro-mechanical Parts (EEE)Parts Listing (CDIL QA-1)      23   
    6.3.2    Material and Processes Reports (CDIL QA-2)      23   
  6.4   A S -B UILT C ONFIGURATION AND C ONFORMANCE      23   
    6.4.1    As-Built Configured Article List (CDIL QA-3)      23   
    6.4.2    Certificate of Conformance (CDIL QA-4)      23   
  6.5   P RODUCT A SSURANCE R EVIEWS (CDIL QA-5)      23   
  6.6   D OCUMENTATION      24   
  6.7   K NOWN N ON -C OMPLIANT H ARDWARE      24   
  6.8   M ILITARY S TANDARD 461      24   
7.0   PROCUREMENT      25   
  7.1   G ENERAL      25   
  7.2   M AKE /B UY P LANS (CDIL PT-1)      25   
  7.3   E NCRYPTION /D ECRYPTION D EVICES      25   
  7.4   R EVIEWS      25   
  7.5   P ROGRAM S UBCONTRACT S TATUS R EPORT (PSSR) (CDIL PT-2)      25   
  7.6   D OCUMENTATION      25   
  7.7   S UBCONTRACT F LOW - DOWNS      25   
    7.7.1    Assignment Clause      25   
    7.7.2    Access      25   
8.0   PRODUCTION ACTIVITIES      26   
  8.1   G ENERAL      26   
  8.2   P RODUCTION P ROCESS      26   
  8.3   A CCESS      26   
  8.4   P RODUCTION D OCUMENTATION      26   
9.0   INTEGRATION AND TEST ACTIVITIES      27   
  9.1   G ENERAL      27   
  9.2   B OX /S UBSYSTEM L EVEL T ESTING      27   
    9.2.1   

General

     27   
    9.2.2    [**Redacted**]      27   
  9.3   WV B US AND S ATELLITE I NTEGRATION AND T EST P LANS (CDIL PT-3)      27   
  9.4   P OST -S HIPMENT I NSTRUMENT T ESTING      27   
  9.5   S UPPORTING D OCUMENTS      28   
  9.6   S YSTEM T EST R EPORTS (CDIL PT-5)      28   
    9.6.1    Content      28   
    9.6.2    Timeliness      28   
  9.7   U NINTERRUPTIBLE P OWER S UPPLY (UPS)      28   
  9.8   D IGITAL G LOBE I NTEGRATION AND T EST E NGINEERING A CCESS      28   
    9.8.1    On-Site and Visiting Engineers      28   

 

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    9.8.2    Access to Live Satellite Telemetry      28   
    9.8.3    Test Observation By Other DG Engineers      29   
    9.8.4    Access to Command and Telemetry Log Files (CDIL PT-6)      29   
  9.9   T EST R EVIEWS      29   
  9.10   O PTIONAL T ESTING      29   
10.0   CUSTOMER FURNISHED EQUIPMENT AND SERVICES      30   
  10.1   G ENERAL      30   
  10.2   F LIGHT E QUIPMENT      30   
    10.2.1    [**Redacted**]      30   
    10.2.2    [**Redacted**]      30   
    10.2.3    [**Redacted**]      30   
    10.2.4    [**Redacted**]      30   
    10.2.5    [**Redacted**]      30   
    10.2.6    [**Redacted**]      30   
  10.3   S IMULATORS (CSIM-1)      30   
  10.4   L AUNCH V EHICLE I NTERFACES      31   
    10.4.1    Launch Vehicle Interface      31   
    10.4.2    Launch Vehicle Separation Connectors (CLSE-3)      31   
  10.5   G ROUND S UPPORT E QUIPMENT      31   
    10.5.1    Wideband Link RGT Equipment      31   
    10.5.2    Narrowband Link RGT Equipment (CGSE-5)      31   
    10.5.3    Special Test Equipment      31   
    10.5.4    Mission Control Center (CGSE-11)      31   
    10.5.5   

[**Redacted**]

     31   
    10.5.6   

[**Redacted**]

     32   
    10.5.7   

[**Redacted**]

     32   
    10.5.8    MGB Test Equipment (CGSE-15)      32   
  10.6   L AUNCH V EHICLE D ATA (CLD-1 AND CLD-2)      32   
  10.7   I NSTRUMENT D ATA      32   
    10.7.1    Instrument Structural Analysis Data (CID-1)      32   
    10.7.2    Instrument Thermal Analysis Data (CID-2)      32   
11.0   STORAGE AND DELIVERY      33   
  11.1   G ENERAL      33   
  11.2   S ATELLITE P RE -S HIPMENT S TORAGE      33   
  11.3   P RE -S HIPMENT R E -T EST      33   
  11.4   S ATELLITE S HIPPING AND D ELIVERY      33   
  11.5   S ATELLITE L AUNCH S ITE S TORAGE      34   
12.0   LAUNCH SUPPORT SERVICES      35   
  12.1   G ENERAL      35   
  12.2   R EQUIREMENT D EFINITION      35   
  12.3   T ECHNICAL I NTERCHANGE M EETINGS      35   
  12.4   FEM AND CLA- TO -D ESIGN L OAD C OMPARISONS (CDIL LM-2)      35   

 

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  12.5   E XPORT R EGULATIONS      49   
  12.6   A DAPTER F IT -C HECK      49   
  12.7   L AUNCH S ITE I NFRASTRUCTURE      49   
  12.8   L AUNCH S ITE O PERATIONS      49   
  12.9   F UELING      50   
13.0   MISSION PREPARATION AND ON-ORBIT COMMISSIONING      51   
  13.1   T RAINING (CDIL LM-3)      51   
    13.1.1    Training Materials      51   
    13.1.2    Training Sessions      51   
  13.2   C OMMAND AND T ELEMETRY H ANDBOOK (CDIL LM-4)      51   
  13.3   B US S UBSYSTEM C ALIBRATION T OOLS (CDIL LM-5)      51   
  13.4   D IGITAL G LOBE P ROCEDURE D EVELOPMENT S UPPORT      51   
  13.5   C OMMISSIONING P LAN (CDIL LM-6)      52   
  13.6   A NOMALY P REPARATIONS      52   
  13.7   S ATELLITE C OMMISSIONING      52   
    13.7.1    Launch and Early Operations (LEOP) Phase      52   
    13.7.2    Verification and Calibration (V&C) Phase      52   
  13.8   S ATELLITE S IMULATOR      53   
    13.8.1    Satellite Simulator (CDIL LM-8)      53   
    13.8.2    Documentation (CDIL LM-9)      53   
    13.8.3    Source Code (CDIL LM-10)      54   
    13.8.4    Delivery Schedule      54   
    13.8.5    Technical Interchange Meetings and Design Reviews      54   
  13.9   M ANEUVER P LANNERS      54   
    13.9.1    High Fidelity Maneuver Planner (CDIL LM-11)      55   
    13.9.2    Peak Estimator Algorithm (Low Fidelity Maneuver Planner) (CDIL LM-12)      55   
    13.9.3    [**Redacted**]      55   
  13.10   S OFTWARE T EST B ENCH      55   
  13.11   G ROUND S TATIONS      55   
  13.12   T ELEMETRY P ACKET C REATION AND M APPING T OOLS (CDIL LM-15)      56   
  13.13   T ELEMETRY M ONITOR AND R ESPONSE (CDIL LM-16)      56   
14.0   COMMUNICATIONS FLEXIBILITY AND TT&C DEFINITION      56   
15.0   FACILITIES      56   
ATTACHMENT 1 CONTRACT DATA ITEMS LIST      1   
ATTACHMENT 2 CUSTOMER FURNISHED EQUIPMENT LIST      1   

 

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1.0 INTRODUCTION

This Statement of Work defines those tasks to be performed by BATC, the Space Segment Integrator, in defining; designing, producing, testing, verifying, and preparing for launch; the DigitalGlobe WorldView 3 Satellite. BATC has the overall responsibility for Satellite performance, as defined in the WV3 Satellite Specification, provided the DG-furnished Instrument meets its interfaces and specifications as defined in Paragraph 2.2. Within this role, BATC has the responsibility to work with DigitalGlobe to define requirements, allocate budgets, analyze performance, execute trade studies, interact with other vendors, define configurations(s), conform to existing Instrument interfaces, assess and mitigate risks, prepare various programmatic documentation, and interact with all participating organizations via meetings, teleconferences, and reviews as defined herein.

BATC shall provide integrating services as defined herein and the hardware and software, exclusive of Customer Furnished Equipment, that comprise the WV3 Satellite.

This document also defines the scope of work required from DigitalGlobe and associated subcontractors in order for BATC to execute this contract successfully.

Associate contractors under contract to DigitalGlobe shall provide the Instrument and Launch services. However, BATC shall fully support defining, documenting, and verifying Satellite(s) to LV and MGB interfaces and integration procedures. BATC shall insure that the Satellite will withstand all launch environments.

 

1.1 Definitions

Agreement: Satellite Purchase Agreement #60150 by and between DigitalGlobe, Inc. and Ball Aerospace and Technologies Corp., dated August 27, 2010, as amended.

Authorization to Proceed (ATP): Effective date of work commencement per the Agreement.

Satellite: The complete space-borne infrastructure required to perform the mission of providing radiometrically and geometrically correct imagery of the Earth. The Satellite consists of the Instrument and the Spacecraft Bus.

[**Redacted**]

Instrument: The Instrument is that part of the Satellite that collects light photons using appropriate mirrors and structure, [**Redacted**] . It also may be designated the Electro-Optical Assembly (EOA). The instrument includes its own thermal control system. However, the instrument focus mechanism depends upon drive electronics to be provided by BATC per this Statement of Work. Also, the instrument stimulation lamp depends upon drive electronics to be provided by BATC per this Statement of Work.

Telescope: That part of the Instrument that collects and focuses light onto a focal plane. [**Redacted**] It also may be designated the Optical Telescope Unit (OTU).

Sensor Subsystem (SSS): That part of the Instrument that converts photons to analog voltage signals, [**Redacted**] , and digitizes [**Redacted**] those signals.

 

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Solid State Recorder: The subsystem that accepts digital data from the SSS and Ancillary Data from the spacecraft bus, provides storage, [**Redacted**] and outputs that data to the wideband transmitter(s).

Spacecraft Bus: The Bus is that part of the Satellite that provides the support infrastructure so the Instrument can function.

[**Redacted**]

MGB: “MGB” is a meaningless three letter designation for an additional subsystem being installed on the WV3 satellite. The MGB subsystem consists of three components. The first is a Sensor Unit (SU) which will attach to the aperture end of the OBA. The second is the Interface Adaptor Unit (IAU) which will mount to the spacecraft bus. The third is an inter-connect cable which connects the first two units.

Initial Acceptance: Occurs upon successful completion of the Satellite Pre-Ship Review as defined in paragraph 4.5.3.2.e

Final Acceptance: Occurs following satellite fueling operations and completion of the Satellite Launch Readiness Review as defined in paragraph 4.5.3.2.f

Transfer of Title: Occurs as defined in the Satellite Purchase Agreement paragraph 8.

 

1.2 Program Overview

Under this Scope of Work, DigitalGlobe will procure one satellite to support the EnhancedView program and future commercial operations. DigitalGlobe shall provide the Instrument as Customer Furnished Equipment via a procurement contract with ITT. DigitalGlobe shall provide the “MGB” subsystem. As on the WV2 program, BATC shall deliver a WorldView 2 like stimulation lamp that will be incorporated into the ITT provided instrument. BATC shall also incorporate into the Bus, an instrument focus mechanism electronics capability.

DigitalGlobe shall provide the Launch Services via a procurement contract with Lockheed Martin-Commercial Launch Services. Lockheed Martin-Commercial Launch Services has in-turn subcontracted with United Launch Alliance to provide the Atlas V launch vehicle and associated launch services. BATC can assume an Atlas V launch vehicle and a launch from Vandenberg Air Force Base. BATC shall assume satellite processing at Vandenberg AFB will occur in either the Astrotech Payload Processing facility or the Spaceport Systems International Processing Facility.

 

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2.0 DOCUMENTS

 

2.1 Applicable Documents

This Statement-of-Work identifies applicable documents. These documents provide detailed requirements regarding Satellite performance, interfaces, and/or standardized design, fabrication, and testing processes/procedures. BATC and DigitalGlobe will perform the defined work according to these standardized processes/procedures such that the delivered products meet the performance and ICD requirements.

In the event of any conflict between these documents, the following order of precedence shall prevail: a) Agreement Terms & Conditions; b) Statement of Work; c) Satellite Specification; d) Other Applicable documents.

 

DigitalGlobe Produced or Provided Documents   

WV3 Satellite Specification

   [**Redacted**]

WV3 Spacecraft Simulator Specification

   [**Redacted**]

WV3 Command & Telemetry Handbook Specification

   [**Redacted**]

WV3 Maneuver Planner Specification

   [**Redacted**]

MGB Data Protection Plan for BATC

   [**Redacted**]

Stim Lamp and Stim Lamp Electronics Specification

   [**Redacted**]

[**Redacted**] Focus Mechanism Electronics Specification

   [**Redacted**]

Star Tracker Simulation Specification

   [**Redacted**]

IRU Simulator Specification

   [**Redacted**]

SSR to DPU Cable Design and Build Documentation

   [**Redacted**]

[**Redacted**]

   [**Redacted**]
BATC Produced Documents   

BATC Product Assurance Plan

   [**Redacted**]

BATC Supplier Product Assurance Plan

   [**Redacted**]

Civil & Operational Space (COS) SBU Configuration and Data Management (CD&M) Plan

   [**Redacted**]

WV-3 CDM Plan Addendum

   [**Redacted**]
Associated Contractor Produced Documents   

Astrotech Vandenberg Facility Accommodations Manual

   [**Redacted**]

Spaceport Systems International, Vandenberg Facility Payload Facility Handbook

   [**Redacted**]

Atlas V Launch Services User’s Guide

   [**Redacted**]

 

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   WV3 Satellite Statement of Work_
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2.2 Reference Documents

The following documents provide the baseline instrument definition. DigitalGlobe shall provide an instrument that is compliant with these documents.

 

DigitalGlobe Produced or Provided Documents   

Instrument Specification

   [**Redacted**]

Instrument Finite Element Model

   [**Redacted**]

 

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3.0 CONTRACT DELIVERABLES

 

3.1 Deliverable Items

 

  a. WV3 Satellite: Initial Acceptance: [**Redacted**] . Final Acceptance: [**Redacted**] Delivery shall be adjusted for Excusable Delay or failure of customer to [**Redacted**] to the extent that these delays affect the Delivery Date.

 

  b. WV3 Satellite Simulator
       Initial release: [**Redacted**]
       Simulator Delivery [**Redacted**]
       Functional and performance signoff: [**Redacted**]
       On orbit performance/tuning update: [**Redacted**]

 

  c. [**Redacted**]

 

  d. [**Redacted**]

 

  e. [**Redacted**]

 

  f. [**Redacted**]

 

  g. [**Redacted**]

 

  h. [**Redacted**]

 

  i. [**Redacted**]

 

  j. [**Redacted**]

 

  k. [**Redacted**]

 

  l. [**Redacted**]

 

  m. [**Redacted**]

 

  n. [**Redacted**]

 

  o. [**Redacted**]

 

  p. [**Redacted**]

 

  q. [**Redacted**]

 

3.2 Deliverable Data

Reference Attachment 1: Contractor Data Items List (CDIL)

 

3.3 Deliverable Services

 

  a. Storage and Delivery (Section 11.0)

 

  b. Launch Support (Section 12.0)

 

  c. Mission, Commissioning, & Readiness Support (Section 13.0)

 

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4.0 PROGRAM MANAGEMENT

 

4.1 Program Philosophy

Emphasis throughout all phases and functions of the project shall be to produce a reliable Satellite that meets the performance requirements on the contracted schedule. [**Redacted**]

 

4.2. BATC Organization (CDIL PM-1)

A dedicated Program Manager shall be appointed by BATC prior to the start of the contract. The Program Manager shall lead all of the Contractor’s activities under the contract.

A diagram illustrating the Program Management Structure shall be provided to DigitalGlobe. (CDIL PM-1) This diagram(s) shall indicate job titles and names of the program management team.

The Program Manager shall coordinate changes to contract conditions, price, timescale, deliverables, services or performance levels, unless a specific alternate has been appointed to deal with any of these matters. All changes to the contract documents shall require the written agreement of BATC contracts representative.

BATC shall also appoint a different and dedicated individual to be a single point of contact for each of the following:

 

  a. Program technical management (Satellite System Engineer)

 

  b. Instrument System Engineer

 

  c. Project Engineer Quality Assurance (PEQA)

 

  d. Program Integration and Test management

[**Redacted**] BATC shall appoint a different individual to be a single point of contact for each of the following:

 

  e. Various Bus Subsystem Lead Engineers

 

  f. Launch Vehicle Integration Engineer

 

  g. Program Contract Management

These individuals are key personnel and, if performing well, should remain unchanged for the duration of the program.

BATC shall appoint a Satellite Simulator Project Lead. This individual will be the technical lead for the Satellite Simulator development effort and will be responsible for meeting its technical and schedule guidelines established herein.

 

4.3 DigitalGlobe Management

DigitalGlobe will appoint a Program Manager who as an individual shall act as DigitalGlobe’s primary point of contact on all program management matters. As required, according to the activity and phase of the contract, the Program Manager will nominate specific individuals to interface directly with BATC.

The DigitalGlobe Program Manager shall coordinate changes to contract conditions, price, timescale, deliverables, services or performance levels, unless a specific alternate has been appointed to deal with any of these matters. All changes to the contract documents shall require the written agreement of the DigitalGlobe contracts representative.

 

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DigitalGlobe will also appoint a responsible individual(s) to be a single point of contact for each of the following.

[**Redacted**]

BATC shall permit direct engineering interactions between these DG individuals and their BATC counterparts.

 

4.4 Space Segment Master Program Schedule (MPS) (CDIL PM-2)

BATC shall develop maintain, and provide a Master Program Schedule (MPS) for the entire program including hardware, software, analyses, data item deliverables, and subcontractor activities for all phases of the program including design, integration, test, and shipment through final acceptance.

 

4.4.1 General

The MPS shall consist of a computer supported dependency network, each element of which shall represent a single program event. Each event shall be attributed a start and finish date. The network must clearly show the interdependency in terms of both time and function amongst the events.

The MPS shall be the major management tool for planning, monitoring and controlling the program, in terms of:

 

  a. Planning the program, monitoring progress, documenting actual activity accomplishment and actual durations.

 

  b. Predicting future progress.

 

  c. Identification of significant milestones e.g. review meeting.

 

  d. Identification of the time critical path.

 

  e. Reflecting actual progress and changes relative to baseline plan.

 

4.4.2 Required Software

The Contractor shall create and maintain the network using Microsoft Project (Version 2003). Schedules of a detailed nature shall be provided electronically on a monthly basis. A hardcopy shall also be provided on request.

 

4.4.3 MPS Construction

Content

The network shall be constructed against the following major classifications:

 

  a. Deliverable hardware down to component level

 

  b. Software development activities

 

  c. Facilities required to support the production of any of the deliverables

 

  d. Other events/items required to support the production of the deliverables or services. e.g. test aids, test software prototypes, etc.

 

  e. Customer Furnished Equipment required from DigitalGlobe

 

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Individual items in each class shall be considered to consist of a number of generic events. These events shall typically consist of such activities as:

 

  a. Plan

 

  b. Design & develop

 

  c. Manufacture

 

  d. Assemble

 

  e. Integrate

 

  f. Test

 

  g. Deliver

 

  h. Reviews

However steps may be omitted or added given unit specific circumstances.

Unique Identifiers

The MPS shall include a unique identifying number for each task. This will more easily allow DigitalGlobe to combine certain tasks into a DigitalGlobe Master Schedule. Unique identifiers will not be deleted, reused, or re-assigned to other tasks.

 

4.4.4 Reports

The MPS shall be capable of generating a number of different types of reports upon demand. All events and milestones shall be coded to permit a variety of sort options to be exercised without program modification. Both GANTT and network form shall be supported.

 

4.5 Meetings & Reviews

BATC shall support the meetings and reviews listed in the following paragraphs.

 

4.5.1 Weekly Status Meeting

BATC Program Manager shall support a weekly meeting/telecon with the DigitalGlobe Program Manager to review program status including schedule, technical, risk register, action item list, and subcontracts.

 

4.5.2 Monthly Program Status Review

BATC Program Manager shall support a monthly Program Status Review with DigitalGlobe.

 

4.5.3 Program Reviews

List of Formal Reviews

BATC will host and conduct formal reviews at the following program milestones. BATC shall prepare charts, viewgraphs, analysis results, trade study results, etc. in the quantity and quality typical of aerospace industries reviews.

 

  a. Satellite Requirements Review (SRR) (CDIL D-34) ) Only changes between WV2 and WV3 must be reviewed.

 

  b. Delta - Preliminary Design Review (PDR) (CDIL D-30) Only changes between WV2 and WV3 must be reviewed.

 

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  c. Delta-Critical Design Review (CDR) (CDIL D-31) Only changes between WV2 and WV3 must be reviewed.

 

  d. Spacecraft Bus Complete/Instrument Integration Readiness Review (IRR) (CDIL – PT-8)

 

  e. Satellite Environmental Testing Readiness Review (CDIL – PT-9)

 

  f. Satellite Pre-Ship Review (CDIL PT-10)

 

  g. Launch Readiness Review (CDIL LM-14)

 

  h. [**Redacted**]

 

4.5.3.2    Content of Reviews

 

  A. PDR and CDR: BATC shall conduct “delta” reviews. These reviews will document the design changes between WV2 and WV3. These design reviews (PDR and CDR) shall include information and documentation typical of aerospace industry reviews, such as:

 

  1. Satellite mechanical configuration including stowed and deployed views

 

  2. Satellite mechanical configuration including [**Redacted**]

 

  3. Satellite electrical/electronic design, including system block diagram and redundancy scheme

 

  4. Satellite software design

 

  5. Satellite Operating Modes

 

  6. Satellite Fault Detection and Safing

 

  7. Satellite Budgets and Margins

 

  A. Performance relative to specifications

 

  B. Mass

 

  C. Power

 

  D. Thermal

 

  E. Consumables

 

  F. Attitude control: stability, pointing and knowledge

 

  G. RF links

 

  H. Satellite resources: relays, telemetry stream, CPU throughput, processor memory

 

  I. MTF

 

  J. Reliability: Ps, critical items list, cycle-limited items, FMECA

 

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  B. Spacecraft Bus Complete/Instrument Integration Readiness Review: BATC shall host this review. The purpose is to ensure the readiness to begin Instrument integration. This review will cover information including:

 

  1. Instrument Integration procedure and hardware status

 

  2. Status of all Certification Logs for all Ball built hardware that will be integrated to the Bus. Ball shall provide rationale and recovery plan for all certification logs that are open, even though the hardware is complete and ready for integration.

 

  3. TAR and HAR status from the Bus Integration and Test phase

 

  4. Test Team Personnel status, certifications, and time-sharing with other programs

 

  5. Facility status

 

  6. Satellite configuration review

 

  7. Other issues that may impact the timely and successful completion of Instrument integration.

 

  8. The Spacecraft Bus shall be deemed complete and ready for Instrument integration when: [**Redacted**]

 

  C. Satellite Environmental Testing Readiness Review: BATC shall host this review. The purpose is to ensure the readiness to begin satellite level environmental testing which includes but is not limited to: TVAC, EMI/EMC, Vibration, Shock, and Acoustic. This review will cover information including:

[**Redacted**]

 

  D. Satellite Pre-Ship Review: BATC shall host this review. The purpose is to ensure the readiness to ship the satellite to the launch site. This review shall be held after completion of all significant testing and all post-test reviews. The purpose shall be to review the results of the entire Integration & Test program, and demonstrate compliance to the satellite specification., and provide for satellite preliminary acceptance.

The Pre-ship Review shall be deemed satisfactory and the satellite preliminary acceptance by DigitalGlobe complete when the:

[**Redacted**]

 

  E. Satellite Launch Readiness Review: BATC shall conduct a Satellite Launch Readiness Review (SLRR) on or about [**Redacted**] . (Note, the Launch Services Provider, Lockheed Martin/ULA also has a review called the Launch Readiness Review. However, that review encompasses the satellite, launch vehicle, weather, and range support.) This SOW paragraph is only concerned with the readiness to launch the satellite. BATC shall review the results of the launch site Integration & Test activities, review any updates to the Verification Matrix, and provide for satellite final acceptance.

 

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The SLRR shall be deemed satisfactory and the satellite final acceptance by DigitalGlobe complete when the:

[**Redacted**]

F. [**Redacted**]

 

4.5.4 Component/Subsystem Design Review Listing (CDIL PM-3)

BATC shall prepare a summary listing of all planned component (box level) and subsystem design reviews. This listing shall include BATC and vendor provided hardware, and BATC provided software including the satellite simulator and maneuver planner software. This listing shall define the meeting format and required attendance. BATC shall provide a minimum of 10 days advance notice to DigitalGlobe for the following major reviews:

 

  a. System/Subsystem & Component PDRs

 

  b. System/Subsystem & Component CDRs

DigitalGlobe attendance and participation, including support consultants, shall be allowed, but not required at all reviews. The review activity will not be repeated if DigitalGlobe fails to attend.

 

4.5.5 Component/Subsystem Test Readiness / Data Review Listing (CDIL PM-4)

BATC shall prepare a summary listing of all planned component (box level) and subsystem qualification and acceptance test reviews. This listing shall include BATC provided and vendor provided hardware, and BATC provided software. This listing shall define the meeting format and required attendance. BATC shall inform DigitalGlobe of upcoming reviews in a timely manner.

DigitalGlobe attendance and participation shall be allowed, but not required at all reviews. The review activity will not be repeated if DigitalGlobe fails to attend.

 

4.5.6 DigitalGlobe Meetings

DigitalGlobe will arrange separate contracts for the:

 

  a. Launch Vehicle Segment (LV)

 

  b. Instrument

 

  c. Launch and Mission insurance

A series of technical interchange and review meetings will be held with these contractors jointly and separately, as required. BATC shall provide representation at these meetings as needed to resolve interface issues.

In the case of the insurance (c), BATC will provide inputs to formal presentations and support meetings to be held at the DigitalGlobe facility. DigitalGlobe will be responsible for responses to action items using information made available or provided by BATC during the course of the program.

 

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4.6 Documentation Management

 

4.6.1 Access to Program Technical Data

DigitalGlobe will have access rights to all program technical data that BATC generates and Subcontractor data to which BATC has legal and contractual rights. Program technical data may include Engineering Reports, drawings, software source code, and other tools used in the development of the spacecraft and analysis of requirements.

 

4.6.2 Objective

BATC shall establish a control and monitoring process relating to all deliverable documentation and other technical and test data for the complete program. The program shall account for the following:

 

  a. Preparation, review, and formal release as required

 

  b. Changes

 

  c. Storage, backup, and retrieval

 

  d. Distribution

Note: BATC shall include the DigitalGlobe Satellite Integration and Test Point-of-Contact on the distribution list of all relevant WV3 Engineering Reports. (“Relevant” in this clause refers to all ERs containing design information, analyses, test data, etc that affect the performance and/or operations of the satellite. It does not include ERs that contain BATC proprietary cost data.)

 

  e. DigitalGlobe access to all BATC documentation prepared on the project

 

  f. Long term storage for the purpose of through-life product support

As a primary supporting management tool, BATC shall use a secure project server. All data items except memory intensive drawings, test data, production logs, and QA data shall be maintained electronically on the project server. The project shall use the Microsoft Office software suite for word processing, spreadsheets, presentations, and documentation databases.

 

4.6.3 Documentation Listing (CDIL PM-5)

BATC shall develop and maintain a Documentation Listing that identifies all deliverable reports, analyses, drawings, software items, etc., that are developed on the project. The Documentation Listing shall include a naming convention that uniquely identifies the documents for electronic access where applicable. The List shall also indicate spacecraft name, a short title/description of the document, subsystem affected, the latest revision number and date, planned completion date, and status information. The List shall indicate those WV1 and WV2 documents that are also applicable to WV3. Document updates are required to reflect content changes. Document updates are not required if the sole purpose is to reflect applicability to WV3.

 

4.6.4 Documentation Delivery

The Contractor shall deliver document in native formats, e.g. Microsoft Word, Excel, etc., as opposed to PDF except as noted below. DigitalGlobe will identify the delivery location, such as a Microsoft Office Sharepoint Server (MOSS) internet site, and provide Contractor with username and password-controlled access. Documents shall be submitted or made available to DigitalGlobe according to the dates indicated in the list provided in Attachment 1.

 

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In the case of deliverables generated in Microsoft Office, such as Word, Excel, PowerPoint, etc; BATC shall populate the document property fields with the following minimum information: Title, Subject, Author, and key words.

In the case of deliverables that are not generated in MicroSoft Office, such as BATC drawings, .pdf is acceptable and BATC shall populate the property fields of drawings after they are converted to .pdf format.

 

4.7 Action Item Tracking (CDIL PM-6)

BATC shall maintain an Action Item List indicating all significant action items, including those of BATC as well as those of other organizations that relate to interactions with BATC. The Action Item List will be developed and maintained in a format that allows sorting by subsystem, originating party, receiving party, originating date, and closing date. BATC shall be responsible for ensuring closure of those items relating to BATC interactions and interfaces.

 

4.8 Financial Management

BATC shall define a standard set of formats for reporting program financial payment and billing status and shall submit them on a monthly basis. This shall consist of the following:

 

4.8.1 Historical Record of Payments (CDIL PM-7)

This shall consist of a record of the individual payments made, updated on a monthly basis. This record shall be cross-referenced to the payment schedule incorporated in the contract. Payments made in support of contract amendments shall be separately reported and cross-referenced to the payment schedule incorporated in the amendment.

 

4.8.2 Payments Forecast (CDIL PM-7)

This shall consist of a forecast of the future invoices and shall be cross-referenced to the payment schedule incorporated in the contract. Payment milestone forecasts shall be consistent with program progress reported on the Master Program Schedule. NOTE: Record of Payments and Payment Forecast are delivered as a single CDIL item.

 

4.9 Contract Change Control

These are considered to be of three types only:

 

  a. Contract Amendments

 

  b. Waivers: A written authorization granted after contract award to accept an item, that during production, or after having been submitted for inspection or acceptance, is found to depart from contract or specified configuration requirements. Waivers are intended only as one-time departures from an established configuration for specified items or lots and are not intended to be repeatedly used in place of formal engineering changes.

 

  c. Deviations: A written authorization, granted after contract award and prior to the manufacture of the item, to depart from a particular performance or design requirement of a contract, specification, or referenced document, for a specific number of units or a specified period of time. Deviations are intended only as one-time departures from an established configuration for specified items or lots and are not intended to be repeatedly used in place of formal engineering changes.

 

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BATC shall devise a system to control, monitor, and notify DigitalGlobe of these changes. The control system shall include provision for:

 

  a. A unique numbering scheme to track the changes through to completion.

 

  b. Impact upon contract obligation: - price, performance and delivery schedule, with specific identification of the item(s) of hardware, software or documentation affected.

 

  c. Notification of timescale for acceptance or rejection for each change, typically 10 business days.

 

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5.0 DESIGN

 

5.1 General

BATC shall perform the necessary trade studies, preliminary design, and detailed design of the Satellite, exclusive of the Customer Furnished Equipment as defined in Section 10, in accordance with the applicable documents. BATC shall design and procure the Ground Support Equipment necessary to support Satellite Integration and Test activities, except for items defined in Section 10.0. Design activities shall be featured in the program master schedule.

 

5.2 Working Groups and Trade Studies

 

5.2.1 Working Groups

[**Redacted**]

 

5.2.2 Trade Studies

 

5.3 [**Redacted**]Satellite Design Data

The satellite shall be designed such that the environmental design criteria of the Instrument as defined in the documents of paragraph 2.2 are not exceeded, and the structural, electrical, and thermal characteristics, as defined in the documents of paragraph 2.2, of the Instrument are accommodated.

DigitalGlobe shall provide information required to update the budgets for the Customer Furnished Equipment, consistent with paragraph 2.2.

 

5.3.1 Satellite to Instrument Interface Control Document(s) (CDIL D-1)

BATC shall produce and maintain the Satellite to Instrument ICD(s). The ICD(s) will address all interface issues including but not limited to: power, commanding, telemetry, mass and mass properties, mechanical envelope and mounting, thermal, fields-of-view, vibration and jitter isolation/management, and accommodation of bus components on the Instrument.

 

5.3.2 Satellite to Ground Terminal Narrowband Link ICD (CDIL D-2)

BATC shall produce and maintain the Satellite to Ground Station Narrowband Link ICD. This link will address both the command uplink and telemetry downlink.

 

5.3.3 Satellite to Ground Terminal Wideband Link ICD (CDIL D-3)

BATC shall produce and maintain the Satellite to Ground Terminal Wideband Link ICD.

 

5.3.4 Satellite Environmental Design and Test Specification (EDTS) (CDIL D-4)

BATC shall prepare and maintain the EDTS, or equivalent document defining the component environmental design and test requirements. Electromagnetic Interference Design and Testing shall be in accordance with the standards specified in Satellite Specification.

 

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5.3.5 Contamination Control Plan(s) (CDIL D-5)

[**Redacted**]

 

5.3.6 Satellite Level Requirements Verification/Compliance Matrix (CDIL D-6)

BATC shall produce a satellite level RVCM. The RVCM will include requirements from the Satellite Specification, [**Redacted**] and the Instrument Specification if applicable. BATC shall update/maintain the Satellite RVCM to reflect changes to these parent specifications. DigitalGlobe shall have review and approval authority over changes to the RVCM. BATC shall include the following information in the RVCM

 

  a. Source of requirement (Parent specification document and paragraph number, i.e. satellite spec, instrument spec, etc)

 

  b. Specification paragraph

 

  c. Paragraph title

 

  d. Summary description of requirement

 

  e. Column indicating status of compliance

 

  f. Summary description of performance

 

  g. Responsible organization

 

  h. Verification Point [**Redacted**]

 

  i. Verification Method [**Redacted**]

 

  j. Verification Source Document indicating applicable paragraph, test sheet, etc.

 

  k. Comments, if required.

 

  l. Other information at BATC’s option

 

5.3.7 Box Level Requirements Verification/Compliance Matrix (CDIL D-7)

BATC shall flow down requirements from the Satellite Specification to box level requirements. BATC shall develop performance requirements for each box level component on the Satellite excluding CFE. For this paragraph, “box level component” also includes all components that are not really “box” like. These include but may not be limited to:

[**Redacted**]

BATC shall use the Box Level RVCM as an input into the box level performance test procedures. BATC shall demonstrate compliance to the box level RVCM.

 

5.3.8 Drawings (CDIL D-8)

A complete file of BATC drawings prepared for the WV3 program, will be maintained on file in electronic and hardcopy form, where appropriate. Electronic transfer to DigitalGlobe will constitute delivery.

 

5.3.9 Performance Compliance and Risk Management

5.3.9.1    Performance Compliance (CDIL D-9)

The contractor shall supply at PDR a Performance Compliance Matrix identifying the performance estimate, allocated uncertainty (and/or contingency as appropriate) and resulting Total Performance (where Total Performance = performance estimate + uncertainty) for the following list. The Performance Compliance Matrix shall be updated and provided with each Quarterly Review following the PDR. [**Redacted**]

 

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[**Redacted**]

DigitalGlobe shall provide performance information required to update the budgets for any of the Customer Furnished Equipment, in accordance with the documents in Paragraph 2.2.

5.3.9.2    Risk Management Report (CDIL D-10)

BATC and DigitalGlobe shall jointly develop and maintain a Risk Status Report. This report highlights known program risks, assigns risk levels, and documents mitigation strategies and status. BATC shall supply at PDR an initial Risk Status Report covering the system elements to be provided by this SOW. BATC shall updated the Risk Status Report monthly following the PDR.

5.3.10    Subsystem Description Documents (CDIL D-11)

BATC shall prepare Subsystem Description Documents for each satellite subsystem.

The Subsystem Description Documents will include as a minimum, unless provided in other deliverable documents, and referenced in the SDD:

 

a. Subsystem Overview including a detailed block diagram

 

b. Functionality and major performance characteristics of each Subsystem Component

 

c. Redundancy

[**Redacted**]

 

d. [**Redacted**]

 

e. [**Redacted**]

 

f. [**Redacted**]

 

g. Subsystem schematic including power, power returns, commands, and telemetry. This schematic shall be updated to reflect Engineering Change Orders.

 

h. Expected nominal operating methods and telemetry limits

[**Redacted**]

 

i. Operational constraints

[**Redacted**]

 

j. Fault Protection

[**Redacted**]

j.2 List the information available to the operator to reconstruct or identity the fault.

 

k. Interfaces between subsystem components

 

l. Major interfaces with other subsystems

The Subsystem Description Documents shall be delivered at CDR + 4 months. If changes require an update to the document, those updates shall be provided at approximately Launch – 4 months and again at Launch + 4 months. The subsystem schematic (item e.) shall be updated as required throughout the program to reflect Engineering Change Orders.

5.3.11    Analysis and reports

BATC shall perform the following analyses. Updates shall be provided when changes significantly invalidate previous results.

 

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  a. (1) Integrated Spacecraft Bus/Instrument thermal analyses, including summary of temperature predictions for unit level components under various operational modes and (2) unit-level thermal analysis [**Redacted**] . (CDIL D-12)

 

  b. Integrated Spacecraft Bus/Instrument structural analysis including [**Redacted**] . (CDIL D-13)

 

  c. Control system analysis including [**Redacted**]. (CDIL D-14)

 

  d. System Level Failure Modes and Effects and Criticality Analysis (FMECA). [**Redacted**] (CDIL D-15)

 

  e. Satellite Reliability Analysis BATC shall calculate satellite reliability using its standard process. [**Redacted**] (CDIL D-16)

 

  f. Satellite Life Prediction Data. DigitalGlobe needs to continually assess expected satellite life based upon actual on-orbit operational parameters. BATC shall provide all backup data used by BATC for sizing and life predictions. BATC does not need to produce a life expectancy analysis. DigitalGlobe will use the provided data and make our own Life Prediction. BATC can provide the life prediction data in one summary package, or in other CDILs.

 

  g. Flight Battery Life Prediction Analysis. BATC shall produce a life expectancy analysis for the satellite battery. The battery life prediction shall account for ground handling and will include a family of curves based upon pertinent on-orbit variables including but not necessarily limited to temperature and depth-of-discharge. (CDIL D-35)

 

  h. Satellite Imaging Performance (CDIL D-17)

BATC shall perform a comprehensive analysis regarding imaging performance. This is a comprehensive look at the numerous subsystem and trans-subsystem performance measures that affect imaging. The list includes but is not limited to:

[**Redacted**]

 

  i. [**Redacted**]

5.3.12    Other Interface Control Documents

BATC shall provide inputs, review, and verify BATC side of the following ICDs.

 

  a. Satellite to Launch Vehicle ICD

In the event the ICDs require revision, the changes will be discussed between the affected parties to determine the most cost and schedule efficient manner to implement the change. If applicable, any impact will be covered under changes provision of the Contract.

5.3.13    Critical Items list (CDIL D-18)

BATC shall maintain a Critical Items List summarizing all known single point failures on the Satellite and any special efforts required to mitigate risk associated with them. It shall also contain any items requiring special handling due to a high potential of damage, mission criticality, or safety concerns.

 

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5.3.14    Component Heritage Summary (CDIL D-19)

The Component Heritage Summary will consist of a listing of all Satellite units by subsystem summarizing:

 

  a. Unit name

 

  b. Development / qualification history (e.g. engineering model, qual, protoflight)

 

  c. Previous flight heritage

 

  d. Modifications to previous uses

 

  e. Any significant known anomalies on flight units

5.3.15    Engineering Reports (CDIL D-20)

A complete file of all relevant Engineering Reports prepared on the WV3 program funding shall be maintained on file in electronic and hardcopy form where appropriate. Electronic transfer to DigitalGlobe will constitute delivery and shall occur within 5 business days of the ER release date. ERs delivered as a separate CDIL do not need to be delivered twice – once per this paragraph and again per the relevant CDIL paragraph. Those ERs need only be delivered once per the relevant CDIL paragraph.

(“Relevant” in this clause refers to all ERs containing design information, analyses, test data, etc that affect the performance and/or operations of the satellite. It does not include ERs that contain BATC proprietary cost data.)

5.3.16    Flight Software Source Code (CDIL D-21)

Per the terms of the software license agreement set forth in the Agreement, BATC shall grant to DigitalGlobe a limited license to use the flight software code. A copy of the flight software code, as identified below, shall be provided to DigitalGlobe on suitable media. Other elements of the software, as identified below, shall be placed in escrow per the Agreement.

[**Redacted**]

For units that are subcontracted by BATC, software and firmware shall be delivered if delivered to BATC and BATC has the right to deliver it to DigitalGlobe.

5.3.17    Composite Grounding Design (CDIL D-22)

[**Redacted**]

5.3.18    Structural, Power, Thermal, and Reliability Analytical Models (CDIL D-23)

BATC shall provide the analytical models used to predict the integrated spacecraft and instrument Structural [**Redacted**] , Power, and Thermal performance.

Satellite thermal performance modeling shall use the instrument thermal model provided by ITT. BATC shall use the integrated Satellite model to:

 

  a. Verify thermal interface requirements documented in the Spacecraft Bus to Instrument ICD are being met. Although BATC shall not be held contractually responsible for non-compliances on the ITT side of the interfaces, any such non-compliances revealed by Satellite thermal modeling shall be reported to DigitalGlobe.

 

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  b. Verify the Bus meets all of its requirements when modeled as a complete Satellite, for example unit temperatures and line of sight stability. BATC shall deliver line of sight motion vs. time profiles to DigitalGlobe (for incorporation into system geolocation budgets).

 

  c. Develop predicted temperature vs. time profiles of key instrument nodes as coordinated with ITT through the established ICD process. BATC shall deliver these temperature profiles to DigitalGlobe and forward a copy to ITT (so that ITT can verify the instrument meets its requirements).

BATC shall also provide the spacecraft bus reliability model down to the component and/or card level. Electronic transfer to DigitalGlobe will constitute delivery.

5.3.19    Coordinate Transformation Document (CDIL D-24)

BATC shall provide the documentation of all coordinate reference frames used in the satellite system including their reference points within the spacecraft. Nominal values for all transformations shall be provided. Reference frames requiring on-orbit calibration shall be noted. The document shall be updated with best-estimates from pre-launch calibrations and measurements.

5.3.20     Flight Software Users Manual (CDIL D-25)

BATC shall provide documentation of the flight software to include flowchart of routines/modules, structure and calling sequences, commands, telemetry, database constants and uploadable parameters, address tables, and log file definitions and locations.

5.3.21     Component Acceptance Data Package (CDIL D-26)

BATC shall provide or make available data acceptance packages for all major components.

5.3.22     [**Redacted**]

[**Redacted**]

5.3.23    Instrument/Sensor Boresight Stability Data (CDIL D-28)

[**Redacted**]

5.3.24     Position and Attitude Accuracy (CDIL D-29)

BATC shall provide detailed analysis and test data showing compliance with position and attitude accuracy requirements.

5.3.25    Satellite to MGB Interface Control Document(s) (CDIL D-32)

BATC shall produce and maintain the Satellite to MGB ICD(s). The ICD will address all interface issues including but not limited to: power, commanding, telemetry, mass and mass properties, mechanical envelope and mounting, thermal, fields-of-view, vibration and jitter isolation/management.

 

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5.3.26    DigitalGlobe to BATC Electrical GSE Interface Control Document (CDIL D-33)

BATC shall produce and maintain an ICD for the STOC-to-NarrowBand Rack interface. This includes but is not limited to: grounding, commanding, telemetry, data formats, etc.

 

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6.0 PRODUCT ASSURANCE

 

6.1 Product Assurance Plan

The Contractor and its subcontractors shall have an established quality control system that meets the requirements of BATC’s Product Assurance Plan and BATC’s Supplier Product Assurance Plan

 

6.2 BATC Parts Control Board (PCB)

The Parts Control Board (PCB) shall be constructed as follows: A PCB will be established. The responsibility of this PCB is to ensure each EEE part was evaluated for performance relative to the requirements. With the exception of System Safety, the PCB will also be used as the forum to discuss other Systems Assurance/Product Assurance issues i.e., Materials and Processes, Reliability, etc. The PCB is responsible for the review and disposition of any noncompliance with BATC’s Product Assurance Plan.

The PCB consists of:

 

  a. BATC Product Assurance Manager (Chairman)

 

  b. BATC WV3 Product Assurance Specialist or designated alternate

 

  c. Designated technical specialist from the hardware/software product team as needed

 

  d. Other necessary disciplines as needed

 

  e. DigitalGlobe Designated Representative(s). (The DigitalGlobe member is a non-voting adjunct member).

6.2.1 Subcontractor Parts Control Board (PCB)

Subcontractor PCBs shall be established as necessary to implement BATC’s supplied Product Assurance Plan. It is BATC’s responsibility to verify compliance.

6.2.2 PCB Process

Upon identification of a need for a PCB, BATC shall document relevant information in a System Engineering Report (SER) and obtain approval (signatures) from the PCB members. DigtalGlobe shall have PCB approval authority or waiver authority for non-compliances listed in the Specification Addendum, otherwise BATC shall notify DigitalGlobe. The SER shall be released to DigitalGlobe under CDIL D-20 within 5 working days of PCB approval. Any PCB discussions prior to release of the SER may be informal and in most cases shall be delivered to DigitalGlobe electronically via e-mail.

Minimal BATC PCB approval/disposition signatures include BATC PAM and BATC WorldView Product Assurance Specialist or his designated alternate. Once the PCB approves a part, the Parts Engineer will indicate approval on the Advanced or Program Parts List (A/PPL).

 

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6.3 Parts and Materials

 

6.3.1 Electrical, Electronic, and Electro-mechanical Parts (EEE)Parts Listing (CDIL QA-1)

BATC shall prepare, maintain, and deliver a EEE Parts Listing for all satellite hardware except for Customer Furnished Equipment. This listing shall identify all EEE parts intended to be used by BATC and its vendors. For each part, the following minimum information shall be identified: manufacturer, description, lot date code. Parts shall be qualified as compared to BATC product assurance criteria and the Satellite Specification and the Satellite Specification Addendum. BATC’s internal process and format for EEE Parts Listing may be utilized.

The Parts List shall be maintained and reviewed by BATC as necessary, but minimally it shall be updated and provided to DigitalGlobe at the following:

 

  a. Prior to manufacturing for each box/component At this phase, it is acknowledged by DigitalGlobe and BATC that the list may be incomplete due to part shortages.

 

  b. Prior to box/component level Test Readiness Review

 

  c. Prior to the integration of any box/component onto the Bus.

 

6.3.2 Material and Processes Reports (CDIL QA-2)

BATC shall prepare and deliver reports documenting their approval of all materials and processes planned for use on the Bus.

 

6.4 As-Built Configuration and Conformance

6.2.1    6.4.1    As-Built Configured Article List (CDIL QA-3)

The as-built configured article status shall be maintained throughout the production program in the certification logs and production orders. At the conclusion of integration, the information shall be used to generate the preliminary As-built Configured Article List. After test and modification (if any) the List shall be finalized and presented.

6.2.2    6.4.2    Certificate of Conformance (CDIL QA-4)

A Certificate of Conformance shall be generated and signed off by Product Assurance and Program Management. It details the conformance (and exceptions) to the SOWs, specifications and other contractual documents for the delivered article. This Certificate of Conformance shall be delivered to DigitalGlobe at the Launch Readiness Review.

 

6.5 Product Assurance Reviews (CDIL QA-5)

The plan shall include a program for the periodic audit of portions of the Contractor’s Product Assurance System in each of the below activity areas to confirm conformance to the requirements. These audits will be conducted by the Program Product Assurance engineer. BATC shall inform DigitalGlobe of the audit results.

 

  a. Reliability

 

  b. Parts Procurement

 

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  c. Materials and Processes

 

  d. Non-Conforming Material Control

 

  e. Configuration Management

 

  f. Safety

 

6.6 Documentation

Documents shall be submitted or made available to DigitalGlobe as indicated in the list provided in Attachment 1.

 

6.7 Known Non-Compliant Hardware

[**Redacted**]

 

6.8 Military Standard 461

[**Redacted**]

 

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7.0 PROCUREMENT

 

7.1 General

BATC shall be responsible for the work associated with the procurement of all material and subcontracts required to provide the deliverable items, except for the CFE items identified in Section 10.0. BATC shall procure according to the CSO Supplier Product Assurance Plan. Procurement activities shall be featured in the program master schedule.

 

7.2 Make/Buy Plans (CDIL PT-1)

BATC shall identify Make/Buy plans for all Satellite components.

 

7.3 Encryption/Decryption Devices

[**Redacted**]

 

7.4 Reviews

A series of reviews shall be established with each subcontractor. A schedule of these reviews shall be included in the Review Listings required by paragraph 4.5.3. The reviews will generally be held at the vendor and DigitalGlobe personnel may attend, at their option.

 

7.5 Program Subcontract Status Report (PSSR) (CDIL PT-2)

BATC shall prepare a Program Subcontract Status Report (PSSR) for the program. The PSSR will contain critical status information on each major subcontract (larger than $1M) relative to:

 

   

Design & development

 

   

Procurement and Production

 

   

Assembly

 

   

Integration

 

   

Test, including any anomalies

 

   

Delivery schedule

 

   

Reviews

 

7.6 Documentation

Documents shall be submitted or made available to DigitalGlobe as indicated in the list provided in Attachment 1.

 

7.7 Subcontract Flow-downs

 

7.7.1 Assignment Clause

[**Redacted**]

 

7.7.2 Access

[**Redacted**]

 

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8.0 PRODUCTION ACTIVITIES

 

8.1 General

BATC shall appoint a Production engineer responsible for ensuring that BATC’s production capabilities match the requirements of the program. With the support of the Program QA engineer, he shall ensure that the production facilities comply with the Product Assurance requirements.

BATC shall be responsible for the work associated with the production of the deliverable items, except for the CFE items identified in Section 10.0. BATC shall be responsible for the production activities associated with integrating the CFE items as defined in Section 10.

Production activities shall be featured in the program master schedule.

 

8.2 Production Process

BATC shall produce the deliverable hardware according to applicable BATC standardized procedures. As a minimum, standardized BATC procedures shall be followed for the following topics:

[**Redacted**]

 

8.3 Access

The production manager shall arrange access for the DigitalGlobe staff to BATC manufacturing areas where manufacturing activities associated with the program are taking place.

 

8.4 Production Documentation

Production orders and Certification Logs shall document the as-built configuration. These logs shall be available on-site for DigitalGlobe review.

 

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9.0 INTEGRATION AND TEST ACTIVITIES

 

9.1 General

For the WV program the Integration and Test activities fall into four logical categories.

 

  a. Box level / Subsystem level testing

 

  b. Bus level integration and testing including integration of the instrument

 

  c. Satellite level testing

 

  d. Mission and Launch Rehearsals

The Integration and Test Manager shall be responsible to ensure that BATC’s integration and test capabilities match the requirements of the program

BATC shall accomplish the work associated with a-d above for all BATC supplied hardware/software. BATC shall accomplish the work associated with b-d above for all CFE.

 

9.2 Box/Subsystem Level Testing

 

9.2.1 General

BATC shall perform all box level testing per environmental design and test specification and the box level Requirements Verification and Compliance Matrix.

 

9.2.2 [**Redacted**]

[**Redacted**]

 

9.3 WV Bus and Satellite Integration and Test Plans (CDIL PT-3)

BATC shall develop a WV Bus and Satellite Integration and Test Plan (Satellite I&T Plan) for the WV3 satellite. The test plans will include all I&T activities starting from the installation of the first component on to the bus structure through launch.

The WV I&T Plan(s) shall:

[**Redacted 4 Pages**]

 

9.4 Post-Shipment Instrument Testing

ITT will perform post-shipment functional testing to verify the Instrument survived shipment without damage. ITT will provide the necessary test equipment for the Instrument.

BATC shall provide:

[**Redacted**]

For schedule purposes the Instrument is not considered delivered to BATC upon arrival at BATC facility. Rather the instrument is considered delivered on the date that the Instrument has completed all necessary post-shipment testing and is ready and available for BATC to integrate to the telescope/bus.

 

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9.5 Supporting Documents

BATC shall provide as a minimum the following support documents:

 

  a. All necessary box level test procedures, integration procedures, and system level test procedures. Each procedure shall include a detailed test description explaining the “what, how, and why” of each test.

 

  b. A System Level Test Matrix. The test matrix will identify which System Level Test procedures or portions of those procedures will be accomplished at each test phase. The System Level Test phases include, but are not limited to:

[**Redacted**]

 

9.6 System Test Reports (CDIL PT-5)

[**Redacted**]

 

9.6.1 Content

The report shall include a summary of satellite configuration, test objectives, test results, significant hardware/software anomalies if any, resolution of significant anomalies, and a copy of all telemetry plots or other post-test data. The cognizant test engineer and the appropriate subsystem engineer(s) shall sign the report.

 

9.6.2 Timeliness

BATC shall publish the test reports No Later Than 15 working days after test completion.

 

9.7 Uninterruptible Power Supply (UPS)

[**Redacted**]

 

9.8 DigitalGlobe Integration and Test Engineering Access

 

9.8.1 On-Site and Visiting Engineers

BATC shall provide dedicated cubicle space, furniture, high-speed internet access, and phone lines for three resident DigitalGlobe I&T engineers. These DG on-site engineers will serve as the I&T focal point between DG and BATC. It is anticipated these engineers will be on-site at BATC on a full-time basis. BATC shall provide dedicated cubicle space, furniture, high-speed internet access, and phone lines for one visiting DigitalGlobe engineer.

 

9.8.2 Access to Live Satellite Telemetry

Once power-on bus integration begins, BATC shall provide DG with access to the live satellite telemetry from the cleanroom. DG will provide the necessary hardware to connect the Mission Control Center (MCC) to BATC GSE. DG will man and operate the DG hardware as necessary to flow the telemetry to the MCC. DigitalGlobe access to telemetry will occur on a non-interference basis to BATC test team.

 

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9.8.3 Test Observation By Other DG Engineers

BATC shall allow other DG satellite and ground system engineers access to the cleanroom to witness satellite testing. BATC is not obligated to coordinate, inform, or schedule testing according to DG engineer availability.

 

9.8.4 Access to Command and Telemetry Log Files (CDIL PT-6)

BATC shall deliver an archive of all command and telemetry files from satellite integration and test in an electronic format. BATC shall deliver an update weekly. Electronic transfer to the DG server shall constitute delivery. BATC shall maintain information about which command and telemetry database was used in delivered files as well as which test procedures were run in each file.

 

9.9 Test Reviews

The status of the Satellite shall be reviewed during the test phases of the program. See paragraph 4.5.3.2 for the list of reviews and required content.

 

9.10 Optional Testing

The following is a list of optional tests to be performed or supported by BATC. These are tests DigitalGlobe may choose to have BATC perform if the schedule permits. BATC should not show these tests in the baseline schedule. In each case after a test option is exercised by DigitalGlobe, BATC has 30 calendar days to prepare for the test. BATC shall provide a separate option price prior to the start of I&T for each of these tests.

[**Redacted**]

 

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10.0 CUSTOMER FURNISHED EQUIPMENT AND SERVICES

 

10.1 General

DigitalGlobe has contracts with vendors other than BATC who are responsible for providing portions of the overall system. DigitalGlobe has the responsibility for monitoring, administering, and verifying performance of those subcontracts. This section defines the items and support requirements that DigitalGlobe is responsible for securing and providing to BATC via these other subcontractors. This section also defines the equipment that DigitalGlobe is responsible for providing directly.

The delivery of all items shall be per Attachment 2: Customer Furnished Equipment list. DigitalGlobe will also arrange for the return of loaned equipment, if required, at no cost to BATC. CFE items shall be featured in the program master schedule. Unless otherwise explicitly provided to the contrary in Attachment 2, title to all equipment identified in this Section 10.0 shall remain in DigitalGlobe.

 

10.2 Flight Equipment

[**Redacted**]

10.2.1    [**Redacted**]

[**Redacted**]

10.2.2    [**Redacted**]

[**Redacted**]

10.2.3    [**Redacted**]

[**Redacted**]

10.2.4    [**Redacted**]

[**Redacted**]

10.2.5    [**Redacted**]

[**Redacted**]

10.2.6    [**Redacted**]

[**Redacted**]

10.3    Simulators (CSIM-1)

[**Redacted**]

 

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10.4 Launch Vehicle Interfaces

 

10.4.1     Launch Vehicle Interface

DigitalGlobe shall provide a launch vehicle interface adapter to BATC (CLSE-1). BATC shall use this for a fit check and for a separation test as described in paragraph 9.3.e. DigitalGlobe shall provide a match drill template to BATC (CLSE-2).

10.4.2    Launch Vehicle Separation Connectors (CLSE-3)

DigitalGlobe shall provide the flight satellite/launch vehicle separation connectors.

 

10.5 Ground Support Equipment

10.5.1    Wideband Link RGT Equipment

DigitalGlobe will provide a set of RGT ground equipment for capturing Instrument data in the cleanroom. Nominally, this will include the following equipment and documentation:

[**Redacted**]

10.5.2    Narrowband Link RGT Equipment (CGSE-5)

DigitalGlobe will provide a set of RGT ground equipment for processing the S-band uplink and X-band narrowband downlink in the cleanroom. The capability to bypass the RF sections and operate at a baseband Satellite interface shall be provided by BATC . This may include elements of the Mission Control Center [**Redacted**] as dictated by the architecture of the ground system. DigitalGlobe shall deliver to BATC operating documentation and interface details one month prior to delivery.

This equipment shall include: [**Redacted**]

10.5.3    Special Test Equipment

DigitalGlobe shall provide special WB Link / WB receiver test equipment for WB link development and testing. This will include:

[**Redacted**]

10.5.4    Mission Control Center (CGSE-11)

DigitalGlobe will provide portions of the Mission Control Center (MCC) and software as required to support the Satellite Integration and Test Plan, via data links between the MCC in Longmont, CO and BATC. BATC shall be responsible for work on the Satellite required to resolve problems associated with the Satellite performance and function. All work associated with resolution of DigitalGlobe provided ground equipment and interfaces shall be at DigitalGlobe expense.

10.5.5    [**Redacted**]

[**Redacted**]

 

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10.5.6    [**Redacted**]

[**Redacted**]

10.5.7    [**Redacted**]

[**Redacted**]

10.5.8    MGB Test Equipment (CGSE-15)

DigitalGlobe shall provide a signal generator, up-converter, feedhorn, and control computer.

10.5.9    [**Redacted**] (CGSE – 16)

[**Redacted**]

 

10.6 Launch Vehicle Data (CLD-1 and CLD-2)

DigitalGlobe shall provide a preliminary and final Coupled Loads Analysis (CLA) to BATC from the Launch Services contractor.

 

10.7 Instrument Data

DigitalGlobe shall provide the WV3 instrument data and models, as specified in Paragraph 2.2, to support satellite level analysis and modeling for the areas listed below. BATC shall be responsible for additional data to support the provisions of this document and the spacecraft specification.

10.7.1    Instrument Structural Analysis Data (CID-1)

DigitalGlobe shall provide the WV3 instrument structural data and model.

10.7.2    Instrument Thermal Analysis Data (CID-2)

DigitalGlobe shall provide WV3 instrument thermal data and model.

 

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11.0 STORAGE AND DELIVERY

 

11.1 General

BATC shall be responsible for storage, if required, and delivery of the WV3 Satellite in accordance with the following paragraphs.

 

11.2 Satellite Pre-Shipment Storage

In the event that the Satellite is completed prior to the contractually scheduled delivery date, BATC shall provide, at their cost, suitable environmentally controlled storage including temperature and humidity monitoring and recording.

If shipment is delayed due to BATC beyond the contractually scheduled delivery date and the Satellite is complete, and such delay by BATC has caused a loss of available launch opportunity, the Satellite shall be placed in storage at BATC’s expense.

If shipment is delayed due to DigitalGlobe beyond the contractually scheduled delivery date and the Satellite is complete, the Satellite shall be placed in storage at DigitalGlobe’s expense.

 

11.3 Pre-Shipment Re-Test

Subject to the length of the storage period, appropriate maintenance and power up of those units sensitive to inactivity shall be undertaken. Any items exhibiting signs of deterioration shall be subject to appropriate follow up action according to the circumstances. All instances shall be reported to DigitalGlobe.

A thorough re-test is required should the storage exceed [**Redacted**] . Details shall be provided in the test requirements document. Appropriate follow up action shall be taken, according to the circumstances, should any problems be detected.

The re-test costs shall be at BATC expense if delay and retest were caused by BATC. The re-test costs shall be at DigitalGlobe’s expense if delay and retest were caused by DigitalGlobe.

 

11.4 Satellite Shipping and Delivery

[**Redacted**]

BATC shall provide shipping from BATC plant to the launch site. BATC shall pack the Satellite and ground support equipment in suitable containers for shipment to the launch site. BATC shall unpack the Satellite and ground support equipment at the payload processing facility at the launch site.

BATC shall provide insurance and security for the satellite and ground support equipment during shipment to the launch site.

BATC shall pack the ground support equipment for return to BATC plant and provide shipping.

BATC shall provide insurance for the ground support equipment during shipment back to BATC plant.

 

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The transportation environment shall be enveloped by the requirements in the Launch Vehicle and Instrument ICD and performance specification. BATC shall be responsible for ensuring the Satellite compatibility with the requirements. BATC shall be responsible for verifying all environmental requirements are met including temperature, humidity, and shock monitoring.

 

11.5 Satellite Launch Site Storage

BATC shall provide volumetric storage and access requirements to DigitalGlobe for shipping containers required at the launch site. The baseline program assumes no Satellite storage requirements at the launch site. However, if the launch should be delayed once the Satellite has been shipped, BATC shall provide, at DigitalGlobe expense, the support necessary to maintain, store, and retest the Satellite.

 

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12.0 LAUNCH SUPPORT SERVICES

BATC shall provide launch support services as defined in the following paragraphs.

 

12.1 General

[**Redacted**] DigitalGlobe will be responsible for overall coordination of launch activities. BATC shall support this activity as defined in this section of the SOW.

The Satellite shall be compatible with U.S. launch safety requirements. BATC shall generate a WV3 Missile System Pre-launch Safety Package (MSPSP) (CDIL LM-1) to document hazardous items or operations and planned safety procedures for the Satellite.

BATC shall support the safety review processes of the Launch Services Contractor and the Launch site.

 

12.2 Requirement Definition

BATC shall support the generation and maintenance of the Launch Vehicle ICD as defined in paragraph 5.3.12. BATC shall supply the following information and any other information normally required by the Atlas V Launch Services User’s Guide to DigitalGlobe and the Launch Services contractor:

 

  a. Launch vehicle interface details and requirements.

 

  b. Requirements for launch site support and services including space, power, environment, contamination control, lifting/moving, telecommunications, etc.

 

  c. Statement of compliance with launch site safety requirements.

 

  d. Environmental requirements pre and post installation on launch vehicle.

 

  e. Verification of applicable portions of the Satellite to Launch Vehicle ICD.

 

  f. Launch Site Procedures.

BATC shall, by means of drawings, analysis, or test, be responsible for specifically confirming Satellite compatibility with the launch vehicle requirements defined in the ICD. BATC shall prepare a RVCM, as defined in paragraph 5.3.6, for those portions of the ICD for which it has responsibility.

 

12.3 Technical Interchange Meetings

BATC shall support up to twenty Technical Interchange Meetings (TIM) with the launch organization . [**Redacted**] In addition, BATC will support informal meetings and teleconferences at DigitalGlobe’s Colorado facilities and BATC facility as required resolving interface and infrastructure issues.

 

12.4 FEM and CLA-to-Design Load Comparisons (CDIL LM-2)

BATC shall provide preliminary Finite Element Models (FEM) and final FEMs for the WV3 Satellite for the purposes of performing coupled loads analyses. DigitalGlobe is responsible for obtaining valid CLA results from the launch service contractor and delivering those to BATC. BATC shall then compare the results of the coupled loads analyses to the design loads used in spacecraft bus and Instrument structural analysis to confirm that the resulting loads are within the design requirements as specified in the respective ICDs. The deliverables are as follows:

[**Redacted**]

 

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12.5 Export Regulations

All contractors on this program are anticipated to be U.S. companies including the launch service contractor. Therefore we anticipate no exports of hardware, software, or technology to foreign companies. However, if that situation changes, DigitalGlobe shall be the single point of contact for all export issues. Therefore:

BATC shall provide information directly to DigitalGlobe and DigitalGlobe will be responsible for obtaining and documenting all export approvals for all documentation transmitted to the launch vehicle agencies.

DigitalGlobe will be responsible for all work associated with compliance to export regulations including licensing, security, customs, document approval, transportation, etc. for documents/data channeled through DigitalGlobe.

It is understood that the Department of State International Traffic in Arms regulations (CFR 22 Part 120 through 130) strictly apply to any data or hardware covered under this SOW.

 

12.6 Adapter Fit-Check

BATC shall perform a launch vehicle interface check on the satellite as defined in the Test Plan. DigitalGlobe will arrange for the launch services contractor to provide the adapter, interface portions of the separation system, and GSE. If required, DigitalGlobe will also arrange for support from the launch services contractor at no cost to BATC.

 

12.7 Launch Site Infrastructure

DigitalGlobe shall arrange for and provide all launch site infrastructure necessary for satellite testing and pre-launch processing. This includes lease of a satellite processing facility.

 

12.8 Launch Site Operations

BATC shall support the launch operations campaign including provision of the test equipment and labor required to perform the launch site unpacking, Satellite checkout as defined by the WV I&T Plan, fueling, final mating to launch vehicle, launch, and repacking for return to BATC plant. Delays associated with BATC performance shall be at BATC expense. Any other delays shall be at DigitalGlobe expense. BATC will be responsible to support meetings for the purpose of coordinating launch site operations including joint operations with the launch services contractor. All efforts associated with reprocessing due to a cancelled or aborted launch shall be at DigitalGlobe expense.

 

12.9 Fueling

BATC shall prepare a fueling plan and the procedures required for fueling the Satellite using an appropriate fueling cart. BATC shall prepare the fueling equipment for hydrazine loading

 

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operations and package for shipment to the launch site. BATC shall be responsible for a single fuel loading operation unless multiple fuelings are required due to reasons under BATC’s control.

BATC shall provide all required consumables, propellant, safety training, and safety equipment including SCAPE gear required to effectively and safely perform satellite fueling operations. DigitalGlobe shall arrange for disposal of all hazardous wastes and any excess materials through its Launch Services provider.

BATC shall provide support to the launch vehicle/range contractor as required to respond to range specific requirements as they pertain to the handling of the hydrazine operations.

 

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13.0 MISSION PREPARATION AND ON-ORBIT COMMISSIONING

BATC shall assist with Mission preparation and On-orbit Commissioning by performing the following tasks and engineering services.

 

13.1 Training (CDIL LM-3)

 

13.1.1 Training Materials

BATC shall develop a training package for each satellite subsystem including the operation of the Instrument to address specifically the changes between WV-2 and WV3. The training package will be based on the Subsystem Description Documents (Paragraph 5.3.10) and include the same minimum information.

The training packages will be delivered on both paper and electronic media.

 

13.1.2 Training Sessions

For each subsystem, a cognizant BATC subsystem engineer shall present the training materials from paragraph 13.1.1. DigitalGlobe will provide the conference room and necessary projectors to support the presentation. DigitalGlobe reserves the right to videotape the training sessions for the purpose of training future DigitalGlobe personnel.

 

13.2 Command and Telemetry Handbook (CDIL LM-4)

BATC shall prepare a command and telemetry handbook. This document shall provide a definitive listing of all satellite telemetry and commands with a full description for each. The handbook shall meet the requirements identified in WV159.

 

13.3 Bus Subsystem Calibration Tools (CDIL LM-5)

BATC shall provide the subsystem calibration tools necessary for on-orbit calibration activities. Depending upon the final satellite design, these tools include but may not be limited to:

[**Redacted**]

 

13.4 DigitalGlobe Procedure Development Support

DigitalGlobe will generate the on-orbit procedures for the WV3 satellite(s). BATC shall understand the DigitalGlobe Concept-of-Operations and assist the procedure development. BATC shall review DigitalGlobe developed procedures for technical, operational, and safety concerns. [**Redacted**]

 

13.5 Commissioning Plan (CDIL LM-6)

DigitalGlobe shall generate the Commissioning Plan for the WV3 satellite. BATC shall assist the commissioning plan development. This includes assisting with the definition of the nominal sequence of events, required prerequisites, allowed out-of-sequence events, and required technical support for each event. DigitalGlobe will provide information about ground contacts, mission control center operations, and other necessary ground information used to create the commissioning plan(s).

 

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The Commissioning Plan shall include subsystem initialization, calibration, and demonstration of performance requirements including, but not limited to, the following:

[**Redacted**]

 

13.6 Anomaly Preparations

DigitalGlobe will generate anomaly resolution flow-charts. BATC shall assist with the anomaly flow-chart development including defining the probable anomalies and proper recovery actions/sequences. BATC shall review DigitalGlobe anomaly resolution flow-charts for technical, operational, and safety concerns.

 

13.7 Satellite Commissioning

13.7.1    Launch and Early Operations (LEOP) Phase

DigitalGlobe shall direct Satellite Launch and Early Operations. BATC shall provide a dedicated engineer for all satellite subsystems except for the Instrument subsystem. This support will run 24 hours per day for up to 7 days at the DigitalGlobe Mission Control Center in Longmont, CO.

13.7.2    Verification and Calibration (V&C) Phase

DigitalGlobe shall conduct the Verification and Calibration activities necessary to achieve Full Operational Capability (FOC). This includes but is not limited to satellite calibration activities such as star tracker and gyroscope calibrations.

Barring anomalies, V&C activities will nominally occur between 0600 and 1800 hours seven days per week. V&C activities will nominally require 30 days. BATC shall provide a dedicated engineer for all satellite subsystems except for the Instrument subsystem.

BATC shall also provide off-hour, on-call engineering support during V&C. A 30 minute or less call-back response is required.

13.7.2.1    Commissioning Reports (CDIL LM-7)

BATC shall produce a Commissioning Report. The report will document spacecraft bus Beginning-of-Life (BOL) performance and will update End-of-Life (EOL) performance predictions for all subsystems for which it has responsibility. At a minimum the report shall include:

 

  a. An explanation of significant deviations from performance metrics as identified in the satellite specification. The explanation shall include the reasons for the performance delta and the anticipated effects, if any, on the subsystem or satellite.

 

  b. An explanation of any known component or sub-component failures encountered during the LEOP or V&C Phases. The explanation shall include the possible causes of the failure, workarounds, updated reliability analysis for the component, subsystem, and satellite, and any impacts to DigitalGlobe’s concept of operation.

 

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13.8 Satellite Simulator

BATC shall provide a high fidelity dynamic satellite simulator. The simulator shall simulate satellite responses to stimuli. BATC shall provide sufficient documentation to accurately capture the design, functionality, capabilities, limitations, maintenance, extension, and operation of the simulator.

13.8.1    Satellite Simulator (CDIL LM-8)

BATC shall deliver a high fidelity satellite simulator per the requirements document [**Redacted**] . [**Redacted**] BATC and DigitalGlobe shall mutually agree upon a computer hardware and operating system, called the computing platform, for use in simulator functional and performance acceptance testing. BATC shall execute spacecraft simulator acceptance testing on the identified platform. DigitalGlobe shall execute the simulator testing on the same platform.

The satellite simulator does not need to include the MGB subsystem.

13.8.2    Documentation (CDIL LM-9)

BATC shall provide a User’s manual with sufficient detail to:

 

   

Develop simulation scenarios including all configuration files, scripts, procedures, ephemeris, initial conditions, etc

 

   

Start-up, shut-down, and operate the simulation console and all simulator components

 

   

Control the simulation in real-time by setting/adjusting variables

 

   

Inspect low level model telemetry through the simulation console and simulator components directly

 

   

Save, modify, and load simulator state files used to start, pause, resume, and diagnose simulation scenarios

 

   

Understand all log files and log entries

 

   

Understand and recover from all error conditions

 

   

Extend, modify, maintain, build and release the simulator.

 

   

Incorporate a new flight software release into the simulator

In this context, “maintain” refers to the functions required to upgrade to new versions of commercial products such as MatLab or Simulink, alter configuration files, or otherwise customize the implementation.

13.8.3    Source Code (CDIL LM-10)

Per the terms of the software license agreement set forth in the Agreement, BATC shall provide all BATC developed bus simulator software components in source format (non binary). Source code shall be delivered in originating and native format. BATC does not need to provide development tools or COTS software, but BATC shall provide COTS software tool configuration including supplier, part number, and revision levels of tools used (e.g. compilers, linkers, and other development tools) and all reasonable data/information necessary for DigitalGlobe to enhance, modify, compile, and deploy the simulator.

 

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13.8.4    Delivery Schedule

BATC shall provide the simulator, manuals, and source code per Attachment 1. BATC shall deliver an updated simulator based upon LEOP/commissioning on-orbit performance. At a minimum, the following subsystem models will be updated: thermal, power, and ADCS models.

13.8.5    Technical Interchange Meetings and Design Reviews

BATC shall include DigitalGlobe in technical interchange meetings and design reviews such that DigitalGlobe can explain the intent behind various simulator requirements. BATC and DigitalGlobe shall refine high level requirements to detailed requirements during technical interchange meetings. BATC shall hold preliminary and critical design reviews for the Satellite Simulator. BATC shall hold intermediate Technical Interchange Meetings for the following modules at a minimum: the console, sensor and actuator models, redundancy modeling, fault modeling, thermal modeling, and power modeling.

 

13.9 Maneuver Planners

[**Redacted**]

13.9.1    [**Redacted**]

[**Redacted**]

13.9.2    [**Redacted**]

[**Redacted**]

13.9.3    [**Redacted**]

[**Redacted**]

13.10    Software Test Bench

BATC shall maintain a test bench suitable for the development and troubleshooting of the satellite computer Flight Software. The bench will include at a minimum:

[**Redacted**]

13.11    Ground Stations

DigitalGlobe is responsible for all Ground Station equipment. DigitalGlobe operators will be the lead operators of the Ground Segment.1

13.12    Telemetry Packet Creation and Mapping Tools (CDIL LM-15)

BATC shall provide the documentation, software, and training necessary for making changes to the telemetry received from the satellite. This includes changes to both telemetry packets and the mapping of those packets into various telemetry streams under CCSDS Grade C protocol.

 

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Initial delivery shall coincide with initial delivery of the Command & Telemetry Handbook (C&TH). BATC shall update if necessary at a. launch minus 6 months, b. final pre-launch C&TH delivery, and c. launch plus 6 months. Training shall occur coincident with Training Sessions specified in section 13.1 with delta training, if needed, at the final pre-launch C&TH delivery.

13.13    Telemetry Monitor and Response (CDIL LM-16)

BATC shall provide the documentation, software, and training necessary for making changes to flight software telemetry monitors and response actions on the satellite. This includes creation of new telemetry monitors and response actions, and changes to existing monitors and response actions.

Initial delivery shall coincide with initial delivery of the Command & Telemetry Handbook (C&TH). BATC shall update if necessary at a. launch minus 6 months, b. final pre-launch C&TH delivery, and c. launch plus 6 months. Training shall occur coincident with Training Sessions specified in section 13.1 with delta training, if needed, at the final pre-launch C&TH delivery.

 

14.0 COMMUNICATIONS FLEXIBILITY AND TT&C DEFINITION

BATC shall work with DigitalGlobe to set/finalize satellite ID’s by CDR.

 

15.0 FACILITIES

BATC shall provide all facilities necessary to perform the scope of this SOW.

 

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LOGO    WV3 Satellite Statement of Work_
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ATTACHMENT 1        CONTRACT DATA ITEMS LIST

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

PROGRAM MANAGEMENT

PM-1

   Program Management Structure    4.2    [**Redacted**]    As req’d   

PM-2

   Master Program Schedule    4.4    [**Redacted**]    monthly   

PM-3

   Component/Subsystem Design Review Listing    4.5.4    [**Redacted**]    As req’d   

PM-4

   Component/Subsystem Test Readiness / Data Review Listing    4.5.5    [**Redacted**]    As req’d   

PM-5

   Documentation Listing    4.6.3    [**Redacted**]    No later than Bi-monthly   

PM-6

   Action Item List    4.7    [**Redacted**]    As req’d   

PM-7

   Historical Record of Payments & Payments Forecast    4.8.1 & 4.8.2    [**Redacted**]    monthly   
DESIGN               

D-1

   Satellite to Instrument ICD    5.3.1    [**Redacted**]    As req’d   

D-2

   Satellite to Ground Station Narrowband ICD    5.3.2    [**Redacted**]    As req’d   

D-3

   Satellite to Ground Station Wideband Link ICD    5.3.3    [**Redacted**]    As req’d   

D-4

   Satellite Environmental Design and Test Specification    5.3.4    [**Redacted**]    As req’d   

D-5

   Contamination Control Plan    5.3.5    [**Redacted**]    As req’d   

D-6

   Satellite Level Requirements Verification/Compliance Matrix    5.3.6    [**Redacted**]    As req’d   

D-7

   Box Level Requirements Verification/Compliance Matrix    5.3.7    [**Redacted**]    As req’d   

D-8

   Drawings    5.3.8    [**Redacted**]    with EOs   

D-9

   Performance Compliance Matrix    5.3.9.1    [**Redacted**]    Quarterly   

D-10

   Risk Management Report    5.3.9.2    [**Redacted**]    Monthly   

 

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   Attch 1 - 1


LOGO    WV3 Satellite Statement of Work_
   Doc Number 10329656

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

D-11

   Subsystem Description Docs    5.3.10    [**Redacted**]    Launch – 4 m; Launch + 4 m    Updates only as required

D-12

   Thermal Analysis and Reports    5.3.11.a    [**Redacted**]    As req’d   

D-13

   Structural Analysis    5.3.11.b    [**Redacted**]    As req’d   

D-14

   Control System Analysis    5.3.11.c    [**Redacted**]    As req’d   

D-15

   Failure Modes and Effects and Criticality Analysis (FMECA)    5.3.11.d    [**Redacted**]    As req’d   

D-16

   Satellite Reliability Analysis    5.3.11.e    [**Redacted**]    As req’d   

D-17

   Satellite Imaging Performance    5.3.11.h    [**Redacted**]    As req’d   

D-18

   Critical Items List    5.3.13    [**Redacted**]    As req’d   

D-19

   Component Heritage Summary    5.3.14    [**Redacted**]    As req’d   

D-20

   System Engineering Reports    5.3.16    [**Redacted**]      

D-21

   Flight Software Code    5.3.16    [**Redacted**]    As req’d Final @ PSR   

D-22

   Composite Grounding Design    5.3.17    [**Redacted**]    As req’d   

D-23

   Structural, Power, Thermal, and Reliability Analytical Models    5.3.18    [**Redacted**]    L+3 m   

D-24

   Coordinate Transformation Document    5.3.19    [**Redacted**]    L – 4m   

D-25

   Flight Software Users Manual    5.3.20    [**Redacted**]    As req’d   

D-26

   Component Acceptance Data Package    5.3.21    [**Redacted**]    As req’d   

D-27

   Jitter Analysis and Test Data    5.3.22    [**Redacted**]    As req’d   

D-28

   Telescope Boresight Stability Data    5.3.23    [**Redacted**]    As req’d   

D-29

   Position and Attitude Accuracy    5.3.24    [**Redacted**]    As req’d   

D-30

   PDR Data Package    4.5.3    [**Redacted**]    As req’d   

D-31

   CDR Data Package    4.5.3    [**Redacted**]    As req’d   

D-32

   Satellite to MGB ICD    5.3.25    [**Redacted**]    As req’d   

 

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LOGO    WV3 Satellite Statement of Work_
   Doc Number 10329656

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

D-33    Electrical GSE ICD    5.3.26    [**Redacted**]    As req’d   
D-34    Satellite Requirements Review    4.5.3.1    [**Redacted**]      
D-35    Battery Life Prediction    5.3.11.g    [**Redacted**]    L+ 1m   
PRODUCT ASSURANCE
QA-1    EEE Parts List    6.2.1    [**Redacted**]      
QA-2    Material Identification and Use Listing    6.2.2    [**Redacted**]    See para 6.3.2   
QA-3    As built configured article list    6.3.1    [**Redacted**]    At Launch Readiness Review   
QA-4    Certification of Conformance    6.3.2    [**Redacted**]      
QA-5    Product Assurance Reviews    6.4    [**Redacted**]      
PROCUREMENT, PRODUCTION & TEST
PT-1    Make / Buy Plans    7.2    [**Redacted**]    As req’d   
PT-2    Program Subcontract Status Report    7.5    [**Redacted**]    monthly   
PT-3    WV I&T Plan    9.3    [**Redacted**]    As req’d   
PT-4    Battery Maintenance Plan    9.3.e    [**Redacted**]    As req’d   
PT-5    System Test Reports    9.6    [**Redacted**]      
PT-6    I&T Command and Telemetry Log Files    9.8.4    [**Redacted**]    weekly   
PT-7    Reserved    Na    [**Redacted**]      
PT-8    Instrument Integration Readiness Review Data Package    4.5.3    [**Redacted**]      
PT-9    Satellite Environmental Testing Readiness Review Data Package    4.5.3    [**Redacted**]      
PT-10    Pre-Ship Review Data Package    4.5.3    [**Redacted**]      
LAUNCH AND MISSION
LM-1    Missile Systems Pre-Launch Safety Package (MSPSP)    12.1    [**Redacted**]    L-52 wks TBD L-26 wks TBD   
LM-2    Preliminary WV3 FEM    12.4.a    [**Redacted**]      
   Preliminary CLA-to-WV3 Design Loads Comparison    12.4.b    [**Redacted**]      

 

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LOGO    WV3 Satellite Statement of Work_
   Doc Number 10329656

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

   Final WV3 FEM    12.4.c    [**Redacted**]      
   Final CLA-to-WV3 Design Loads Comparison    12.4.d    [**Redacted**]      
LM-3    Training Materials and sessions    13.1.1    [**Redacted**]    As revised   
LM-4    Command &Telemetry Handbook    13.2    [**Redacted**]    As revised   
LM-5    Calibration Tools    13.3    [**Redacted**]    As revised & L+3 m   
LM-6    Commissioning Plan    13.5    [**Redacted**]    As revised   
LM-7    Commissioning Report    13.7.2.1    [**Redacted**]      
LM-8    Satellite Simulator    13.8.1    [**Redacted**]    See Para 3.1.b   
LM-9    Satellite Simulator Documentation    13.8.2    [**Redacted**]    With LM-8   
LM-10    Satellite Simulator Source Code    13.8.3    [**Redacted**]    With LM-8   
LM-11    High Fidelity Maneuver Planner    13.9.1    [**Redacted**]      
LM-12    Peak Estimator Algorithm    13.9.2    [**Redacted**]      
LM-13    Integrative Maneuver Model    3    [**Redacted**]      
LM-14    Satellite Launch Readiness Review Data Package    4.5.3    [**Redacted**]      
LM-15    Telemetry Packet Creation and Mapping Tools    13.12    [**Redacted**]    See 13.12   
LM-16    Telemetry Monitor and Response    13.13    [**Redacted**]    See 13.13   
[**Redacted**]
[**Redacted**]    [**Redacted**]    4.5.3.1    [**Redacted**]      
[**Redacted**]    [**Redacted**]    4.5.3.1    [**Redacted**]      
[**Redacted**]    [**Redacted**]    4.5.3.1    [**Redacted**]      
[**Redacted**]    [**Redacted**]    4.5.3.1    [**Redacted**]      

 

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LOGO    WV3 Satellite Statement of Work_
   Doc Number 10329656

 

Data Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

[**Redacted**]    [**Redacted**]    4.5.3.1    [**Redacted**]      
[**Redacted**]    [**Redacted**]    4.5.3.11.i    [**Redacted**]    As rqd   
[**Redacted**]    [**Redacted**]    4.5.3.11.j    [**Redacted**]      
[**Redacted**]    [**Redacted**]    4.5.3.11.k    [**Redacted**]      
[**Redacted**]    [**Redacted**]    4.5.3.11.l    [**Redacted**]      
[**Redacted**]    [**Redacted**]    4.5.3.11.m    [**Redacted**]      

All items are provided for DigitalGlobe information only. Approvals are not required except for ICDs, changes to ICDs, and as otherwise noted.

ATP +1m is 1 month after Authorization to Proceed.

 

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ATTACHMENT 2        CUSTOMER FURNISHED EQUIPMENT LIST

 

Item

  

Title

   SOW
Ref
  

Date

  

Comment

FLIGHT HARDWARE

CFHW-1

   [**Redacted**]    10.2.1    [**Redacted**]   

CFHW-2

   [**Redacted**]    10.2.2    [**Redacted**]    Flight and corresponding ground keys.

CFHW-3

   [**Redacted**]    10.2.3    [**Redacted**]   

CFHW-4

   [**Redacted**]    10.2.4    [**Redacted**]   

CFHW-5

   [**Redacted**]    10.2.5    [**Redacted**]   

CFHW-6

   [**Redacted**]    10.2.6    [**Redacted**]   
[**Redacted**]

CSIM-1

   [**Redacted**]    10.3    [**Redacted**]    Remains the property of DG
[**Redacted**]

CLSE-1

   [**Redacted**]    10.4.1    [**Redacted**]   

CLSE-2

   [**Redacted**]    10.4.1    [**Redacted**]   

CLSE-3

   [**Redacted**]    10.4.2    [**Redacted**]   
[**Redacted**]

CGSE-1

   [**Redacted**]    10.5.1.a    [**Redacted**]    Remains the property of DG

CGSE-2

   [**Redacted**]    10.5.1.b    [**Redacted**]    Remains the property of DG

CGSE-3

   [**Redacted**]    10.5.1.c    [**Redacted**]    Remains the property of DG

CGSE-4

   [**Redacted**]    10.5.1.d    [**Redacted**]    Remains the property of DG

CGSE-5

   [**Redacted**]    10.5.2.    [**Redacted**]    Remains the property of DG

CGSE-6

   [**Redacted**]    10.5.2.0    [**Redacted**]    Remains the property of DG

CGSE-7

   [**Redacted**]    10.5.2.0    [**Redacted**]    Remains the property of DG

CGSE-8

   [**Redacted**]    10.5.3.a    [**Redacted**]    Remains the property of DG

CGSE-9

   [**Redacted**]    10.5.3.b    [**Redacted**]    Remains the property of DG

CGSE-10

   [**Redacted**]    10.5.3.c    [**Redacted**]    Remains the property of DG

CGSE-11

   [**Redacted**]    10.5.4    [**Redacted**]    Remains the property of DG

 

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LOGO    WV3 Satellite Statement of Work_
   Doc Number 10329656

 

Item

  

Title

   SOW
Ref
  

Date

  

Comment

CGSE-12

   [**Redacted**]    10.5.5    [**Redacted**]    Remains the property of DG

CGSE-13

   [**Redacted**]    10.5.6    [**Redacted**]    Remains the property of DG

CGSE-14

   [**Redacted**]    10.5.7    [**Redacted**]    Remains the property of DG

CGSE-15

   [**Redacted**]    10.5.8    [**Redacted**]    Remains the property of DG

CGSE-16

   [**Redacted**]    10.5.9    [**Redacted**]    Remains the property of DG
LAUNCH VEHICLE DATA ITEM

CLD-1

   WV3 Preliminary CLA    10.6    [**Redacted**]   

CLD-2

   WV3 Final CLA    10.6    [**Redacted**]   
INSTRUMENT DATA ITEM

CID-1

   WV3 Instrument Structural Data    10.7.1    [**Redacted**]   

CID-2

   WV3 Instrument Thermal Data    10.7.2    [**Redacted**]   

DigitalGlobe will provide this equipment in accordance with the requirements of the Agreement.

 

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Use or disclosure of data is subject to the restriction on the title page of this document.
   Attch 1 - 7


Attachment 2

Specifications for the WorldView 3 Satellite, Rev 7.0

Dated 13 Sept 2011


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

 

LOGO    Exhibit 2 to Contract 60150

 

 

WorldView-3 Satellite

Specification

 

 

 

  Document #    10329655
  Revision #    7.0
  Release Date    13 Sept 2011
  Prepared by    George Hunyadi
  Approved by    Keith Constantinides

This Document Is ITAR Controlled

This document contains Technical Data as defined and controlled under the International Traffic In Arms Regulations (ITAR). Transfer of this data by any means to a foreign person, whether in the United States or abroad, without an export license or other approval from the U.S. Department of State is prohibited.

RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION

This document contains information proprietary and confidential to DigitalGlobe , to its subsidiaries, or to a third party to whom DigitalGlobe may have a legal obligation to protect such information from unauthorized disclosure, use or duplication. Any disclosure, use or duplication of this document or of any of the information contained herein for other than the specific purpose for which it was disclosed is expressly prohibited, except as DigitalGlobe may otherwise agree to in writing. This document may only be used for the purpose for which it is provided. All copies of this document are the sole property of DigitalGlobe and will be returned promptly upon request.


LOGO

   WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 7.0: 13 Sept 2011

 

 

Change Record

 

Revision

   Date   

Sections

  

Description of Change

1.0    20 Aug 2010    All    Initial Release
[**Redacted**]         
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        

 

 

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DigitalGlobe Proprietary and Confidential

  Use or disclosure of data is subject to the restriction on the title page of this  document.    i


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 7.0: 13 Sept 2011

 

 

Table of Contents

 

1.   

SCOPE

     7   
   1.1   

P URPOSE

     7   
   1.2   

S YSTEM O VERVIEW

     7   
   1.3   

D OCUMENT O VERVIEW

     7   

2.

  

APPLICABLE DOCUMENTS

     8   
   2.1   

G OVERNMENT D OCUMENTS

     8   
     

2.1.1

  

[ **Redacted**]

     8   
     

2.1.2

  

[**Redacted**]

     8   
   2.2   

N ON -G OVERNMENT D OCUMENTS

     8   
     

2.2.1

  

[**Redacted**]

     8   
     

2.2.2

  

[**Redacted**]

     8   
     

2.2.3

  

[**Redacted**]

     8   
   2.3   

R EFERENCE D OCUMENTS

     8   

3.

  

REQUIREMENTS

     9   
   3.1   

S ATELLITE D EFINITION

     9   
     

3.1.1

  

Satellite Diagrams

     9   
        

3.1.1.1

  

Component Tree

     9   
        

3.1.1.2

  

Coordinate System

     9   
     

3.1.2

  

Satellite Interfaces

     9   
        

3.1.2.1

  

Non-interference with Outside Systems

     9   
           

3.1.2.1.1

  

[**Redacted**

     9   
           

3.1.2.1.2

  

[**Redacted**]

     9   
           

3.1.2.1.3

  

[**Redacted**]

     9   
        

3.1.2.2

  

Satellite-Global Positioning System Interfaces

     9   
           

3.1.2.2.1

  

Compatibility

     9   
        

3.1.2.3

  

Satellite-Ground Interfaces

     10   
           

3.1.2.3.1

  

Compatibility

     10   
           

3.1.2.3.2

  

Remote Ground Terminal Locations

     10   
           

3.1.2.3.3

  

Command Uplink

     10   
           

3.1.2.3.4

  

Narrowband Telemetry Downlink

     10   
           

3.1.2.3.5

  

Wideband Data Downlink

     10   
        

3.1.2.4

  

Satellite-Launch Vehicle Interfaces

     11   
           

3.1.2.4.1

  

Compatibility

     11   
           

3.1.2.4.2

  

[**Redacted**]

     11   
           

3.1.2.4.3

  

Umbilical

     11   
     

3.1.3

  

Customer Furnished Equipment

     11   
        

3.1.3.1

  

Instrument

     11   
           

3.1.3.1.1

  

Physical, Structural and Mechanical Requirements

     12   
           

3.1.3.1.2

  

Thermal Interfaces

     12   
           

3.1.3.1.3

  

Power Interfaces

     12   
           

3.1.3.1.4

  

Command and Telemetry Interfaces

     13   
           

3.1.3.1.5

  

Image Data Interfaces

     13   
           

3.1.3.1.6

  

EOA Thermal Control Interfaces

     13   
           

3.1.3.1.7

  

[**Redacted**]

     14   

 

 

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LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 7.0: 13 Sept 2011

 

 

         3.1.3.2   

MGB

     14   
         3.1.3.3   

[**Redacted**]

     14   
         3.1.3.3.1   

[**Redacted**]

     14   
         3.1.3.3.2   

[**Redacted**]

     14   
         3.1.3.3.3   

[**Redacted**]

     14   
         3.1.3.3.4   

[**Redacted**]

     14   
         3.1.3.3.5   

[**Redacted**]

     15   
         3.1.4   

[**Redacted**]

     15   
         3.1.4.1.1   

[**Redacted**]

     15   
         3.1.4.1.2   

[**Redacted**]

     15   
         3.1.4.1.3   

[**Redacted**]

     16   
         3.1.4.1.4   

[**Redacted**]

     16   
         3.1.4.1.5   

[**Redacted**]

     16   
   3.2   

S ATELLITE C HARACTERISTICS

     16   
     

3.2.1

   Performance      17   
         3.2.1.1   

General Mission Requirements

     17   
            3.2.1.1.1   

Mission Life

     17   
            3.2.1.1.2   

Orbits

     17   
         3.2.1.2    Satellite Operating Modes      17   
            3.2.1.2.1   

Normal Operating Modes

     17   
            3.2.1.2.2   

Special / Contingency Modes

     18   
            3.2.1.2.3   

Intermediate and Transitional Modes

     19   
         3.2.1.3    Pre-Launch Operations      19   
            3.2.1.3.1   

Ground Storage

     19   
            3.2.1.3.2   

Launch Delay

     19   
         3.2.1.4    Early Orbit Operations      20   
            3.2.1.4.1   

Autonomous Operations After Separation

     20   
            3.2.1.4.2   

First [**Redacted**]

     20   
            3.2.1.4.3   

Commissioning

     20   
         3.2.1.5    Mission Operations      20   
            3.2.1.5.1   

Viewing Angles

     20   
            3.2.1.5.2   

Imaging and Downlink Operations

     20   
            3.2.1.5.3   

Stereo Imaging

     21   
            3.2.1.5.4   

Off-Nadir Imaging

     21   
            3.2.1.5.5   

[**Redacted**]

     21   
            3.2.1.5.6   

[**Redacted**]

     21   
         3.2.1.6    Instrument Requirements      21   
            3.2.1.6.1   

Integrated Bus/Instrument Performance Effects

     21   
            3.2.1.6.2   

[**Redacted**]

     21   
            3.2.1.6.3   

[**Redacted**]

     22   
            3.2.1.6.4   

Instrument Cleanliness

     23   
         3.2.1.7    Bus Subsystem Requirements      23   
            3.2.1.7.1   

[**Redacted**]

     23   
            3.2.1.7.2   

ADCS

     24   
            3.2.1.7.3   

Propulsion

     26   
            3.2.1.7.4   

Flight Software

     27   

 

 

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            3.2.1.7.5    C&DH      28   
           

3.2.1.7.6

  

Narrowband Communications

     32   
           

3.2.1.7.7

  

[**Redacted**]

     34   
           

3.2.1.7.8

  

EPDS

     37   
           

3.2.1.7.9

  

Structures and Mechanisms

     38   
           

3.2.1.7.10

  

Thermal Control

     39   
           

3.2.1.7.11

  

Direct Tasking

     40   
     

3.2.2

   Physical Characteristics      44   
         3.2.2.1   

Size Constraints

     44   
         3.2.2.2   

Mass Constraints

     44   
         3.2.2.3   

Shipping Constraints

     44   
     

3.2.3

   Reliability      44   
         3.2.3.1   

End of Life Ps

     44   
         3.2.3.2   

[**Redacted**]

     44   
         3.2.3.3   

[**Redacted**]

     44   
         3.2.3.4   

Cycle-Limited Items

     44   
           

3.2.3.4.1

  

[**Redacted**]

     44   
           

3.2.3.4.2

  

[**Redacted**]

     45   
     

3.2.4

   Availability and Maintainability      45   
         3.2.4.1   

Fault Recovery Timeline

     45   
         3.2.4.2   

Environmental Conditions

     45   
            3.2.4.2.1   

Launch Induced Environments

     45   
           

3.2.4.2.2

  

On-Orbit Environments

     45   
           

3.2.4.2.3

  

Pre-Launch Environments

     45   
   3.3   

S ATELLITE D ESIGN AND C ONSTRUCTION

     45   
     

3.3.1

   General      45   
     

3.3.2

   SEUs      45   
     

3.3.3

   Immunity to Latch-Up      45   
     

3.3.4

   Cleanliness and Contamination Control      45   
         3.3.4.1   

[**Redacted**]

     46   
         3.3.4.2   

[**Redacted**]

     46   
         3.3.4.3   

[**Redacted**]

     46   
         3.3.4.4   

[**Redacted**]

     46   
     

3.3.5

   Safety      46   
     

3.3.6

   [**Redacted**]      46   

4.

  

VERIFICATION

     46   

5.

  

QUALITY ASSURANCE

     46   

 

 

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LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 7.0: 13 Sept 2011

 

 

List of Tables

[**Redacted**]

List of Figures

[**Redacted**]

 

 

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LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 7.0: 13 Sept 2011

 

 

1. SCOPE

 

1.1 Purpose

This document describes the requirements for design and implementation of the DigitalGlobe WorldView-3 Satellite, being constructed to support DigitalGlobe commercial imaging operations.

 

1.2 System Overview

Ball Aerospace & Technology Corporation (BATC) is providing the integrated WorldView-3 imaging satellite to DigitalGlobe, Inc. As the Space Segment Integrator (SSI), BATC is manufacturing a Spacecraft Bus that can accommodate the panchromatic + multi-spectral WorldView-3 Instrument [**Redacted**] . This will be the same Bus design as used for predecessor WorldView Satellites. The Instrument is being supplied by ITT Industries Space Systems Division (ITT) to DigitalGlobe, with miscellaneous support units / functions provided by BATC. All ITT equipment will be provided as Customer Furnished Equipment (CFE) to BATC for Satellite integration. [**Redacted**] As the SSI, BATC will then perform Satellite level testing, prepare the Satellite for launch, and support on-orbit checkout of the Satellite.

The Satellite will be in a sun-synchronous orbit at an altitude between 450 and 830 km with a descending equator crossing time between 10:00 AM and 2:00 PM. [**Redacted**] Image data is recorded by the Spacecraft Bus and is normally downlinked to DigitalGlobe ground stations. However, direct downlink to user sites may also be performed in certain circumstances. Direct downlink is via the normal wideband downlink.

A key feature of the WordView-3 Satellite is Direct Tasking, where imaging and downlink parameters are directly uplinked from a customer’s ground station to the satellite, and image data is directly downlinked to a customer’s ground station, on the same and/or successive passes. Direct Tasking supports an expanded customer base and fulfills these customers’ desires to compress the overall planning-tasking-collection-downlink timeline and to not expose their task list to outside parties (including DigitalGlobe) prior to image collection. Full command authority is maintained by DigitalGlobe, with key commands needed to initiate the image and downlink operations uploaded from DigitalGlobe ground stations.

 

1.3 Document Overview

This document specifies functional, performance and interface requirements for the integrated Satellite and the Spacecraft Bus, including external Satellite interfaces, Instrument-Bus interfaces and Instrument integration, Bus and Satellite test, launch, and operational requirements. Separate Interface Control Documents (ICDs) detail the specifics of the Instrument-Bus interfaces and Integration and Test processes. Satisfaction of the Satellite-level requirements contained in this specification assume the Instrument provided as CFE meets its requirements, which are documented separately. As the SSI, BATC will refer to the separate Instrument Specifications as necessary to maintain the Spacecraft Bus to Instrument ICDs and develop an integration and test plan sufficient to ensure the integrated Satellite meets its system-level functional and performance requirements.

 

 

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This specification may contain requirements that have not been fully defined. These open requirements are indicated by a TBR, and/or TBD:

TBR – To Be Resolved: Indicates parameters that exist, but may change after discussions with Contractor and others (e.g.: DigitalGlobe).

TBD – To Be Determined: Indicates parameters that have not yet been determined.

 

2. APPLICABLE DOCUMENTS

This document is the Satellite Specification. This specification defines the technical requirements called out in the Contract and a Statement of Work (SOW). The Contract and SOW define schedule requirements, deliverable items and programmatics. However, in the event of a conflict between a specific requirement herein and documents, then the Contract, the Statement of Work, this document, and Applicable documents shall govern in this order. If the revision is not specifically noted, the latest revision of each document applies.

At contract signing, the Environmental Design and Test Specification and Interface Control Documents from predecessor DigitalGlobe WorldView satellite programs listed below shall be considered the baseline release for WV-3. It is anticipated that the WV-3 versions of these documents will require few modifications from the predecessor baselines, with changes focused in a few key areas as driven by WV-3 unique requirements (for example enhanced Instrument thermal control and updated power values). The first release of the WV-3 version of each document shall supersede the predecessor version, which shall no longer be considered an Applicable Document.

Although the Satellite Integrating Contractor physically maintains many of these ICDs, their development is inherently a cooperative process. Accordingly, the latest released ICD revision shall always apply, where release is predicated on mutual agreement between all involved parties; for example the Instrument to Spacecraft ICD requires consensus between the Satellite Integrating Contractor, the Instrument Contractor, and DigitalGlobe.

 

2.1 Government Documents

 

2.1.1 [**Redacted**]

 

2.1.2 [**Redacted**]

 

2.2 Non-Government Documents

 

2.2.1 [**Redacted**]

 

2.2.2 [**Redacted**]

 

2.2.3 [**Redacted**]

 

2.3 Reference Documents

[**Redacted**]

 

 

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3. REQUIREMENTS

Remarks contained as Rationale/Info shall NOT be considered a formal part of this specification and are provided for reference only.

[**Redacted**]

 

3.1 Satellite Definition

This Section defines fundamental terminology and identifies the basic Satellite functions along with the provider of each function. It also provides external interface requirements and internal interface requirements for the equipment to be provided [**Redacted**] to the SSI.

 

3.1.1 Satellite Diagrams

3.1.1.1    Component Tree

[**Redacted**] defines the major elements, subsystems, assemblies and units/functions of the Satellite and shows how they are allocated between DigitalGlobe’s contractors. The figure also indicates items that are delivered to the SSI [**Redacted 1 Page**].

3.1.1.2    Coordinate System

The base coordinate system used for all major Satellite element and segment mechanical interfaces shall be as shown in [**Redacted**] , for example, Instrument to Spacecraft Bus and Satellite to Launch Vehicle.

Other coordinate systems may be used as appropriate within elements and/or subsystems; [**Redacted**] . The relationships between the base coordinate system and other coordinate systems shall be explicitly shown in the appropriate documents (drawings, interface control documents, etc.).

[**Redacted**]

 

3.1.2 Satellite Interfaces

3.1.2.1    Non-interference with Outside Systems

3.1.2.1.1    [**Redacted**]

The Satellite shall not interfere with [**Redacted**].

3.1.2.1.2    [**Redacted**]

During normal operations, RF emissions from the Satellite shall not exceed the limits specified in the [**Redacted**] .

3.1.2.1.3    [**Redacted**]

All RF emissions shall use the frequency allocation of [**Redacted**] , with out-of-band emissions compliant with [**Redacted**].

3.1.2.2    Satellite-Global Positioning System Interfaces

3.1.2.2.1    Compatibility

The Spacecraft Bus shall be compatible with standard GPS interfaces as defined in [**Redacted**] .

 

 

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3.1.2.3    Satellite-Ground Interfaces

The following paragraphs define high-level requirements for Satellite-Ground compatibility; detailed interface requirements shall be defined in the Narrowband and Wideband Satellite-Ground ICD.

[**Redacted**]

3.1.2.3.1    Compatibility

The Satellite Narrowband and Wideband Communications Subsystems shall be compatible with [**Redacted**] .

3.1.2.3.2    Remote Ground Terminal Locations

Remote Ground Terminals (RGTs) will be located as follows:

[**Redacted**]

3.1.2.3.3    Command Uplink

3.1.2.3.3.1    Effective Isotropic Radiated Power

The minimum Effective Isotropic Radiated Power (EIRP) of the command uplink antenna will be [**Redacted** ].

3.1.2.3.3.2    Axial Ratio

The command uplink antenna will transmit using [**Redacted**] .

3.1.2.3.4    Narrowband Telemetry Downlink

3.1.2.3.4.1    Figure of Merit (G/T)

The minimum G/T of the Narrowband receive antenna will be as follows across the frequency range of [**Redacted**] under all conditions, for the RGT locations defined in Section 3.1.2.3.2 Remote Ground Terminal Locations. These values include the effects of antenna pointing error and atmospheric conditions.

[**Redacted**]

3.1.2.3.4.2    Axial Ratio

The Narrowband receive antenna will receive using [**Redacted**] .

3.1.2.3.4.3    Implementation Loss

The demodulator implementation loss for the Narrowband telemetry receiver will be [**Redacted**] .

3.1.2.3.5    Wideband Data Downlink

3.1.2.3.5.1    Figure of Merit (G/T)

The minimum G/T of the Wideband receive antenna will be as follows across the frequency range of [**Redacted**] under all conditions, for the RGT locations defined in Section 3.1.2.3.2 Remote Ground Terminal Locations. These values include the effects of antenna pointing error and atmospheric conditions.

[**Redacted**]

3.1.2.3.5.2    Axial Ratio

The Wideband receive antenna will receive using [**Redacted**] .

 

 

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3.1.2.3.5.3    Implementation Loss

The demodulator implementation loss for the wideband telemetry receiver will be [**Redacted**] .

3.1.2.4    Satellite-Launch Vehicle Interfaces

The following paragraphs define high-level requirements for Satellite – Launch Vehicle compatibility; detailed interface requirements shall be defined in the Mission Specification.

3.1.2.4.1    Compatibility

The Satellite design shall be compatible with the [**Redacted**]

3.1.2.4.2    [**Redacted**]

The Satellite shall accommodate [**Redacted**].

3.1.2.4.3    Umbilical

The Satellite shall accommodate an umbilical to support all required functions for launch mode, including at a minimum the following critical electrical functions:

[**Redacted**]

3.1.3 Customer Furnished Equipment

3.1.3.1    Instrument

The Instrument will be provided to the SSI [**Redacted**] . The SSI shall provide interfaces as specified herein, with detailed interface requirements provided in accordance with the [**Redacted**] .

3.1.3.1.1    Physical, Structural and Mechanical Requirements

3.1.3.1.1.1    Configuration

The Spacecraft Bus shall accommodate the following major Instrument assemblies and/or units:

[**Redacted**]

3.1.3.1.1.2    Size

The Spacecraft Bus shall be capable of supporting the Instrument assemblies/units as specified in the Spacecraft Bus to Instrument ICDs.

3.1.3.1.1.3    Mass Properties

[**Redacted**]

3.1.3.1.1.4    EOA-Mounted Spacecraft Bus Equipment

The SSI shall provide the following equipment to be mounted on the EOA:

[**Redacted**]

3.1.3.1.1.5    EOA Fields of View

The Spacecraft Bus shall provide the Instrument with [**Redacted**] .

3.1.3.1.1.6    EOA Purge Fitting

The Satellite shall be configured to provide a purge fitting [**Redacted**] .

 

 

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3.1.3.1.1.7    Assembly, Integration and Test

 

a) To the maximum extent possible, the Satellite configuration shall permit independent integration of all Instrument assemblies/units and access to internal Instrument test ports and harness connections.

 

b) The Satellite configuration shall allow clear access to Instrument equipment essential to integration and test activities, for example: test ports, purge lines, aperture cover, interface connectors, etc.

3.1.3.1.1.8    EOA Vibration Environment

The SI shall ensure that the [**Redacted**]

3.1.3.1.1.9    [**Redacted**]

The Spacecraft Bus shall provide radiation shielding for the [**Redacted**] .

3.1.3.1.2    Thermal Interfaces

The Spacecraft Bus shall perform the following thermal functions, with interfaces to the Instrument as specified in the Spacecraft Bus to Instrument ICDs:

[**Redacted**]

3.1.3.1.3    Power Interfaces

The Spacecraft Bus shall provide electrical power to the Instrument as specified below, with the breakdown of individual unit powers and other characteristics as specified in the Spacecraft Bus to Instrument ICDs.

3.1.3.1.3.1    Instrument Power Feeds

The Spacecraft Bus shall provide power to all Instrument units as follows:

[**Redacted**]

3.1.3.1.3.2    Voltage

The Spacecraft Bus shall present power at the Instrument interfaces as follows:

[**Redacted**]

3.1.3.1.3.3    [**Redacted**]

[**Redacted**]

3.1.3.1.3.4    Average Operating Power

During normal operations, the Spacecraft Bus shall be able to perform [**Redacted**]

3.1.3.1.3.5    Survival Power

When in Emergency Mode, the Spacecraft Bus shall provide power as specified in [**Redacted**] via the Essential Bus, as specified in Section 3.1.3.1.3.1 Instrument Power Feeds.

3.1.3.1.3.6    Maximum Power

 

a) The Spacecraft Bus shall be capable of supporting the sustained maximum Instrument power specified in [**Redacted**] .

 

b) The Spacecraft Bus shall [**Redacted**]

 

 

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3.1.3.1.4    Command and Telemetry Interfaces

The Spacecraft Bus shall provide the following command and telemetry interfaces to the Instrument, all of which shall be cross-strapped between the primary and redundant Spacecraft Bus electronics and primary and redundant Instrument electronics:

[**Redacted**]

3.1.3.1.4.1    Instrument Commanding

Using the specified data interfaces, the Spacecraft Bus shall forward commands to the Instrument, [**Redacted**] as documented in the Spacecraft Bus to Instrument ICDs.

3.1.3.1.4.2    Image Start and Stop Commands

The commands for image [**Redacted**] shall be issued from the Spacecraft Bus [**Redacted**] .

3.1.3.1.4.3    Image Duration

 

a) The minimum Image duration possible shall be no more than [**Redacted**] .

 

b) There shall be [**Redacted**] .

 

c) Image durations shall be commandable in [**Redacted**] .

[**Redacted**]

3.1.3.1.4.4    Instrument Telemetry

Using the specified data interfaces, the Spacecraft Bus shall receive telemetry from the Instrument as documented in the Spacecraft Bus to Instrument ICDs. The following rules shall be applied to Instrument telemetry:

[**Redacted**]

3.1.3.1.4.5    [**Redacted**]

The Spacecraft Bus shall provide a [**Redacted**] as follows:

[**Redacted**]

3.1.3.1.5    Image Data Interfaces

The Spacecraft Bus shall provide image data interfaces [**Redacted**]

3.1.3.1.5.1    General Interface Definition

The Spacecraft Bus to Instrument data interface shall be as follows:

[**Redacted**]

3.1.3.1.5.2    Maximizing Storage and Downlink Efficiency

The Spacecraft Bus to Instrument data interface shall be capable of supporting the following Instrument configurations and shall ensure [**Redacted**]

3.1.3.1.6    EOA Thermal Control Interfaces

[**Redacted**]

3.1.3.1.6.1    [**Redacted**]

[**Redacted**]

3.1.3.1.6.2    [**Redacted**]

[**Redacted**]

 

 

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3.1.3.1.6.3    [**Redacted**]

[**Redacted**]

3.1.3.1.7    [**Redacted**]

The [**Redacted**] system will be provided to the SSI [**Redacted**] . The Spacecraft Bus shall interface to the [**Redacted**] system as specified in [**Redacted**] .

3.1.3.2    MGB

The MGB will be provided to the SSI [**Redacted**] . The SSI shall meet the MGB requirements specified in the MGB Requirements Documents and Interface Control Documents.

3.1.3.3    [**Redacted**]

[**Redacted**]

3.1.3.3.1     [**Redacted**]

3.1.3.3.1.1     [**Redacted**]

[**Redacted**]

3.1.3.3.1.2     [**Redacted**]

[**Redacted**]

3.1.3.3.1.3     [**Redacted**]

[**Redacted**]

3.1.3.3.1.4     [**Redacted**]

[**Redacted**]

3.1.3.3.2     [**Redacted**]

[**Redacted**]

3.1.3.3.3     [**Redacted**]

[**Redacted**]

3.1.3.3.3.1     [**Redacted**]

[**Redacted**]

3.1.3.3.3.2     [**Redacted**]

[**Redacted**]

 

 

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3.1.3.3.3.3     [**Redacted**]

[**Redacted**].

3.1.3.3.3.4     [**Redacted**]

[**Redacted**]

3.1.3.3.4     [**Redacted**]

[**Redacted**]

3.1.3.3.4.1     [**Redacted**]

[**Redacted**]

3.1.3.3.4.2    [**Redacted**]

[**Redacted**]

3.1.3.3.4.3     [**Redacted**]

[**Redacted**]

3.1.3.3.4.4     [**Redacted**]

[**Redacted**]

3.1.3.3.4.5     [**Redacted**]

[**Redacted**]

3.1.3.3.5     [**Redacted**]

[**Redacted**]

3.1.3.3.5.1     [**Redacted**]

[**Redacted**]

 

3.1.4 [**Redacted**]

[**Redacted**]

3.1.4.1.1     [**Redacted**]

[**Redacted**]

3.1.4.1.2     [**Redacted**]

[**Redacted**]

 

 

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3.1.4.1.3    [**Redacted**]

[**Redacted**]

3.1.4.1.3.1     [**Redacted**]

[**Redacted**]

3.1.4.1.3.2    [**Redacted**]

[**Redacted**]

3.1.4.1.4     [**Redacted**]

[**Redacted**]

3.1.4.1.4.1     [**Redacted**]

[**Redacted**]

3.1.4.1.4.2     [**Redacted**]

[**Redacted**]

3.1.4.1.4.3     [**Redacted**]

[**Redacted**]

3.1.4.1.4.4    [**Redacted**]

[**Redacted**]

3.1.4.1.5     [**Redacted**]

[**Redacted**]

 

3.2 Satellite Characteristics

This Section defines the characteristics of the Satellite required to support the mission with respect to performance, physical characteristics, reliability, availability, and environmental conditions. The SSI shall derive and otherwise define lower level requirements necessary to implement the requirements of this specification, including those that are passed to the Instrument Contractor via the Spacecraft Bus to Instrument ICD, the Environmental Design and Test Specification, and other relevant documents.

 

 

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3.2.1 Performance

3.2.1.1    General Mission Requirements

3.2.1.1.1    Mission Life

The Satellite shall meet all on-orbit performance requirements for a Mission Life of [**Redacted**] . The end of this period is defined as End of Life (EOL).

[**Redacted**]

3.2.1.1.2    Orbits

3.2.1.1.2.1    General Orbit Compatibility

The Satellite shall be capable of operating at any equatorial altitude between [ **Redacted**]

3.2.1.1.2.2    Reserved

3.2.1.1.2.3    Mission Orbit

The Mission Orbit shall be defined as:

[**Redacted**]

3.2.1.1.2.4    Reserved

3.2.1.1.2.5    Insertion Orbit and Dispersions

The Satellite shall be compatible with being inserted directly into any of the orbits defined under General Orbit Compatibility, [**Redacted**]

3.2.1.2    Satellite Operating Modes

3.2.1.2.1    Normal Operating Modes

The Satellite shall, at a minimum, provide the operating modes defined in Table 3-1 Normal Operating Modes, with the following additional requirements:

[**Redacted**]

Table 3-1 Normal Operating Modes

 

Mode

  

Basic Satellite State

  

Satellite Pointing

Cruise Mode

 

   [**Redacted**]    [**Redacted**]

[**Redacted**]

 

      [**Redacted**]

[**Redacted**]

 

   [**Redacted**]    [**Redacted**]

[**Redacted**]

 

      [**Redacted**]

 

 

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3.2.1.2.2    Special / Contingency Modes

The Satellite shall, at a minimum, provide the modes defined in [**Redacted**] , with the following additional requirements:

[**Redacted**]

Table 3-2 Special / Contingency Modes

 

Mode

  

Basic Satellite State

  

Satellite Pointing

[**Redacted**]

 

   [**Redacted**]    [**Redacted**]

[**Redacted**]

 

   [**Redacted**]    [**Redacted**]

[**Redacted**]

 

   [**Redacted**]   

 

 

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Table 3-3 Simultaneous Operations

 

Simultaneous
Operations

  

Normal Operating Modes

   Special / Contingency Modes
  

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]

Recording Image Data [**Redacted**]

         [**Redacted**]    [**Redacted**]            

Recording Ancillary Data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]         

Transmitting recorded Image and Ancillary Data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]         

Recording Satellite state of health data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]   

Transmitting stored state-of-health data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]   

Transmitting real-time state-of-health data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]   

Preserving stored Image and Ancillary Data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]   

Preserving stored state-of-health data

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]    [**Redacted**]

Receiving and executing real-time commands

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]

Receiving and storing stored commands

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]       [**Redacted**]   

Executing stored commands

   [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]    [**Redacted**]   

[**Redacted**]

3.2.1.2.3    Intermediate and Transitional Modes

Additional intermediate and transitional modes may be defined for the Satellite and Spacecraft Bus. [**Redacted**]

3.2.1.3    Pre-Launch Operations

3.2.1.3.1    Ground Storage

The Satellite shall be capable of being stored under proper conditions for up to [**Redacted**] without the need for refurbishment.

3.2.1.3.2    Launch Delay

 

a) The Satellite shall be capable of remaining loaded with propellant for a minimum of [**Redacted**] prior to launch, while maintaining safety and status monitoring.

 

b) The Satellite shall be capable of launch for up to [**Redacted**] following the integration of the Satellite to the Launch Vehicle without the need for demate, while maintaining safety and status monitoring.

 

c) The Satellite shall be designed to permit [**Redacted**] .

 

 

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3.2.1.4    Early Orbit Operations

3.2.1.4.1    Autonomous Operations After Separation

Following the separation event, the Satellite shall autonomously:

[**Redacted**]

3.2.1.4.2    First [**Redacted**]

Following the Autonomous Operations after Separation, the Satellite shall pose no constraints on operation such that:

[**Redacted**]

3.2.1.4.3    Commissioning

The Satellite shall pose no constraints on operation such that total Satellite on-orbit performance can be fully verified as specified in the Statement of Work.

3.2.1.5    Mission Operations

3.2.1.5.1    Viewing Angles

Viewing angles referred to in the [**Redacted**] and elsewhere in this specification shall be as defined below.

[**Redacted**]

3.2.1.5.1.1    Nominal Field of Regard

The Nominal Field of Regard shall be defined as a [**Redacted**]

3.2.1.5.1.2    Maximum Field of Regard

The Maximum Field of Regard shall be defined as a [**Redacted**]

3.2.1.5.1.3    [**Redacted**]

[**Redacted**]

3.2.1.5.1.4    [**Redacted**]

[**Redacted**]

3.2.1.5.1.5     [**Redacted**]

The Satellite shall allow operation of the Instrument in the modes specified in [**Redacted**]

3.2.1.5.2    Imaging and Downlink Operations

The Satellite shall be capable of performing the imaging and downlink operations specified below assuming [**Redacted**]

3.2.1.5.2.1    [**Redacted**]

[**Redacted 1 Page**]

3.2.1.5.2.2    Wideband and Narrowband Downlinks

It shall be possible to perform both Wideband and Narrowband downlinks as follows:

[**Redacted**]

3.2.1.5.2.3     Instrument Mass Properties for [**Redacted**]

For purposes of verifying the Satellite’s ability to perform the DIS, [**Redacted**]

 

 

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3.2.1.5.2.4    [**Redacted**]

[**Redacted**]

3.2.1.5.3    Stereo Imaging

 

a) The Satellite shall be capable of collecting the stereo imagery [**Redacted**]

 

b) The Satellite shall be capable of collecting stereo imagery [**Redacted**]

3.2.1.5.4    Off-Nadir Imaging

The Satellite shall be capable of supporting off-nadir image collections as follows:

[**Redacted**]

3.2.1.5.5    Special Imaging

3.2.1.5.5.1    Minimum Capabilities

[**Redacted**]

3.2.1.5.5.2    [**Redacted**]

[**Redacted**]

3.2.1.5.6    [**Redacted**]

[**Redacted**]

3.2.1.6    Instrument Requirements

3.2.1.6.1    Integrated Bus/Instrument Performance Effects

The SSI shall perform appropriate integrated Satellite-level analyses and design work in order to ensure the Satellite meets the following performance requirements. LOS motion shall be calculated using an Instrument Finite Element Model (FEM) provided by the Instrument Contractor as defined under Applicable Documents, which shall be assumed to meet the following requirements:

[**Redacted**]

3.2.1.6.1.1    [**Redacted**]

[**Redacted**]

3.2.1.6.1.2    [**Redacted**]

[**Redacted**]

3.2.1.6.2    [**Redacted**]

[**Redated**]

 

 

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3.2.1.6.2.1    [**Redated**]

[**Redacted**]

3.2.1.6.2.2    [**Redacted**]

[**Redacted**]

3.2.1.6.3    [**Redacted**]

[**Redacted**]

3.2.1.6.3.1    [**Redacted**]

[**Redacted**]

3.2.1.6.3.2    [**Redacted**]

[**Redacted**]

3.2.1.6.3.3    [**Redacted**]

[**Redacted**]

3.2.1.6.3.4    [**Redacted**]

[**Redacted**]

3.2.1.6.3.4.1    [**Redacted**]

[**Redacted**]

3.2.1.6.3.4.2    [**Redacted**]

[**Redacted**]

3.2.1.6.3.4.3    [**Redacted**]

[**Redacted**]

3.2.1.6.3.5    [**Redacted**]

[**Redacted**]

3.2.1.6.3.5.1    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.6.3.5.2    [**Redacted**]

[**Redacted**]

3.2.1.6.3.6    [**Redacted**]

[**Redacted**]

3.2.1.6.4    Instrument Cleanliness

[**Redacted**]

3.2.1.6.4.1    [**Redacted**]

[**Redacted**]

3.2.1.6.4.2    [**Redacted**]

[**Redacted**]

3.2.1.7    Bus Subsystem Requirements

In addition to supporting all subsystem-level requirements derived from the Satellite-level requirements specified in the above sections, Spacecraft Bus subsystems shall meet the specific requirements contained within this section.

3.2.1.7.1    [**Redacted**]

3.2.1.7.1.1    [**Redacted**]

[**Redacted**]

3.2.1.7.1.2    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.1    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.2    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.1.3.3    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.4    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.5    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.6    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.7    [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.8    [**Redacted**]

[**Redacted**]

3.2.1.7.1.4    [**Redacted**]

3.2.1.7.1.4.1    [**Redacted**]

[**Redacted**]

3.2.1.7.1.4.2    [**Redacted**]

[**Redacted**]

3.2.1.7.1.4.3    [**Redacted**]

[**Redacted**]

3.2.1.7.1.4.4    [**Redacted**]

[**Redacted**]

3.2.1.7.2 ADCS

3.2.1.7.2.1    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.2.2    [**Redacted**]

3.2.1.7.2.2.1    [**Redacted**]

[**Redacted**]

3.2.1.7.2.2.2    [**Redacted**]

[**Redacted**]

3.2.1.7.2.2.3    [**Redacted**]

[**Redacted**]

3.2.1.7.2.2.4    [**Redacted**]

[**Redacted**]

3.2.1.7.2.2.5    [**Redacted**]

[**Redacted**]

3.2.1.7.2.3    [**Redacted**]

[**Redacted**]

3.2.1.7.2.4    [**Redacted**]

3.2.1.7.2.4.1    [**Redacted**]

[**Redacted**]

3.2.1.7.2.4.2    [**Redacted**]

[**Redacted**]

3.2.1.7.2.5    [**Redacted**]

3.2.1.7.2.6    [**Redacted**]

[**Redacted**]

3.2.1.7.2.7    [**Redacted**]

[**Redacted**]

3.2.1.7.2.8    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.2.9    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.1    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.2    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.3    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.4    [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.5    [**Redacted**]

[**Redacted**]

3.2.1.7.2.10    [**Redacted**]

[**Redacted**]

3.2.1.7.2.11    Solar Arrays

In all modes of operation except Launch Mode, the ADCS shall be capable of pointing the Solar Array as follows:

[**Redacted**]

3.2.1.7.2.12    Wideband Antenna

While in Cruise Mode, Earth or Fixed Frame Imaging Mode, or maneuvering to/from Images, the ADCS shall be capable of pointing the Wideband Antenna as follows:

[**Redacted**]

3.2.1.7.3    Propulsion

3.2.1.7.3.1    Minimum Delta-V Capability

The Propulsion subsystem shall provide at least [**Redacted**]

3.2.1.7.3.2    Propellant Budget

The SSI shall develop and maintain a [**Redacted**]

3.2.1.7.3.3    Inefficiencies of Operation

The propellant budget shall, at a minimum, account for the following inefficiencies of operation:

[**Redacted**]

 

 

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3.2.1.7.3.4    Thruster Orientation

[**Redacted**]

3.2.1.7.3.5    [**Redacted**]

[**Redacted**]

3.2.1.7.4    Flight Software

3.2.1.7.4.1    [**Redacted**]

The Flight Software shall provide the capability to [**Redacted**] .

3.2.1.7.4.2    Modularity

The design of the Satellite flight software shall be [**Redacted**] .

3.2.1.7.4.2.1    Module Size

The patching or replacing of any single Satellite flight software module shall not require more than [**Redacted**] or the [**Redacted**] shall be uploadable in no more than [**Redacted**] split across multiple contacts [**Redacted**].

3.2.1.7.4.3    Parameterization

The design of the Satellite flight software shall incorporate parameterization to support operational flexibility and command versatility.

[**Redacted**]

3.2.1.7.4.3.1    Parameter Range and Resolution

Parameters shall have enough range and resolution to permit operation of the Satellite to the requirements of this specification without having to patch the Satellite Flight software.

3.2.1.7.4.3.2    [**Redacted**]

[**Redacted**]

3.2.1.7.4.4    [**Redacted**]

[**Redacted**]

3.2.1.7.4.4.1    [**Redacted**]

[**Redacted**]

3.2.1.7.4.4.2    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.4.5    [**Redacted**]

[**Redacted**]

3.2.1.7.4.6    [**Redacted**]

[**Redacted**]

3.2.1.7.4.7    [**Redacted**]

[**Redacted**]

3.2.1.7.4.7.1    [**Redacted**]

[**Redacted**]

3.2.1.7.4.8    [**Redacted**]

[**Redacted**]

3.2.1.7.4.9    [**Redacted**]

[**Redacted**]

3.2.1.7.4.10    [**Redacted**]

[**Redacted**]

3.2.1.7.4.11    [**Redacted**]

[**Redacted**]

3.2.1.7.5    C&DH

3.2.1.7.5.1    Commands

3.2.1.7.5.1.1    Command Formats

Commands shall be formatted as specified in the [**Redacted**] .

3.2.1.7.5.1.2    Command Length

Commands shall be [**Redacted**] to assure compatibility with [**Redacted**] with [**Redacted**] and [**Redacted**] .

3.2.1.7.5.1.3    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.4    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.5.1.5    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.6    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.7    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.8    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.9    [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.10    Unique Satellite Identification

The Satellite identification used for command verification and acceptance shall be unique for each redundancy string and shall be different than IDs used on previous DigitalGlobe satellites.

[**Redacted**]

3.2.1.7.5.2    State-of-Health Telemetry

3.2.1.7.5.2.1    Telemetry Content

The C&DH subsystem shall collect and format housekeeping telemetry for the Spacecraft Bus [**Redacted**] sufficient to provide the following capabilities on the ground:

[**Redacted**]

3.2.1.7.5.2.2    Telemetry Format

The C&DH subsystem shall format and transmit the [**Redacted**] as follows:

[**Redacted**]

3.2.1.7.5.2.3    [**Redacted**]

[**Redacted**]

3.2.1.7.5.2.4    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.5.2.5    [**Redacted**]

[**Redacted**]

3.2.1.7.5.2.6    Unique Satellite Identification

All telemetry data shall periodically include a Satellite identification that is different than IDs used on previous DigitalGlobe satellites.

[**Redacted**]

3.2.1.7.5.2.7    Storage Capacity

The C&DH subsystem shall be capable of storing at least 36 hours of telemetry at an average rate of [**Redacted**] .

[**Redacted**]

3.2.1.7.5.2.8    [**Redacted**]

[**Redacted**]

3.2.1.7.5.2.9    [**Redacted**]

[**Redacted**]

3.2.1.7.5.3    [**Redacted**]

[**Redacted**]

3.2.1.7.5.4    Ancillary Data

During normal operations, the C&DH subsystem shall collect Ancillary Data from Bus and Instrument equipment and forward it [**Redacted**]

3.2.1.7.5.4.1    Standard Content

The standard content of the two Ancillary Data streams shall be as defined in [**Redacted**] .

[**Redacted**]

 

 

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Table 3-4 Standard Ancillary Data Content

 

Data Type

  

Description

  

Frequency

  

Minimum Rate

Continuous Ancillary Data Stream

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]

[**Redacted**]

Image Ancillary Data Stream

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

3.2.1.7.5.4.2    Format

The C&DH subsystem shall format the [**Redacted**]

3.2.1.7.5.4.3    Redefinable Content

It shall be possible to independently re-define the content of [**Redacted**] , subject to data bandwidth constraints.

[**Redacted**]

3.2.1.7.5.4.4    [**Redacted**]

[**Redacted**]

3.2.1.7.5.4.5    Data Transfer

The C&DH subsystem shall transfer the Ancillary Data to the MDR as follows:

[**Redacted**]

3.2.1.7.5.4.6    [**Redacted**]

[**Redacted**]

3.2.1.7.5.4.7    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.5.5    Command & Telemetry Protocol

The satellite shall meet the requirements for the satellite command and telemetry protocol as specified in the [**Redacted**]

3.2.1.7.6    Narrowband Communications

3.2.1.7.6.1    Command Uplink

3.2.1.7.6.1.1    Uplink Bit Rate

The Command Uplink shall operate at one of two selectable rates, including all headers and other formatting, as follows:

[**Redacted**]

3.2.1.7.6.1.2    Bit Error Rate

The Command Uplink shall provide a bit error rate not to exceed [**Redacted**] .

3.2.1.7.6.1.3    Availability

The Command Uplink shall provide an availability of at least [**Redacted**] .

3.2.1.7.6.1.4    Elevation Angle

The Command Uplink shall operate at elevation angles of [**Redacted**] .

3.2.1.7.6.1.5    Link Margin

The Command Uplink shall meet all performance and functional requirements specified herein at EOL with a link margin of at least [**Redacted**] .

3.2.1.7.6.1.6    [**Redacted**]

[**Redacted**]

3.2.1.7.6.1.7    Modulation

The Command Uplink shall be modulated using [**Redacted**] .

3.2.1.7.6.1.8    Radio Frequency

The nominal Command Uplink carrier frequency shall be [**Redacted**] .

3.2.1.7.6.1.9    Antenna Coverage

Command Uplink antenna coverage shall be provided as follows:

[**Redacted**]

c) Provides realistic allowances for blockages by the Instrument.

3.2.1.7.6.1.10    Antenna Polarization

The Command Uplink antenna shall use [**Redacted**] .

3.2.1.7.6.1.11    Idle Patterns

[**Redacted**]

3.2.1.7.6.2    Telemetry Downlink

3.2.1.7.6.2.1     [**Redacted**] Telemetry Bit Rate

The Telemetry Downlink shall be at the following selectable rates, including all header and other formatting required to structure the commands:

[**Redacted**]

 

 

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3.2.1.7.6.2.2     [**Redacted**] Telemetry Bit Rate

The Telemetry Downlink shall be at a rate of [**Redacted**].

3.2.1.7.6.2.3    Bit Error Rate

The Telemetry Downlink shall provide a bit error rate not to exceed [**Redacted**] .

3.2.1.7.6.2.4    Availability

The Telemetry Downlink shall provide an availability of at least [**Redacted**] .

3.2.1.7.6.2.5    Elevation Angle

The Telemetry Downlink shall operate at elevation angles of [**Redacted**] .

3.2.1.7.6.2.6    Link Margin

The Telemetry Downlink shall meet all performance and functional requirements specified herein at EOL with a link margin of at least [**Redacted**] .

3.2.1.7.6.2.7    [**Redacted**]

[**Redacted**]

3.2.1.7.6.2.8    [**Redacted**]

[**Redacted**]

3.2.1.7.6.2.9    Modulation

 

a) The Telemetry Downlink shall use [**Redacted**] modulation as specified in the [**Redacted**] .

 

b) Any processing of the original data stream before transmission shall result in a [**Redacted**] .

3.2.1.7.6.2.10    Radio Frequency

The nominal Telemetry Downlink carrier frequency shall be [**Redacted**] .

3.2.1.7.6.2.11    Antenna Coverage: Special / Contingency Modes

 

a) Telemetry Downlink antenna coverage shall support all RF performance requirements specified herein (e.g. all downlink rates, both real-time and stored telemetry, BER, availability, elevation angle, etc.) with a [**Redacted**] when transmitting within [**Redacted**] .

 

b) A minimum elevation angle up to [**Redacted**] shall be permitted.

 

c) It shall be permissible to require ground commands in order to [**Redacted**] for operation in this mode, for example to switch from [**Redacted**] to [**Redacted**]

3.2.1.7.6.2.12    Antenna Coverage: Normal Operating Modes

Telemetry Downlink antenna coverage shall support all RF performance requirements specified herein (e.g. all downlink rates, BER, link margin, etc.) as follows:

[**Redacted**]

 

 

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3.2.1.7.6.2.13    Antenna Polarization

The Telemetry Downlink antenna shall use [**Redacted**]

3.2.1.7.6.2.14    Adjustable RF Output Power

The Telemetry Downlink shall provide the capability to adjust RF output power levels by ground command (real-time or stored), in increments sufficient to meet the link margin and interference limits specified in Sections 3.2.1.7.6.2.6 Link Margin and 3.1.2.1 Non-interference with Outside Systems, at any altitude over the range specified in Section 3.2.1.1.2.1 General Orbit Compatibility.

[**Redacted**]

3.2.1.7.7    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.1    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.2    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.3    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.4    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.5    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.6    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.7.1.7    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.8    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.9    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.10    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.11    [**Redacted**]

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3.2.1.7.7.1.12    [**Redacted**]

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3.2.1.7.7.1.13    [**Redacted**]

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3.2.1.7.7.1.14    [**Redacted**]

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3.2.1.7.7.1.15    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.16    [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.17    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.7.2    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.1    [**Redacted**]

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3.2.1.7.7.2.2    [**Redacted**]

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3.2.1.7.7.2.3    [**Redacted**]

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3.2.1.7.7.2.4    [**Redacted**]

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3.2.1.7.7.2.5    [**Redacted**]

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3.2.1.7.7.2.6    [**Redacted**]

3.2.1.7.7.2.7    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.8    [**Redacted**]

3.2.1.7.7.2.9    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.10    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.11    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.12    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.7.2.13    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.14    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.15    [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.16    [**Redacted**]

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3.2.1.7.7.2.17    [**Redacted**]

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3.2.1.7.7.2.18    [**Redacted**]

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3.2.1.7.7.2.19    [**Redacted**]

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3.2.1.7.7.2.20    [**Redacted**]

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3.2.1.7.7.2.21    [**Redacted**]

[**Redacted**]

3.2.1.7.8    EPDS

3.2.1.7.8.1    Functional Requirements

The EPDS shall perform the following functions under the Conditions and Operational Scenarios specified below:

 

a) Provide sufficient power to all Spacecraft Bus and Instrument equipment to

[**Redacted**]

3.2.1.7.8.2    Realistic Worst Case Conditions

EPDS performance shall be evaluated under realistic worst-case conditions [**Redacted**], including, but not limited to:

[**Redacted**]

 

 

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3.2.1.7.8.3    Operational Scenarios

EPDS performance shall be evaluated using the following operational scenarios for the range of orbits specified in Section 3.2.1.1.2.1 General Orbit Compatibility. For requirements verification, it is acceptable to perform in-depth analysis [**Redacted**]

3.2.1.7.8.4    Instrument Power

The EPDS shall provide power to the Instrument as specified in Section 3.1.3.1.3 Power Interfaces.

3.2.1.7.8.5    [**Redacted**]

[**Redacted**]

3.2.1.7.8.6    [**Redacted**]

[**Redacted**]

3.2.1.7.8.7    [**Redacted**]

[**Redacted**]

3.2.1.7.8.8    [**Redacted**]

[**Redacted**]

3.2.1.7.9    Structures and Mechanisms

3.2.1.7.9.1    Functional Requirements

The Structure shall perform the following functions:

 

a) Support all Bus and [**Redacted**] equipment through all mission phases, including pre-launch, launch, initialization, normal operations, and EOL disposal.

 

b) [**Redacted**]

3.2.1.7.9.2    Factors and Margins of Safety

[**Redacted**]

3.2.1.7.9.3    Mechanisms

3.2.1.7.9.3.1    [**Redacted**]

[**Redacted**]

3.2.1.7.9.3.2    Accessibility

Deployment devices shall be accessible with minimum disturbance to the relative position of the mechanisms or their thermal control hardware.

3.2.1.7.9.3.3    Thermal Constraints

There shall be no thermal constraints against the operation of any mechanism at any time during the Satellite Mission Life such that:

[**Redacted**]

 

 

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3.2.1.7.9.3.4    [**Redacted**]

[**Redacted**]

3.2.1.7.9.3.5    [**Redacted**]

[**Redacted**]

3.2.1.7.10    Thermal Control

3.2.1.7.10.1    Functional Requirements

The Thermal Control subsystem shall autonomously perform the following functions under the Conditions and Operational Scenarios specified below:

[**Redacted**]

3.2.1.7.10.2    Realistic Worst Case Conditions

Thermal Control Subsystem performance shall be evaluated under realistic worst-case conditions (i.e. precluding combinations of conditions that can not physically occur), including, but not limited to:

[**Redacted**]

3.2.1.7.10.3    Operational Scenarios

The Thermal Control Subsystem performance shall be evaluated using the following operational scenarios for the range of orbits specified in Section 3.2.1.1.2.1 General Orbit Compatibility. For requirements verification, it is acceptable to perform in-depth analysis [**Redacted**]

3.2.1.7.10.4    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.1    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.2    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.3    [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.4    [**Redacted**]

[**Redacted**]

 

 

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3.2.1.7.10.4.5    [**Redacted**]

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3.2.1.7.10.4.6    [**Redacted**]

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3.2.1.7.10.4.7    [**Redacted**]

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3.2.1.7.10.4.8    [**Redacted**]

3.2.1.7.10.4.9    [**Redacted**]

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3.2.1.7.10.5    [**Redacted**]

[**Redacted**]

3.2.1.7.11    Direct Tasking

The Satellite shall provide Direct Tasking capabilities as specified below, with the following definitions of key terms:

[**Redacted**]

3.2.1.7.11.1    [**Redacted**]

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3.2.1.7.11.1.1    [**Redacted**]

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3.2.1.7.11.1.2    [**Redacted**]

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3.2.1.7.11.1.3    [**Redacted**]

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3.2.1.7.11.1.4    [**Redacted**]

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3.2.1.7.11.1.5    [**Redacted**]

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3.2.1.7.11.1.6    [**Redacted**]

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3.2.1.7.11.1.7    [**Redacted**]

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3.2.1.7.11.2    [**Redacted**]

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3.2.1.7.11.2.1    [**Redacted**]

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3.2.1.7.11.2.2    [**Redacted**]

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3.2.1.7.11.2.3    [**Redacted**]

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3.2.1.7.11.2.4    [**Redacted**]

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3.2.1.7.11.2.5    [**Redacted**]

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3.2.1.7.11.3    [**Redacted**]

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3.2.1.7.11.3.1    [**Redacted**]

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3.2.1.7.11.3.2    [**Redacted**]

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3.2.1.7.11.3.3    [**Redacted**]

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3.2.1.7.11.3.4    [**Redacted**]

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3.2.1.7.11.3.5    [**Redacted**]

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3.2.1.7.11.3.6    [**Redacted**]

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3.2.1.7.11.3.7    [**Redacted**]

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3.2.1.7.11.3.8    [**Redacted**]

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3.2.1.7.11.3.9    [**Redacted**]

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3.2.1.7.11.3.10    [**Redacted**]

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3.2.1.7.11.4    [**Redacted**]

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3.2.1.7.11.4.1    [**Redacted**]

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3.2.1.7.11.4.2    [**Redacted**]

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3.2.1.7.11.4.3    [**Redacted**]

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3.2.1.7.11.4.4    [**Redacted**]

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3.2.1.7.11.4.5    [**Redacted**]

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3.2.1.7.11.4.6    [**Redacted**]

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3.2.1.7.11.4.7    [**Redacted**]

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3.2.1.7.11.4.8    [**Redacted**]

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3.2.1.7.11.4.9    [**Redacted**]

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3.2.1.7.11.5    [**Redacted**]

3.2.1.7.11.5.1    [**Redacted**]

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3.2.1.7.11.5.2    [**Redacted**]

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3.2.1.7.11.5.3    [**Redacted**]

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3.2.1.7.11.5.4    [**Redacted**]

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3.2.1.7.11.5.5    [**Redacted**]

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3.2.1.7.11.5.6    [**Redacted**]

[**Redacted**]

3.2.1.7.11.5.7    [**Redacted**]

[**Redacted**]

3.2.2    Physical Characteristics

3.2.2.1    Size Constraints

The size of the integrated Satellite shall be compatible with the specified Launch Vehicles and Shipping Constraints.

3.2.2.2    Mass Constraints

The total Satellite mass (including all parts of the Launch Vehicle adapter / separation mechanism that remain with the Satellite after separation) shall not exceed the limits established by the [**Redacted**] and the [**Redacted**] .

[**Redacted**]

3.2.2.3    Shipping Constraints

The Satellite and associated Ground Support Equipment (GSE), including the shipping container, shall be designed to allow transportation to the Launch Site via the [**Redacted**] or by [**Redacted**] and [**Redacted**] .

3.2.3    Reliability

3.2.3.1    End of Life Ps

[**Redacted**]

3.2.3.2    [**Redacted**]

[**Redacted]

3.2.3.3    [**Redacted**]

[**Redacted**]

3.2.3.4    Cycle-Limited Items

Items whose life is limited by the total number of operating cycles shall meet all on-orbit performance requirements after operating for [**Redacted**] the predicted number of cycles, including all cycles incurred during both the Mission Life and during ground testing. Cycle-limited items shall include at a minimum:

[**Redacted**]

3.2.3.4.1    [**Redacted**]

[**Redacted**]

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

  Use or disclosure of data is subject to the restriction on the title page of this  document.    44


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 7.0: 13 Sept 2011

 

 

3.2.3.4.2    [**Redacted**]

[**Redacted**]

3.2.4    Availability and Maintainability

3.2.4.1    Fault Recovery Timeline

The Satellite equipment provided by the SSI shall be designed to allow recovery from any fault conditions and single event upsets or latch-ups within [**Redacted**] of ground operator intervention, with the exception of [**Redacted**] , which shall take no longer than [**Redacted**]

3.2.4.2    Environmental Conditions

The Satellite shall meet all functional and performance requirements after exposure to the following environments.

3.2.4.2.1    Launch Induced Environments

[**Redacted**]

3.2.4.2.2    On-Orbit Environments

On-orbit environments shall be consistent with operation in the Mission Orbit for the Mission Life and shall include, at a minimum:

[**Redacted**]

3.2.4.2.3    Pre-Launch Environments

Except for any specific testing aimed at verifying the design margins, the Satellite shall not be subjected to any environments that exceed the launch and on-orbit environments. This includes integration and test activities, transportation, launch site processing, and the period the Satellite is within the Launch Vehicle Fairing prior to launch.

 

3.3 Satellite Design and Construction

3.3.1    General

The Satellite Design and Construction shall be performed per standard SSI practices in accordance with the Environmental Design and Test Specification and the DigitalGlobe Space Segment Specification Addendum, including at a minimum the following items:

[**Redacted**]

3.3.2    SEUs

[**Redacted**]

3.3.3    Immunity to Latch-Up

[**Redacted**]

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

  Use or disclosure of data is subject to the restriction on the title page of this  document.    45


LOGO    WorldView-3 Satellite Specification
   Doc’t # 10329655
   Rev 7.0: 13 Sept 2011

 

 

3.3.4    Cleanliness and Contamination Control

[**Redacted**]

3.3.4.1    [**Redacted**]

[**Redacted**]

3.3.4.2    [**Redacted**]

[**Redacted**]

3.3.4.3    [**Redacted**]

[**Redacted**]

3.3.4.4    [**Redacted**]

[**Redacted**]

3.3.5    Safety

The Satellite shall be designed to allow for safe handling, operation, transportation, fuel loading and pressurization through all mission phases. It shall comply with the specific requirements of [**Redacted**] , including at a minimum:

[**Redacted**]

3.3.6    [**Redacted**]

[**Redacted**]

 

4. VERIFICATION

Requirements verification shall be performed per standard SSI practices, in accordance with the DigitalGlobe Space Segment Specification Addendum and the Statement of Work.

 

5. QUALITY ASSURANCE

Quality Assurance shall be performed per standard SSI practices, in accordance with the DigitalGlobe Space Segment Specification Addendum and the Statement of Work.

 

 

ITAR-Controlled Document

DigitalGlobe Proprietary and Confidential

  Use or disclosure of data is subject to the restriction on the title page of this  document.    46


Attachment 3

WorldView 3 Payment Milestone Schedule, Rev 3.0

Dated 9 Sept 2011


WorldView 3 Payment Milestone Schedule

Exhibit 3 to WV3 Satellite Agreement # 60150

 

Item
#

  

Invoice Date

  

Line
Item

  

Description

   Completed   

Milestone

Value

  

Cumulative
Milestones

  

Termination
Liability

1    [**Redacted**]       Milestone 1 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]            
2    [**Redacted**]       Milestone 2 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
3    [**Redacted**]       Milestone 3 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
4    [**Redacted**]       Milestone 4 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
5    [**Redacted**]       Milestone 5 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
6    [**Redacted**]       Milestone 6 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
7    [**Redacted**]       Milestone 7 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
8    [**Redacted**]       Milestone 8 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      
9    [**Redacted**]       Milestone 9 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      9a    [**Redacted**]       [**Redacted**]      
      9b    [**Redacted**]       [**Redacted**]      
      9c    [**Redacted**]       [**Redacted**]      
      9d    [**Redacted**]       [**Redacted**]      
10    [**Redacted**]       Milestone 10 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      10a    [**Redacted**]       [**Redacted**]      
      10b    [**Redacted**]       [**Redacted**]      
      10c    [**Redacted**]       [**Redacted**]      
      10d    [**Redacted**]       [**Redacted**]      


11    [**Redacted**]       Milestone 11 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      11a    [**Redacted**]       [**Redacted**]      
      11b    [**Redacted**]       [**Redacted**]      
      11c    [**Redacted**]       [**Redacted**]      
      11d    [**Redacted**]       [**Redacted**]      
      11e    [**Redacted**]       [**Redacted**]      
12    [**Redacted**]       Milestone 12 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      12a    [**Redacted**]       [**Redacted**]      
      12b    [**Redacted**]       [**Redacted**]      
      12c    [**Redacted**]       [**Redacted**]      
      12d    [**Redacted**]       [**Redacted**]      
      12e    [**Redacted**]       [**Redacted**]      
13    [**Redacted**]       Milestone 13 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      13a    [**Redacted**]       [**Redacted**]      
      13b    [**Redacted**]       [**Redacted**]      
      13c    [**Redacted**]       [**Redacted**]      
      13d    [**Redacted**]       [**Redacted**]      
      13e    [**Redacted**]       [**Redacted**]      
      13f    [**Redacted**]       [**Redacted**]      
14    [**Redacted**]       Milestone 14 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      14a    [**Redacted**]       [**Redacted**]      
      14b    [**Redacted**]       [**Redacted**]      
      14c    [**Redacted**]       [**Redacted**]      
      14d    [**Redacted**]       [**Redacted**]      
      14e    [**Redacted**]       [**Redacted**]      
15    [**Redacted**]       Milestone 15 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      15a    [**Redacted**]       [**Redacted**]      
      15b    [**Redacted**]       [**Redacted**]      
      15c    [**Redacted**]       [**Redacted**]      
      15d    [**Redacted**]       [**Redacted**]      
      15e    [**Redacted**]       [**Redacted**]      
      15f    [**Redacted**]       [**Redacted**]      
16    [**Redacted**]       Milestone 16 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      16a    [**Redacted**]       [**Redacted**]      
      16b    [**Redacted**]       [**Redacted**]      
      16c    [**Redacted**]       [**Redacted**]      
      16d    [**Redacted**]       [**Redacted**]      
      16e    [**Redacted**]       [**Redacted**]      
17    [**Redacted**]       Milestone 17 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      17a    [**Redacted**]       [**Redacted**]      
      17b    [**Redacted**]       [**Redacted**]      
      17c    [**Redacted**]       [**Redacted**]      
      17d    [**Redacted**]       [**Redacted**]      
18    [**Redacted**]       Milestone 18 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      18a    [**Redacted**]       [**Redacted**]      
      18b    [**Redacted**]       [**Redacted**]      
      18c    [**Redacted**]       [**Redacted**]      
      18d    [**Redacted**]       [**Redacted**]      


19    [**Redacted**]       Milestone 19 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      19a    [**Redacted**]       [**Redacted**]      
      19b    [**Redacted**]       [**Redacted**]      
      19c    [**Redacted**]       [**Redacted**]      
      19d    [**Redacted**]       [**Redacted**]      
      19e    [**Redacted**]       [**Redacted**]      
20    [**Redacted**]       Milestone 20 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      20a    [**Redacted**]       [**Redacted**]      
      20b    [**Redacted**]       [**Redacted**]      
      20c    [**Redacted**]       [**Redacted**]      
      20d    [**Redacted**]       [**Redacted**]      
21    [**Redacted**]       Milestone 21 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      21a    [**Redacted**]       [**Redacted**]      
      21b    [**Redacted**]       [**Redacted**]      
      21c    [**Redacted**]       [**Redacted**]      
      21d    [**Redacted**]       [**Redacted**]      
      21e    [**Redacted**]       [**Redacted**]      
22    [**Redacted**]       Milestone 22 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      22a    [**Redacted**]       [**Redacted**]      
      22b    [**Redacted**]       [**Redacted**]      
      22c    [**Redacted**]       [**Redacted**]      
      22d    [**Redacted**]       [**Redacted**]      
      22e    [**Redacted**]       [**Redacted**]      
23    [**Redacted**]       Milestone 23 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      23a    [**Redacted**]       [**Redacted**]      
      23b    [**Redacted**]       [**Redacted**]      
      23c    [**Redacted**]       [**Redacted**]      
      23d    [**Redacted**]       [**Redacted**]      
      23e    [**Redacted**]       [**Redacted**]      
      23f    [**Redacted**]       [**Redacted**]      
24    [**Redacted**]       Milestone 24 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      24a    [**Redacted**]       [**Redacted**]      
      24b    [**Redacted**]       [**Redacted**]      
      24c    [**Redacted**]       [**Redacted**]      
      24d    [**Redacted**]       [**Redacted**]      
      24e    [**Redacted**]       [**Redacted**]      
25    [**Redacted**]       Milestone 25 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      25a    [**Redacted**]       [**Redacted**]      
      25b    [**Redacted**]       [**Redacted**]      
      25c    [**Redacted**]       [**Redacted**]      
      25d    [**Redacted**]       [**Redacted**]      
26    [**Redacted**]       Milestone 26 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      26a    [**Redacted**]       [**Redacted**]      
      26b    [**Redacted**]       [**Redacted**]      
      26c    [**Redacted**]       [**Redacted**]      
      26d    [**Redacted**]       [**Redacted**]      
      26e    [**Redacted**]       [**Redacted**]      


27    [**Redacted**]       Milestone 27 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      27a    [**Redacted**]       [**Redacted**]      
      27b    [**Redacted**]       [**Redacted**]      
      27c    [**Redacted**]       [**Redacted**]      
      27d    [**Redacted**]       [**Redacted**]      
28    [**Redacted**]       Milestone 28 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      28a    [**Redacted**]       [**Redacted**]      
      28b    [**Redacted**]       [**Redacted**]      
      28c    [**Redacted**]       [**Redacted**]      
      28d    [**Redacted**]       [**Redacted**]      
      28e    [**Redacted**]       [**Redacted**]      
      28f    [**Redacted**]       [**Redacted**]      
29    [**Redacted**]       Milestone 29 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      29a    [**Redacted**]       [**Redacted**]      
      29b    [**Redacted**]       [**Redacted**]      
      29c    [**Redacted**]       [**Redacted**]      
      29d    [**Redacted**]       [**Redacted**]      
      29e    [**Redacted**]       [**Redacted**]      
30    [**Redacted**]       Milestone 30 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      30a    [**Redacted**]       [**Redacted**]      
      30b    [**Redacted**]       [**Redacted**]      
      30c    [**Redacted**]       [**Redacted**]      
      30d    [**Redacted**]       [**Redacted**]      
31    [**Redacted**]       Milestone 31 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      31a    [**Redacted**]       [**Redacted**]      
      31b    [**Redacted**]       [**Redacted**]      
      31c    [**Redacted**]       [**Redacted**]      
      31d    [**Redacted**]       [**Redacted**]      
32    [**Redacted**]       Milestone 32 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      32a    [**Redacted**]       [**Redacted**]      
      32b    [**Redacted**]       [**Redacted**]      
      32c    [**Redacted**]       [**Redacted**]      
      32d    [**Redacted**]       [**Redacted**]      
33    [**Redacted**]       Milestone 33 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      33a    [**Redacted**]       [**Redacted**]      
      33b    [**Redacted**]       [**Redacted**]      
      33c    [**Redacted**]       [**Redacted**]      
      33d    [**Redacted**]       [**Redacted**]      
      33e    [**Redacted**]       [**Redacted**]      
34    [**Redacted**]       Milestone 34 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      34a    [**Redacted**]       [**Redacted**]      
      34b    [**Redacted**]       [**Redacted**]      
      34c    [**Redacted**]       [**Redacted**]      
      34d    [**Redacted**]       [**Redacted**]      
      34e    [**Redacted**]       [**Redacted**]      
      34f    [**Redacted**]       [**Redacted**]      
35    [**Redacted**]       Milestone 35 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      35a    [**Redacted**]       [**Redacted**]      
      35b    [**Redacted**]       [**Redacted**]      
      35c    [**Redacted**]       [**Redacted**]      
      35d    [**Redacted**]       [**Redacted**]      
      35e    [**Redacted**]       [**Redacted**]      


36    [**Redacted**]       Milestone 36 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      36a    [**Redacted**]       [**Redacted**]      
      36b    [**Redacted**]       [**Redacted**]      
      36c    [**Redacted**]       [**Redacted**]      
      36d    [**Redacted**]       [**Redacted**]      
37    [**Redacted**]       Milestone 37 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      37a    [**Redacted**]       [**Redacted**]      
      37b    [**Redacted**]       [**Redacted**]      
      37c    [**Redacted**]       [**Redacted**]      
      37d    [**Redacted**]       [**Redacted**]      
      37e    [**Redacted**]       [**Redacted**]      
38    [**Redacted**]       Milestone 38 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      38a    [**Redacted**]       [**Redacted**]      
      38b    [**Redacted**]       [**Redacted**]      
      38c    [**Redacted**]       [**Redacted**]      
      38d    [**Redacted**]       [**Redacted**]      
      38e    [**Redacted**]       [**Redacted**]      
39    [**Redacted**]       Milestone 39 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      39a    [**Redacted**]       [**Redacted**]      
      39b    [**Redacted**]       [**Redacted**]      
      39c    [**Redacted**]       [**Redacted**]      
      39d    [**Redacted**]       [**Redacted**]      
40    [**Redacted**]       Milestone 40 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      40a    [**Redacted**]       [**Redacted**]      
      40b    [**Redacted**]       [**Redacted**]      
      40c    [**Redacted**]       [**Redacted**]      
      40d    [**Redacted**]       [**Redacted**]      
      40e    [**Redacted**]       [**Redacted**]      
41    [**Redacted**]       Milestone 41 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      41a    [**Redacted**]       [**Redacted**]      
      41b    [**Redacted**]       [**Redacted**]      
      41c    [**Redacted**]       [**Redacted**]      
      41d    [**Redacted**]       [**Redacted**]      
42    [**Redacted**]       Milestone 42 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      42a    [**Redacted**]       [**Redacted**]      
      42b    [**Redacted**]       [**Redacted**]      
      42c    [**Redacted**]       [**Redacted**]      
      42d    [**Redacted**]       [**Redacted**]      
43    [**Redacted**]       Milestone 43 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      43a    [**Redacted**]       [**Redacted**]      
      43b    [**Redacted**]       [**Redacted**]      
      43c    [**Redacted**]       [**Redacted**]      
      43d    [**Redacted**]       [**Redacted**]      
      43e    [**Redacted**]       [**Redacted**]      
44    [**Redacted**]       Milestone 44 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      44a    [**Redacted**]       [**Redacted**]      
      44b    [**Redacted**]       [**Redacted**]      
      44c    [**Redacted**]       [**Redacted**]      


45    [**Redacted**]       Milestone 45 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      45a    [**Redacted**]         [**Redacted**]         
      45b    [**Redacted**]         [**Redacted**]         
46    [**Redacted**]       Milestone 46 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      46a    [**Redacted**]         [**Redacted**]         
      46b    [**Redacted**]         [**Redacted**]         
      46c    [**Redacted**]         [**Redacted**]         
      46d    [**Redacted**]         [**Redacted**]         
47    [**Redacted**]       Milestone 47 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      47a    [**Redacted**]         [**Redacted**]         
48    [**Redacted**]       Milestone 48 Total Value         [**Redacted**]         [**Redacted**]         [**Redacted**]   
      48a    [**Redacted**]         [**Redacted**]         
      48b    [**Redacted**]         [**Redacted**]         
      48c    [**Redacted**]         [**Redacted**]         
         TOTALS           $ 213,277,399       $ 213,277,399       $ 213,277,399   


Attachment 4

WorldView 3 Spacecraft Simulator Specification, Rev 1.0

Dated 9 Sept 2011

[**Redacted**]


Attachment 5

[**Redacted**]

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.

Exhibit 10.5.4

FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

Amendment No. 5

To the

WorldView 3 Satellite Purchase Agreement #60150

This Amendment No. 5 (“Amendment”) to WorldView 3 Satellite Purchase Agreement #60150 (the “Agreement”) is entered into by and between DigitalGlobe, Inc. (“DigitalGlobe”), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, CO 80503; and Ball Aerospace & Technologies Corp., a Delaware corporation with its principal offices located at 1600 Commerce Street, Boulder, CO 80301 (“BATC”). As used in this Agreement, “Party” means either DigitalGlobe or BATC, as appropriate, and “Parties” means DigitalGlobe and BATC.

WHEREAS, DigitalGlobe and BATC entered into the WorldView 3 Satellite Purchase Agreement #60150 (“Agreement”) on September 1, 2010;

Now , THEREFORE, the parties hereby agree to amend the Agreement to incorporate the following Engineering Change Proposals (“ECP”):

 

1. ECP 013: [**Redacted**] .

This change directs BATC to [**Redacted**] .

Price: The Firm-Fixed Price for the [**Redacted**] is [**Redacted**].

 

2. ECP 014: Document Updates

This change updates four specifications currently under contract. In addition the Payment Milestone Schedule, Exhibit 3, has been updated. This change also adds a new document, the [**Redacted**] .

Therefore, this Amendment updates and updates the following documents which are provided as Attachments 1-5 to the Agreement.

 

  a. Exhibit 1 to the Agreement, titled “Statement of Work for the WorldView 3 Satellite—10329656, Rev 3.0,” and dated 9 September 2011, is replaced in its entirety by the updated version “Statement of Work for the WorldView 3 Satellite—10329656, Rev 4.0,” dated 24 October 2011, included as Attachment 1 to this Amendment; and

 

  b. Exhibit 2 to the Agreement, titled “DigitalGlobe WorldView 3 Satellite Specification – 10329655, Rev 7.0,” and dated 13 September 2011, is replaced in its entirety by the updated version “WorldView-3 Satellite Specification – 10329655, Rev 8.0”, dated 2 November 2011, included as Attachment 2 to this Amendment; and

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


  c. Exhibit 3 to the Agreement, titled “WorldView 3 Payment Milestone Schedule – 10329669, Rev 3.0” and dated 9 September 2011, is replaced in its entirety by the updated version “WorldView 3 Payment Milestone Schedule, Rev—10329669, Rev 4.0,” dated 24 October 2011, included as Attachment 3 to this Amendment; and

 

  d. “WorldView-3 Spacecraft Simulator Specification – 10258368, Rev 1.0”, and dated 9 September 2011, is replaced in its entirety by the document “WorldView-3 Spacecraft Simulator Specification – 10258368, Rev 3.0”, dated 24 October 2011, included as Attachment 4 to this Amendment.

 

  e. [**Redacted**]

 

  f. [**Redacted**]

SUMMARY

The value for these ECPs is $4,000,000, outlined in the following table:

 

Change #

  

Change Description

   $  
013    [**Redacted**]    $ 4,000,000.00   
     

 

 

 
014    Documentation Updates    $ 0.00   
     

 

 

 
   TOTAL    $ 4,000,000.00   
     

 

 

 

Contract Value Summary

 

Previous Contract Value

   $ 213,277,399.00   
  

 

 

 

ECPs

   $ 4,000,000.00   
  

 

 

 

New Contract Value

   $ 217,277,399.00   
  

 

 

 

Unless otherwise expressly provided herein, all other terms and conditions of the Agreement shall remain in full force and effect.

This Amendment No. 5 is hereby executed and agreed to by DigitalGlobe and BATC and shall be binding and effective as of the last date executed below.

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


 

Ball Aerospace & Technologies Corp.      DigitalGlobe, Inc.

[**Redacted**]                                                                                 

     /s/ Yancey Spruill

Signature

     Signature

[**Redacted**]                                                                                 

        

Name

     Name: Yancey Spruill

[**Redacted**]                                                                                 

        

Title

     Title: Chief Financial Officer

11/28/11

     11/28/11

Date

     Date

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


Attachment 1

Statement of Work for the WorldView3 Satellite, Rev 4.0

Dated 24 October 2011

 

DigitalGlobe Proprietary and Confidential

Use or disclosure of data is subject to the restriction on the title page of this document.


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

 

LOGO   

WV3 Satellite Statement of Work_

Doc Number 10329656

Exhibit 1 to Agreement 60150

Statement of Work

for the WorldView 3

Satellite

 

  Document Number    10329656
  Release Date:    Oct 24, 2011
  Issue/Revision:    Release 4.0
  Prepared by:    Brian Uzzle
  Approved by    Steve Linn

RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION

This document contains information proprietary and confidential to DigitalGlobe Incorporated, to its subsidiaries, or to a third party to whom DigitalGlobe Incorporated may have a legal obligation to protect such information from unauthorized disclosure, use or duplication. Any disclosure, use or duplication of this document or of any of the information contained herein for other than the specific purpose for which it was disclosed is expressly prohibited, except as DigitalGlobe Incorporated may otherwise agree to in writing. This document may only be used for the purpose for which it is provided. All copies of this document are the sole property of DigitalGlobe and will be returned promptly upon request.

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LOGO

 

WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

Change Record

 

Issue

  

Date

  

Section(s)

  

Description of Change

Initial

   20 Aug 2010       Initial Release

Rev 1

   7 Feb 2011    2.1    Updated references for Satellite Specification, Satellite Simulator Specification, and Instrument Specification
      3.1.b    Updated dates for Satellite Simulator releases and number of deliveries
      3.1.n    Added deliverable item [**Redacted**]
      3.1.o    Added deliverable item [**Redacted**] .
      13.8.1    Clarified WV3 simulator changes versus WV2 simulator [**Redacted**] .
      Attachment 1    Updated release dates for Satellite Simulator (LM-8), Satellite Simulator Documentation (LM-9), and Satellite Simulator Source Code (LM-10).
      Attachment 1    Updated [**Redacted**] (CFHW-1)

Rev 2

   14 Apr 2011    10.2.2    Updated [**Redacted**] , to be consistent with the date in Attachment 1 (CFHW-2)
      1.2, 2.1, 4.5.3.2.F, [**Redacted** ] , 11.4, 12.1, 12.2, 12.3, Attachment 2   

Changed launch vehicle baseline from Delta-2 to Atlas V.

Changed number of TIMs from 8 to 20.

Changed SLRR from [**Redacted**] to [**Redacted**] .

      3.1(b)    Updated delivery date for Simulator [**Redacted**] per Ball’s request.

Rev 3

   9 Sep 2011    1.1    Added definitions for [**Redacted**] .
      2.1    Added [**Redacted**] specification. Updated Satellite Spec and Simulator Spec versions. Changed BATC documents for Configuration and Data Management to current doc numbers and release versions. Updated Spaceport Systems International handbook version.
      3.1.a    Updated delivery date for Satellite, based on [**Redacted**]
      3.1.b    Updated delivery date for Simulator [**Redacted**] (LM-8) to match agreed upon dates.
      3.1.p, 3.1.q    Added deliverable items for [**Redacted**]
      4.2    Added [**Redacted**]
      4.5.3.1    Added [**Redacted**]
      4.5.3.2.F    Added [**Redacted**] specifics
      5.2.2    Added [**Redacted**] .
      5.3.9.1    Added [**Redacted**]
      5.3.11.i-m    Added [**Redacted**]
      6.2.2    Updated PCB Section to reflect virtual nature of PCBs
      9.3.b    Added [**Redacted**]
      9.3.g    Added [**Redacted**]
      10.5.9    Added [**Redacted**]
      13.5.g-l    Added [**Redacted**]
      Attachment 1    Added [**Redacted**] and CGSE-16. Changed [**Redacted**]
      n/a    Added Table of Contents

 

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i


LOGO

 

WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

Issue

  

Date

  

Section(s)

  

Description of Change

Rev 4

   3 Oct 2011    [**Redacted**]    [**Redacted**]

 

ITAR Controlled Document - DigitalGlobe Proprietary and Confidential

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ii


LOGO

 

WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

Issue

  

Date

  

Section(s)

  

Description of Change

 

ITAR Controlled Document - DigitalGlobe Proprietary and Confidential

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iii


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WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

Table of Contents

 

1.0

 

INTRODUCTION

     1   

1.1

 

D EFINITIONS

     1   

1.2

 

P ROGRAM O VERVIEW

     2   

2.0

 

DOCUMENTS

     3   

2.1

 

A PPLICABLE D OCUMENTS

     4   

2.2

 

R EFERENCE D OCUMENTS

     4   

3.0

 

CONTRACT DELIVERABLES

     5   

3.1

 

D ELIVERABLE I TEMS

     5   

3.2

 

D ELIVERABLE D ATA

     5   

3.3

 

D ELIVERABLE S ERVICES

     5   

4.0

 

PROGRAM MANAGEMENT

     6   

4.1

 

P ROGRAM P HILOSOPHY

     6   

4.2

 

BATC O RGANIZATION (CDIL PM-1)

     6   

4.3

 

D IGITAL G LOBE M ANAGEMENT

     6   

4.4

 

S PACE S EGMENT M ASTER P ROGRAM S CHEDULE (MPS) (CDIL PM-2)

     6   

4.4.1

 

General

     7   

4.4.2

 

Required Software

     7   

4.4.3

 

MPS Construction

     7   

4.4.4

 

Reports

     7   

4.5

 

M EETINGS & R EVIEWS

     7   

4.5.1

 

Weekly Status Meeting

     8   

4.5.2

 

Monthly Program Status Review

     8   

4.5.3

 

Program Reviews

     8   

4.5.4

 

Component/Subsystem Design Review Listing (CDIL PM-3)

     9   

4.5.5

 

Component/Subsystem Test Readiness / Data Review Listing (CDIL PM-4)

     10   

4.5.6

 

DigitalGlobe Meetings

     10   

4.6

 

D OCUMENTATION M ANAGEMENT

     10   

4.6.1

 

Access to Program Technical Data

     10   

4.6.2

 

Objective

     10   

4.6.3

 

Documentation Listing (CDIL PM-5)

     11   

4.6.4

 

Documentation Delivery

     11   

4.7

 

A CTION I TEM T RACKING (CDIL PM-6)

     11   

4.8

 

F INANCIAL M ANAGEMENT

     11   

4.8.1

 

Historical Record of Payments (CDIL PM-7)

     11   

4.8.2

 

Payments Forecast (CDIL PM-7)

     11   

4.9

 

C ONTRACT C HANGE C ONTROL

     11   

5.0

 

DESIGN

     13   

5.1

 

G ENERAL

     13   

5.2

 

W ORKING G ROUPS AND T RADE S TUDIES

     13   

5.2.1

 

Working Groups

     13   

5.2.2

 

Trade Studies

     13   

5.3

 

S ATELLITE D ESIGN D ATA

     13   

 

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WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

 

5.3.1

 

Satellite to Instrument Interface Control Document(s) (CDIL D-1)

     13   

5.3.2

 

Satellite to Ground Terminal Narrowband Link ICD (CDIL D-2)

     13   

5.3.3

 

Satellite to Ground Terminal Wideband Link ICD (CDIL D-3)

     13   

5.3.4

 

Satellite Environmental Design and Test Specification (EDTS) (CDIL D-4)

     13   

5.3.5

 

Contamination Control Plan(s) (CDIL D-5)

     13   

5.3.6

 

Satellite Level Requirements Verification/Compliance Matrix (CDIL D-6)

     13   

5.3.7

 

Box Level Requirements Verification/Compliance Matrix (CDIL D-7)

     14   

5.3.8

 

Drawings (CDIL D-8)

     14   

5.3.9

 

Performance Compliance and Risk Management

     14   

5.3.10

 

Subsystem Description Documents (CDIL D-11)

     14   

5.3.11

 

Analysis and reports

     15   

5.3.12

 

Other Interface Control Documents

     16   

5.3.13

 

Critical Items list (CDIL D-18)

     16   

5.3.14

 

Component Heritage Summary (CDIL D-19)

     16   

5.3.15

 

Engineering Reports (CDIL D-20)

     16   

5.3.16

 

Flight Software Source Code (CDIL D-21)

     16   

5.3.17

 

Composite Grounding Design (CDIL D-22)

     16   

5.3.18

 

Structural, Power, Thermal, and Reliability Analytical Models (CDIL D-23)

     16   

5.3.19

 

Coordinate Transformation Document (CDIL D-24)

     17   

5.3.20

 

Flight Software Users Manual (CDIL D-25)

     17   

5.3.21

 

Component Acceptance Data Package (CDIL D-26)

     17   

5.3.22

 

Jitter/MTF Analysis and Test Data (CDIL D-27)

     17   

5.3.23

 

Instrument/Sensor Boresight Stability Data (CDIL D-28)

     17   

5.3.24

 

Position and Attitude Accuracy (CDIL D-29)

     17   

5.3.25

 

Satellite to MGB Interface Control Document(s) (CDIL D-32)

     17   

5.3.26

 

DigitalGlobe to BATC Electrical GSE Interface Control Document (CDIL D-33)

     17   

6.0

 

PRODUCT ASSURANCE

     18   

6.1

 

P RODUCT A SSURANCE P LAN

     18   

6.2

 

BATC P ARTS C ONTROL B OARD (PCB)

     18   

6.2.1

 

Subcontractor Parts Control Board (PCB)

     18   

6.2.2

 

PCB Meetings

     18   

6.3

 

P ARTS AND M ATERIALS

     18   

6.3.1

 

Electrical, Electronic, and Electro-mechanical Parts (EEE)Parts Listing (CDIL QA-1)

     18   

 

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6.3.2

 

Material and Processes Reports (CDIL QA-2)

     19   

6.4

 

A S -B UILT C ONFIGURATION AND C ONFORMANCE

     19   

6.4.1

 

As-Built Configured Article List (CDIL QA-3)

     19   

6.4.2

 

Certificate of Conformance (CDIL QA-4)

     19   

6.5

 

P RODUCT A SSURANCE R EVIEWS (CDIL QA-5)

     19   

6.6

 

D OCUMENTATION

     19   

6.7

 

K NOWN N ON -C OMPLIANT H ARDWARE

     19   

6.8

 

M ILITARY S TANDARD 461

     19   

7.0

 

PROCUREMENT

     20   

7.1

 

G ENERAL

     20   

7.2

 

M AKE /B UY P LANS (CDIL PT-1)

     20   

7.3

 

E NCRYPTION /D ECRYPTION D EVICES

     20   

7.4

 

R EVIEWS

     20   

7.5

 

P ROGRAM S UBCONTRACT S TATUS R EPORT (PSSR) (CDIL PT-2)

     20   

7.6

 

D OCUMENTATION

     20   

7.7

 

S UBCONTRACT F LOW - DOWNS

     20   

7.7.1

 

Assignment Clause

     20   

7.7.2

 

Access

     20   

8.0

 

PRODUCTION ACTIVITIES

     21   

8.1

 

G ENERAL

     21   

8.2

 

P RODUCTION P ROCESS

     21   

8.3

 

A CCESS

     21   

8.4

 

P RODUCTION D OCUMENTATION

     21   

9.0

 

INTEGRATION AND TEST ACTIVITIES

     22   

9.1

 

G ENERAL

     22   

9.2

 

B OX /S UBSYSTEM L EVEL T ESTING

     22   

9.2.1

 

General

     22   

9.2.2

 

[**Redacted**]

     22   

9.3

 

WV B US AND S ATELLITE I NTEGRATION AND T EST P LANS (CDIL PT-3)

     22   

9.4

 

P OST -S HIPMENT I NSTRUMENT T ESTING

     22   

9.5

 

S UPPORTING D OCUMENTS

     22   

9.6

 

S YSTEM T EST R EPORTS (CDIL PT-5)

     23   

9.6.1

 

Content

     23   

9.6.2

 

Timeliness

     23   

9.7

 

U NINTERRUPTIBLE P OWER S UPPLY (UPS)

     23   

9.8

 

D IGITAL G LOBE I NTEGRATION AND T EST E NGINEERING A CCESS

     23   

9.8.1

 

On-Site and Visiting Engineers

     23   

9.8.2

 

Access to Live Satellite Telemetry

     23   

9.8.3

 

Test Observation By Other DG Engineers

     23   

9.8.4

 

Access to Command and Telemetry Log Files (CDIL PT-6)

     23   

9.9

 

T EST R EVIEWS

     23   

9.10

 

O PTIONAL T ESTING

     23   

 

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WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

 

10.0

 

CUSTOMER FURNISHED EQUIPMENT AND SERVICES

     24   

10.1

 

G ENERAL

     24   

10.2

 

F LIGHT E QUIPMENT

     24   

10.2.1

 

[**Redacted**]

     24   

10.2.2

 

[**Redacted**]

     24   

10.2.3

 

[**Redacted**]

     24   

10.2.4

 

[**Redacted**]

     24   

10.2.5

 

[**Redacted**]

     24   

10.2.6

 

[**Redacted**]

     24   

10.3

 

S IMULATORS (CSIM-1)

     24   

10.4

 

L AUNCH V EHICLE I NTERFACES

     24   

10.4.1

 

Launch Vehicle Interface

     24   

10.4.2

 

Launch Vehicle Separation Connectors (CLSE-3)

     24   

10.5

 

G ROUND S UPPORT E QUIPMENT

     25   

10.5.1

 

Wideband Link RGT Equipment

     25   

10.5.2

 

Narrowband Link RGT Equipment (CGSE-5)

     25   

10.5.3

 

Special Test Equipment

     25   

10.5.4

 

Mission Control Center (CGSE-11)

     25   

10.5.5

 

[**Redacted**]

     25   

10.5.6

 

[**Redacted**]

     25   

10.5.7

 

[**Redacted**]

     25   

10.5.8

 

MGB Test Equipment (CGSE-15)

     25   

10.6

 

L AUNCH V EHICLE D ATA (CLD-1 AND CLD-2)

     25   

10.7

 

I NSTRUMENT D ATA

     26   

10.7.1

 

Instrument Structural Analysis Data (CID-1)

     26   

10.7.2

 

Instrument Thermal Analysis Data (CID-2)

     26   

11.0

 

STORAGE AND DELIVERY

     27   

11.1

 

G ENERAL

     27   

11.2

 

S ATELLITE P RE -S HIPMENT S TORAGE

     27   

11.3

 

P RE -S HIPMENT R E -T EST

     27   

11.4

 

S ATELLITE S HIPPING AND D ELIVERY

     27   

11.5

 

S ATELLITE L AUNCH S ITE S TORAGE

     27   

12.0

 

LAUNCH SUPPORT SERVICES

     28   

12.1

 

G ENERAL

     28   

12.2

 

R EQUIREMENT D EFINITION

     28   

12.3

 

T ECHNICAL I NTERCHANGE M EETINGS

     28   

12.4

 

FEM AND CLA- TO -D ESIGN L OAD C OMPARISONS (CDIL LM-2)

     28   

12.5

 

E XPORT R EGULATIONS

     28   

12.6

 

A DAPTER F IT -C HECK

     29   

12.7

 

L AUNCH S ITE I NFRASTRUCTURE

     29   

12.8

 

L AUNCH S ITE O PERATIONS

     29   

12.9

 

F UELING

     29   

13.0

 

MISSION PREPARATION AND ON-ORBIT COMMISSIONING

     30   

13.1

 

T RAINING (CDIL LM-3)

     30   

13.1.1

 

Training Materials

     30   

 

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13.1.2

 

Training Sessions

     30   

13.2

 

C OMMAND AND T ELEMETRY H ANDBOOK (CDIL LM-4)

     30   

13.3

 

B US S UBSYSTEM C ALIBRATION T OOLS (CDIL LM-5)

     30   

13.4

 

D IGITAL G LOBE P ROCEDURE D EVELOPMENT S UPPORT

     30   

13.5

 

C OMMISSIONING P LAN (CDIL LM-6)

     30   

13.6

 

A NOMALY P REPARATIONS

     31   

13.7

 

S ATELLITE C OMMISSIONING

     31   

13.7.1

 

Launch and Early Operations (LEOP) Phase

     31   

13.7.2

 

Verification and Calibration (V&C) Phase

     31   

13.8

 

S ATELLITE S IMULATOR

     31   

13.8.1

 

Satellite Simulator (CDIL LM-8)

     31   

13.8.2

 

Documentation (CDIL LM-9)

     31   

13.8.3

 

Source Code (CDIL LM-10)

     32   

13.8.4

 

Delivery Schedule

     32   

13.8.5

 

Technical Interchange Meetings and Design Reviews

     32   

13.9

 

M ANEUVER P LANNERS

     32   

13.9.1

 

High Fidelity Maneuver Planner (CDIL LM-11)

     32   

13.9.2

 

Peak Estimator Algorithm (Low Fidelity Maneuver Planner) (CDIL LM-12)

     32   

13.9.3

 

[**Redacted**]

     32   

13.10

 

S OFTWARE T EST B ENCH

     33   

13.11

 

G ROUND S TATIONS

     33   

13.12

 

T ELEMETRY P ACKET C REATION AND M APPING T OOLS (CDIL LM-15)

     33   

13.13

 

T ELEMETRY M ONITOR AND R ESPONSE (CDIL LM-16)

     33   

14.0

 

COMMUNICATIONS FLEXIBILITY AND TT&C DEFINITION

     33   

15.0

 

FACILITIES

     33   
ATTACHMENT  1   CONTRACT DATA ITEMS LIST      Attch 1   
ATTACHMENT  2  CUSTOMER FURNISHED EQUIPMENT LIST      1   

 

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WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

1.0 Introduction

This Statement of Work defines those tasks to be performed by BATC, the Space Segment Integrator, in defining; designing, producing, testing, verifying, and preparing for launch; the DigitalGlobe WorldView 3 Satellite. BATC has the overall responsibility for Satellite performance, as defined in the WV3 Satellite Specification, provided the DG-furnished Instrument meets its interfaces and specifications as defined in Paragraph 2.2. Within this role, BATC has the responsibility to work with DigitalGlobe to define requirements, allocate budgets, analyze performance, execute trade studies, interact with other vendors, define configurations(s), conform to existing Instrument interfaces, assess and mitigate risks, prepare various programmatic documentation, and interact with all participating organizations via meetings, teleconferences, and reviews as defined herein.

BATC shall provide integrating services as defined herein and the hardware and software, exclusive of Customer Furnished Equipment, that comprise the WV3 Satellite.

This document also defines the scope of work required from DigitalGlobe and associated subcontractors in order for BATC to execute this contract successfully.

Associate contractors under contract to DigitalGlobe shall provide the Instrument and Launch services. However, BATC shall fully support defining, documenting, and verifying Satellite(s) to LV and MGB interfaces and integration procedures. BATC shall insure that the Satellite will withstand all launch environments.

1.1 Definitions

Agreement: Satellite Purchase Agreement #60150 by and between DigitalGlobe, Inc. and Ball Aerospace and Technologies Corp., dated August 27, 2010, as amended.

Authorization to Proceed (ATP): Effective date of work commencement per the Agreement.

Satellite: The complete space-borne infrastructure required to perform the mission of providing radiometrically and geometrically correct imagery of the Earth. The Satellite consists of the Instrument and the Spacecraft Bus.

[**Redacted**]

Instrument: The Instrument is that part of the Satellite that collects light photons using appropriate mirrors and structure, [**Redacted**] . It also may be designated the Electro-Optical Assembly (EOA). The instrument includes its own thermal control system. However, the instrument focus mechanism depends upon drive electronics to be provided by BATC per this Statement of Work. Also, the instrument stimulation lamp depends upon drive electronics to be provided by BATC per this Statement of Work.

Telescope: That part of the Instrument that collects and focuses light onto a focal plane. [**Redacted**] It also may be designated the Optical Telescope Unit (OTU).

Sensor Subsystem (SSS): That part of the Instrument that converts photons to analog voltage signals, [**Redacted**] , and digitizes [**Redacted**] those signals.

[**Redacted**]

Solid State Recorder: The subsystem that accepts digital data from the SSS and Ancillary Data from the spacecraft bus, provides storage, [**Redacted**] and outputs that data to the wideband transmitter(s).

Spacecraft Bus: The Bus is that part of the Satellite that provides the support infrastructure so the Instrument can function.

[**Redacted**]

MGB: “MGB” is a meaningless three letter designation for an additional subsystem being installed on the WV3 satellite. The MGB subsystem consists of three components. The first is a Sensor Unit (SU) which will attach to the aperture end of the OBA. The second is the Interface Adaptor Unit (IAU) which will mount to the spacecraft bus. The third is an inter-connect cable which connects the first two units.

Initial Acceptance: Occurs upon successful completion of the Satellite Pre-Ship Review as defined in paragraph 4.5.3.2.e

Final Acceptance: Occurs following satellite fueling operations and completion of the Satellite Launch Readiness Review as defined in paragraph 4.5.3.2.f

 

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WV3 Satellite Statement of Work_

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Transfer of Title: Occurs as defined in the Satellite Purchase Agreement paragraph 8.

1.2 Program Overview

Under this Scope of Work, DigitalGlobe will procure one satellite to support the EnhancedView program and future commercial operations. DigitalGlobe shall provide the Instrument as Customer Furnished Equipment via a procurement contract with ITT. DigitalGlobe shall provide the “MGB” subsystem. As on the WV2 program, BATC shall deliver a WorldView 2 like stimulation lamp that will be incorporated into the ITT provided instrument. BATC shall also incorporate into the Bus, an instrument focus mechanism electronics capability.

DigitalGlobe shall provide the Launch Services via a procurement contract with Lockheed Martin-Commercial Launch Services. Lockheed Martin-Commercial Launch Services has in-turn subcontracted with United Launch Alliance to provide the Atlas V launch vehicle and associated launch services. BATC can assume an Atlas V launch vehicle and a launch from Vandenberg Air Force Base. BATC shall assume satellite processing at Vandenberg AFB will occur in either the Astrotech Payload Processing facility or the Spaceport Systems International Processing Facility.

 

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2.0 Documents

2.1 Applicable Documents

This Statement-of-Work identifies applicable documents. These documents provide detailed requirements regarding Satellite performance, interfaces, and/or standardized design, fabrication, and testing processes/procedures. BATC and DigitalGlobe will perform the defined work according to these standardized processes/procedures such that the delivered products meet the performance and ICD requirements.

In the event of any conflict between these documents, the following order of precedence shall prevail: a) Agreement Terms & Conditions; b) Statement of Work; c) Satellite Specification; d) Other Applicable documents.

 

DigitalGlobe Produced or Provided Documents   

WV3 Satellite Specification

   [**Redacted**]

WV3 Spacecraft Simulator Specification

   [**Redacted**]

WV3 Command & Telemetry Handbook Specification

   [**Redacted**]

WV3 Maneuver Planner Specification

   [**Redacted**]

MGB Data Protection Plan for BATC

   [**Redacted**]

Stim Lamp and Stim Lamp Electronics Specification

   [**Redacted**]

[**Redacted**] Focus Mechanism Electronics Specification

   [**Redacted**]

Star Tracker Simulation Specification

   [**Redacted**]

IRU Simulator Specification

   [**Redacted**]

SSR to DPU Cable Design and Build Documentation

   [**Redacted**]

[**Redacted**]

   [**Redacted**]
BATC Produced Documents   

BATC Product Assurance Plan

   [**Redacted**]

BATC Supplier Product Assurance Plan

   [**Redacted**]

Civil & Operational Space (COS) SBU Configuration and Data Management (CD&M) Plan

   [**Redacted**]

WV-3 CDM Plan Addendum

   [**Redacted**]
Associated Contractor Produced Documents   

Astrotech Vandenberg Facility Accommodations Manual

   [**Redacted**]

Spaceport Systems International, Vandenberg Facility Payload Facility Handbook

   [**Redacted**]

Atlas V Launch Services User’s Guide

   [**Redacted**]

 

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2.2 Reference Documents

The following documents provide the baseline instrument definition. DigitalGlobe shall provide an instrument that is compliant with these documents.

DigitalGlobe Produced or Provided Documents

 

Instrument Specification

   [**Redacted**]

Instrument Finite Element Model

   [**Redacted**]

[**Redacted**]

   [**Redacted**]

 

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3.0 Contract Deliverables

3.1 Deliverable Items

 

  a. WV3 Satellite: Initial Acceptance: [**Redacted**] . Final Acceptance: [**Redacted**] Delivery shall be adjusted for Excusable Delay or failure of customer to [**Redacted**] to the extent that these delays affect the Delivery Date.

 

  b. WV3 Satellite Simulator

Initial release: [**Redacted**]

Simulator Delivery [**Redacted**]

Functional and performance signoff: [**Redacted**]

On orbit performance/tuning update: [**Redacted**]

 

  c. [**Redacted**]

 

  d. [**Redacted**]

 

  e. [**Redacted**]

 

  f. [**Redacted**]

 

  g. [**Redacted**]

 

  h. [**Redacted**]

 

  i. [**Redacted**]

 

  j. [**Redacted**]

 

  k. [**Redacted**]

 

  l. [**Redacted**]

 

  m. [**Redacted**]

 

  n. [**Redacted**]
  o. [**Redacted**]
  p. [**Redacted**]
  q. [**Redacted**]
  r. [**Redacted**]

3.2 Deliverable Data

Reference Attachment 1: Contractor Data Items List (CDIL)

3.3 Deliverable Services

  a. Storage and Delivery (Section 11.0)
  b. Launch Support (Section 12.0)
  c. Mission, Commissioning, & Readiness Support (Section 13.0)

 

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4.0 Program Management

4.1 Program Philosophy

Emphasis throughout all phases and functions of the project shall be to produce a reliable Satellite that meets the performance requirements on the contracted schedule. [**Redacted**]

4.2. BATC Organization (CDIL PM-1)

A dedicated Program Manager shall be appointed by BATC prior to the start of the contract. The Program Manager shall lead all of the Contractor’s activities under the contract.

A diagram illustrating the Program Management Structure shall be provided to DigitalGlobe. (CDIL PM-1) This diagram(s) shall indicate job titles and names of the program management team.

The Program Manager shall coordinate changes to contract conditions, price, timescale, deliverables, services or performance levels, unless a specific alternate has been appointed to deal with any of these matters. All changes to the contract documents shall require the written agreement of BATC contracts representative.

BATC shall also appoint a different and dedicated individual to be a single point of contact for each of the following:

 

  a. Program technical management (Satellite System Engineer)

 

  b. Instrument System Engineer

 

  c. Project Engineer Quality Assurance (PEQA)

 

  d. Program Integration and Test management

[**Redacted**] BATC shall appoint a different individual to be a single point of contact for each of the following:

 

  e. Various Bus Subsystem Lead Engineers

 

  f. Launch Vehicle Integration Engineer

 

  g. Program Contract Management

These individuals are key personnel and, if performing well, should remain unchanged for the duration of the program.

BATC shall appoint a Satellite Simulator Project Lead. This individual will be the technical lead for the Satellite Simulator development effort and will be responsible for meeting its technical and schedule guidelines established herein.

4.3 DigitalGlobe Management

DigitalGlobe will appoint a Program Manager who as an individual shall act as DigitalGlobe’s primary point of contact on all program management matters. As required, according to the activity and phase of the contract, the Program Manager will nominate specific individuals to interface directly with BATC.

The DigitalGlobe Program Manager shall coordinate changes to contract conditions, price, timescale, deliverables, services or performance levels, unless a specific alternate has been appointed to deal with any of these matters. All changes to the contract documents shall require the written agreement of the DigitalGlobe contracts representative.

DigitalGlobe will also appoint a responsible individual(s) to be a single point of contact for each of the following.

[**Redacted**]

BATC shall permit direct engineering interactions between these DG individuals and their BATC counterparts.

4.4 Space Segment Master Program Schedule (MPS) (CDIL PM-2)

BATC shall develop maintain, and provide a Master Program Schedule (MPS) for the entire program including hardware, software, analyses, data item deliverables, and subcontractor activities for all phases of the program including design, integration, test, and shipment through final acceptance.

 

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4.4.1 General

The MPS shall consist of a computer supported dependency network, each element of which shall represent a single program event. Each event shall be attributed a start and finish date. The network must clearly show the interdependency in terms of both time and function amongst the events.

The MPS shall be the major management tool for planning, monitoring and controlling the program, in terms of:

 

  a. Planning the program, monitoring progress, documenting actual activity accomplishment and actual durations.

 

  b. Predicting future progress.

 

  c. Identification of significant milestones e.g. review meeting.

 

  d. Identification of the time critical path.

 

  e. Reflecting actual progress and changes relative to baseline plan.

4.4.2 Required Software

The Contractor shall create and maintain the network using Microsoft Project (Version 2003). Schedules of a detailed nature shall be provided electronically on a monthly basis. A hardcopy shall also be provided on request.

4.4.3 MPS Construction

Content

The network shall be constructed against the following major classifications:

 

  a. Deliverable hardware down to component level

 

  b. Software development activities

 

  c. Facilities required to support the production of any of the deliverables

 

  d. Other events/items required to support the production of the deliverables or services. e.g. test aids, test software prototypes, etc.

 

  e. Customer Furnished Equipment required from DigitalGlobe

Individual items in each class shall be considered to consist of a number of generic events. These events shall typically consist of such activities as:

 

  a. Plan

 

  b. Design & develop

 

  c. Manufacture

 

  d. Assemble

 

  e. Integrate

 

  f. Test

 

  g. Deliver

 

  h. Reviews

However steps may be omitted or added given unit specific circumstances.

Unique Identifiers

The MPS shall include a unique identifying number for each task. This will more easily allow DigitalGlobe to combine certain tasks into a DigitalGlobe Master Schedule. Unique identifiers will not be deleted, reused, or re-assigned to other tasks.

Reports

The MPS shall be capable of generating a number of different types of reports upon demand. All events and milestones shall be coded to permit a variety of sort options to be exercised without program modification. Both GANTT and network form shall be supported.

4.5 Meetings & Reviews

BATC shall support the meetings and reviews listed in the following paragraphs.

 

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4.5.1 Weekly Status Meeting

BATC Program Manager shall support a weekly meeting/telecon with the DigitalGlobe Program Manager to review program status including schedule, technical, risk register, action item list, and subcontracts.

4.5.2 Monthly Program Status Review

BATC Program Manager shall support a monthly Program Status Review with DigitalGlobe.

4.5.3 Program Reviews

List of Formal Reviews

BATC will host and conduct formal reviews at the following program milestones. BATC shall prepare charts, viewgraphs, analysis results, trade study results, etc. in the quantity and quality typical of aerospace industries reviews.

 

  a. Satellite Requirements Review (SRR) (CDIL D-34) ) Only changes between WV2 and WV3 must be reviewed.

 

  b. Delta—Preliminary Design Review (PDR) (CDIL D-30) Only changes between WV2 and WV3 must be reviewed.

 

  c. Delta-Critical Design Review (CDR) (CDIL D-31) Only changes between WV2 and WV3 must be reviewed.

 

  d. Spacecraft Bus Complete/Instrument Integration Readiness Review (IRR) (CDIL – PT-8)

 

  e. Satellite Environmental Testing Readiness Review (CDIL – PT-9)

 

  f. Satellite Pre-Ship Review (CDIL PT-10)

 

  g. Launch Readiness Review (CDIL LM-14)

 

  h. [**Redacted**]

4.5.3.2 Content of Reviews

 

  A. PDR and CDR: BATC shall conduct “delta” reviews. These reviews will document the design changes between WV2 and WV3. These design reviews (PDR and CDR) shall include information and documentation typical of aerospace industry reviews, such as:

 

  1. Satellite mechanical configuration including stowed and deployed views

 

  2. Satellite mechanical configuration including [**Redacted**]

 

  3. Satellite electrical/electronic design, including system block diagram and redundancy scheme

 

  4. Satellite software design

 

  5. Satellite Operating Modes

 

  6. Satellite Fault Detection and Safing

 

  7. Satellite Budgets and Margins

 

  A. Performance relative to specifications

 

  B. Mass

 

  C. Power

 

  D. Thermal

 

  E. Consumables

 

  F. Attitude control: stability, pointing and knowledge

 

  G. RF links

 

  H. Satellite resources: relays, telemetry stream, CPU throughput, processor memory

 

  I. MTF

 

  J. Reliability: Ps, critical items list, cycle-limited items, FMECA

 

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  B. Spacecraft Bus Complete/Instrument Integration Readiness Review: BATC shall host this review. The purpose is to ensure the readiness to begin Instrument integration. This review will cover information including:

 

  1. Instrument Integration procedure and hardware status

 

  2. Status of all Certification Logs for all Ball built hardware that will be integrated to the Bus. Ball shall provide rationale and recovery plan for all certification logs that are open, even though the hardware is complete and ready for integration.

 

  3. TAR and HAR status from the Bus Integration and Test phase

 

  4. Test Team Personnel status, certifications, and time-sharing with other programs

 

  5. Facility status

 

  6. Satellite configuration review

 

  7. Other issues that may impact the timely and successful completion of Instrument integration.

 

  8. The Spacecraft Bus shall be deemed complete and ready for Instrument integration when: [**Redacted**]

 

  C. Satellite Environmental Testing Readiness Review: BATC shall host this review. The purpose is to ensure the readiness to begin satellite level environmental testing which includes but is not limited to: TVAC, EMI/EMC, Vibration, Shock, and Acoustic. This review will cover information including:

[**Redacted**]

 

  D. Satellite Pre-Ship Review: BATC shall host this review. The purpose is to ensure the readiness to ship the satellite to the launch site. This review shall be held after completion of all significant testing and all post-test reviews. The purpose shall be to review the results of the entire Integration & Test program, and demonstrate compliance to the satellite specification., and provide for satellite preliminary acceptance.

 

  The Pre-ship Review shall be deemed satisfactory and the satellite preliminary acceptance by DigitalGlobe complete when the:

[**Redacted**]

 

  E. Satellite Launch Readiness Review: BATC shall conduct a Satellite Launch Readiness Review (SLRR) on or about [**Redacted**] . (Note, the Launch Services Provider, Lockheed Martin/ULA also has a review called the Launch Readiness Review. However, that review encompasses the satellite, launch vehicle, weather, and range support.) This SOW paragraph is only concerned with the readiness to launch the satellite. BATC shall review the results of the launch site Integration & Test activities, review any updates to the Verification Matrix, and provide for satellite final acceptance.

 

  The SLRR shall be deemed satisfactory and the satellite final acceptance by DigitalGlobe complete when the:

[**Redacted**]

F. [**Redacted**]

4.5.4 Component/Subsystem Design Review Listing (CDIL PM-3)

BATC shall prepare a summary listing of all planned component (box level) and subsystem design reviews. This listing shall include BATC and vendor provided hardware, and BATC provided software including the satellite simulator and maneuver planner software. This listing shall define the meeting format and required attendance. BATC shall provide a minimum of 10 days advance notice to DigitalGlobe for the following major reviews:

 

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  a. System/Subsystem & Component PDRs
  b. System/Subsystem & Component CDRs

DigitalGlobe attendance and participation, including support consultants, shall be allowed, but not required at all reviews. The review activity will not be repeated if DigitalGlobe fails to attend.

4.5.5 Component/Subsystem Test Readiness / Data Review Listing (CDIL PM-4)

BATC shall prepare a summary listing of all planned component (box level) and subsystem qualification and acceptance test reviews. This listing shall include BATC provided and vendor provided hardware, and BATC provided software. This listing shall define the meeting format and required attendance. BATC shall inform DigitalGlobe of upcoming reviews in a timely manner.

DigitalGlobe attendance and participation shall be allowed, but not required at all reviews. The review activity will not be repeated if DigitalGlobe fails to attend.

4.5.6 DigitalGlobe Meetings

DigitalGlobe will arrange separate contracts for the:

 

  a. Launch Vehicle Segment (LV)

 

  b. Instrument

 

  c. Launch and Mission insurance

A series of technical interchange and review meetings will be held with these contractors jointly and separately, as required. BATC shall provide representation at these meetings as needed to resolve interface issues.

In the case of the insurance (c), BATC will provide inputs to formal presentations and support meetings to be held at the DigitalGlobe facility. DigitalGlobe will be responsible for responses to action items using information made available or provided by BATC during the course of the program.

4.6 Documentation Management

4.6.1 Access to Program Technical Data

DigitalGlobe will have access rights to all program technical data that BATC generates and Subcontractor data to which BATC has legal and contractual rights. Program technical data may include Engineering Reports, drawings, software source code, and other tools used in the development of the spacecraft and analysis of requirements.

4.6.2 Objective

BATC shall establish a control and monitoring process relating to all deliverable documentation and other technical and test data for the complete program. The program shall account for the following:

 

  a. Preparation, review, and formal release as required

 

  b. Changes

 

  c. Storage, backup, and retrieval

 

  d. Distribution

 

  Note: BATC shall include the DigitalGlobe Satellite Integration and Test Point-of-Contact on the distribution list of all relevant WV3 Engineering Reports. (“Relevant” in this clause refers to all ERs containing design information, analyses, test data, etc that affect the performance and/or operations of the satellite. It does not include ERs that contain BATC proprietary cost data.)

 

  e. DigitalGlobe access to all BATC documentation prepared on the project

 

  f. Long term storage for the purpose of through-life product support

As a primary supporting management tool, BATC shall use a secure project server. All data items except memory intensive drawings, test data, production logs, and QA data shall be maintained electronically on the project server. The project shall use the Microsoft Office software suite for word processing, spreadsheets, presentations, and documentation databases.

 

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4.6.3 Documentation Listing (CDIL PM-5)

BATC shall develop and maintain a Documentation Listing that identifies all deliverable reports, analyses, drawings, software items, etc., that are developed on the project. The Documentation Listing shall include a naming convention that uniquely identifies the documents for electronic access where applicable. The List shall also indicate spacecraft name, a short title/description of the document, subsystem affected, the latest revision number and date, planned completion date, and status information. The List shall indicate those WV1 and WV2 documents that are also applicable to WV3. Document updates are required to reflect content changes. Document updates are not required if the sole purpose is to reflect applicability to WV3.

4.6.4 Documentation Delivery

The Contractor shall deliver document in native formats, e.g. Microsoft Word, Excel, etc., as opposed to PDF except as noted below. DigitalGlobe will identify the delivery location, such as a Microsoft Office Sharepoint Server (MOSS) internet site, and provide Contractor with username and password-controlled access. Documents shall be submitted or made available to DigitalGlobe according to the dates indicated in the list provided in Attachment 1.

In the case of deliverables generated in Microsoft Office, such as Word, Excel, PowerPoint, etc; BATC shall populate the document property fields with the following minimum information: Title, Subject, Author, and key words.

In the case of deliverables that are not generated in MicroSoft Office, such as BATC drawings, .pdf is acceptable and BATC shall populate the property fields of drawings after they are converted to .pdf format.

4.7 Action Item Tracking (CDIL PM-6)

BATC shall maintain an Action Item List indicating all significant action items, including those of BATC as well as those of other organizations that relate to interactions with BATC. The Action Item List will be developed and maintained in a format that allows sorting by subsystem, originating party, receiving party, originating date, and closing date. BATC shall be responsible for ensuring closure of those items relating to BATC interactions and interfaces.

4.8 Financial Management

BATC shall define a standard set of formats for reporting program financial payment and billing status and shall submit them on a monthly basis. This shall consist of the following:

4.8.1 Historical Record of Payments (CDIL PM-7)

This shall consist of a record of the individual payments made, updated on a monthly basis. This record shall be cross-referenced to the payment schedule incorporated in the contract. Payments made in support of contract amendments shall be separately reported and cross-referenced to the payment schedule incorporated in the amendment.

4.8.2 Payments Forecast (CDIL PM-7)

This shall consist of a forecast of the future invoices and shall be cross-referenced to the payment schedule incorporated in the contract. Payment milestone forecasts shall be consistent with program progress reported on the Master Program Schedule. NOTE: Record of Payments and Payment Forecast are delivered as a single CDIL item.

4.9 Contract Change Control

These are considered to be of three types only:

 

  a. Contract Amendments

 

  b.

Waivers: A written authorization granted after contract award to accept an item, that during production, or after having been submitted for inspection or acceptance, is found to depart from contract or specified

 

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  configuration requirements. Waivers are intended only as one-time departures from an established configuration for specified items or lots and are not intended to be repeatedly used in place of formal engineering changes.

 

  c. Deviations: A written authorization, granted after contract award and prior to the manufacture of the item, to depart from a particular performance or design requirement of a contract, specification, or referenced document, for a specific number of units or a specified period of time. Deviations are intended only as one-time departures from an established configuration for specified items or lots and are not intended to be repeatedly used in place of formal engineering changes.

BATC shall devise a system to control, monitor, and notify DigitalGlobe of these changes. The control system shall include provision for:

 

  a. A unique numbering scheme to track the changes through to completion.

 

  b. Impact upon contract obligation:—price, performance and delivery schedule, with specific identification of the item(s) of hardware, software or documentation affected.

 

  c. Notification of timescale for acceptance or rejection for each change, typically 10 business days.

 

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5.0 Design

 

5.1 General

BATC shall perform the necessary trade studies, preliminary design, and detailed design of the Satellite, exclusive of the Customer Furnished Equipment as defined in Section 10, in accordance with the applicable documents. BATC shall design and procure the Ground Support Equipment necessary to support Satellite Integration and Test activities, except for items defined in Section 10.0. Design activities shall be featured in the program master schedule.

 

5.2 Working Groups and Trade Studies

5.2.1 Working Groups

[**Redacted**]

5.2.2 Trade Studies

 

5.3 [**Redacted**]Satellite Design Data

The satellite shall be designed such that the environmental design criteria of the Instrument as defined in the documents of paragraph 2.2 are not exceeded, and the structural, electrical, and thermal characteristics, as defined in the documents of paragraph 2.2, of the Instrument are accommodated.

DigitalGlobe shall provide information required to update the budgets for the Customer Furnished Equipment, consistent with paragraph 2.2.

5.3.1 Satellite to Instrument Interface Control Document(s) (CDIL D-1)

BATC shall produce and maintain the Satellite to Instrument ICD(s). The ICD(s) will address all interface issues including but not limited to: power, commanding, telemetry, mass and mass properties, mechanical envelope and mounting, thermal, fields-of-view, vibration and jitter isolation/management, and accommodation of bus components on the Instrument.

5.3.2 Satellite to Ground Terminal Narrowband Link ICD (CDIL D-2)

BATC shall produce and maintain the Satellite to Ground Station Narrowband Link ICD. This link will address both the command uplink and telemetry downlink.

5.3.3 Satellite to Ground Terminal Wideband Link ICD (CDIL D-3)

BATC shall produce and maintain the Satellite to Ground Terminal Wideband Link ICD.

5.3.4 Satellite Environmental Design and Test Specification (EDTS) (CDIL D-4)

BATC shall prepare and maintain the EDTS, or equivalent document defining the component environmental design and test requirements. Electromagnetic Interference Design and Testing shall be in accordance with the standards specified in Satellite Specification.

5.3.5 Contamination Control Plan(s) (CDIL D-5)

[**Redacted**]

5.3.6 Satellite Level Requirements Verification/Compliance Matrix (CDIL D-6)

BATC shall produce a satellite level RVCM. The RVCM will include requirements from the Satellite Specification, [**Redacted**] and the Instrument Specification if applicable. BATC shall update/maintain the Satellite RVCM to reflect changes to these parent specifications. DigitalGlobe shall have review and approval authority over changes to the RVCM. BATC shall include the following information in the RVCM

 

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  a. Source of requirement (Parent specification document and paragraph number, i.e. satellite spec, instrument spec, etc)
  b. Specification paragraph
  c. Paragraph title
  d. Summary description of requirement
  e. Column indicating status of compliance
  f. Summary description of performance
  g. Responsible organization
  h. Verification Point [**Redacted**]
  i. Verification Method [**Redacted**]
  j. Verification Source Document indicating applicable paragraph, test sheet, etc.
  k. Comments, if required.
  l. Other information at BATC’s option

5.3.7 Box Level Requirements Verification/Compliance Matrix (CDIL D-7)

BATC shall flow down requirements from the Satellite Specification to box level requirements. BATC shall develop performance requirements for each box level component on the Satellite excluding CFE. For this paragraph, “box level component” also includes all components that are not really “box” like. These include but may not be limited to:

[**Redacted**]

BATC shall use the Box Level RVCM as an input into the box level performance test procedures. BATC shall demonstrate compliance to the box level RVCM.

5.3.8 Drawings (CDIL D-8)

A complete file of BATC drawings prepared for the WV3 program, will be maintained on file in electronic and hardcopy form, where appropriate. Electronic transfer to DigitalGlobe will constitute delivery.

5.3.9 Performance Compliance and Risk Management

5.3.9.1 Performance Compliance (CDIL D-9)

The contractor shall supply at PDR a Performance Compliance Matrix identifying the performance estimate, allocated uncertainty (and/or contingency as appropriate) and resulting Total Performance (where Total Performance = performance estimate + uncertainty) for the following list. The Performance Compliance Matrix shall be updated and provided with each Quarterly Review following the PDR. [**Redacted**]

[**Redacted**]

DigitalGlobe shall provide performance information required to update the budgets for any of the Customer Furnished Equipment, in accordance with the documents in Paragraph 2.2.

5.3.9.2 Risk Management Report (CDIL D-10)

BATC and DigitalGlobe shall jointly develop and maintain a Risk Status Report. This report highlights known program risks, assigns risk levels, and documents mitigation strategies and status. BATC shall supply at PDR an initial Risk Status Report covering the system elements to be provided by this SOW. BATC shall updated the Risk Status Report monthly following the PDR.

5.3.10 Subsystem Description Documents (CDIL D-11)

BATC shall prepare Subsystem Description Documents for each satellite subsystem.

The Subsystem Description Documents will include as a minimum, unless provided in other deliverable documents, and referenced in the SDD:

a. Subsystem Overview including a detailed block diagram
b. Functionality and major performance characteristics of each Subsystem Component
c. Redundancy

[**Redacted**]

d. [**Redacted**]

 

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e. [**Redacted**]

 

f. [**Redacted**]

 

g. Subsystem schematic including power, power returns, commands, and telemetry. This schematic shall be updated to reflect Engineering Change Orders.

 

h. Expected nominal operating methods and telemetry limits

[**Redacted**]

 

i. Operational constraints

[**Redacted**]

 

j. Fault Protection

[**Redacted**]

j.2 List the information available to the operator to reconstruct or identity the fault.

 

k. Interfaces between subsystem components

 

l. Major interfaces with other subsystems

The Subsystem Description Documents shall be delivered at CDR + 4 months. If changes require an update to the document, those updates shall be provided at approximately Launch – 4 months and again at Launch + 4 months. The subsystem schematic (item e.) shall be updated as required throughout the program to reflect Engineering Change Orders.

5.3.11 Analysis and reports

BATC shall perform the following analyses. Updates shall be provided when changes significantly invalidate previous results.

 

  a. (1) Integrated Spacecraft Bus/Instrument thermal analyses, including summary of temperature predictions for unit level components under various operational modes and (2) unit-level thermal analysis [**Redacted**] . (CDIL D-12)

 

  b. Integrated Spacecraft Bus/Instrument structural analysis including [**Redacted**] . (CDIL D-13)

 

  c. Control system analysis including [**Redacted**]. (CDIL D-14)

 

  d. System Level Failure Modes and Effects and Criticality Analysis (FMECA). [**Redacted**] (CDIL D-15)

 

  e. Satellite Reliability Analysis BATC shall calculate satellite reliability using its standard process. [**Redacted**] (CDIL D-16)

 

  f. Satellite Life Prediction Data. DigitalGlobe needs to continually assess expected satellite life based upon actual on-orbit operational parameters. BATC shall provide all backup data used by BATC for sizing and life predictions. BATC does not need to produce a life expectancy analysis. DigitalGlobe will use the provided data and make our own Life Prediction. BATC can provide the life prediction data in one summary package, or in other CDILs.

 

  g. Flight Battery Life Prediction Analysis. BATC shall produce a life expectancy analysis for the satellite battery. The battery life prediction shall account for ground handling and will include a family of curves based upon pertinent on-orbit variables including but not necessarily limited to temperature and depth-of-discharge. (CDIL D-35)

 

  h. Satellite Imaging Performance (CDIL D-17)

BATC shall perform a comprehensive analysis regarding imaging performance. This is a comprehensive look at the numerous subsystem and trans-subsystem performance measures that affect imaging. The list includes but is not limited to:

[**Redacted**]

 

  i. [**Redacted**]

 

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5.3.12 Other Interface Control Documents

BATC shall provide inputs, review, and verify BATC side of the following ICDs.

a. Satellite to Launch Vehicle ICD

In the event the ICDs require revision, the changes will be discussed between the affected parties to determine the most cost and schedule efficient manner to implement the change. If applicable, any impact will be covered under changes provision of the Contract.

5.3.13 Critical Items list (CDIL D-18)

BATC shall maintain a Critical Items List summarizing all known single point failures on the Satellite and any special efforts required to mitigate risk associated with them. It shall also contain any items requiring special handling due to a high potential of damage, mission criticality, or safety concerns.

5.3.14 Component Heritage Summary (CDIL D-19)

The Component Heritage Summary will consist of a listing of all Satellite units by subsystem summarizing:

 

  a. Unit name

 

  b. Development / qualification history (e.g. engineering model, qual, protoflight)

 

  c. Previous flight heritage

 

  d. Modifications to previous uses

 

  e. Any significant known anomalies on flight units

5.3.15 Engineering Reports (CDIL D-20)

A complete file of all relevant Engineering Reports prepared on the WV3 program funding shall be maintained on file in electronic and hardcopy form where appropriate. Electronic transfer to DigitalGlobe will constitute delivery and shall occur within 5 business days of the ER release date. ERs delivered as a separate CDIL do not need to be delivered twice – once per this paragraph and again per the relevant CDIL paragraph. Those ERs need only be delivered once per the relevant CDIL paragraph.

(“Relevant” in this clause refers to all ERs containing design information, analyses, test data, etc that affect the performance and/or operations of the satellite. It does not include ERs that contain BATC proprietary cost data.)

5.3.16 Flight Software Source Code (CDIL D-21)

Per the terms of the software license agreement set forth in the Agreement, BATC shall grant to DigitalGlobe a limited license to use the flight software code. A copy of the flight software code, as identified below, shall be provided to DigitalGlobe on suitable media. Other elements of the software, as identified below, shall be placed in escrow per the Agreement.

[**Redacted**]

For units that are subcontracted by BATC, software and firmware shall be delivered if delivered to BATC and BATC has the right to deliver it to DigitalGlobe.

5.3.17 Composite Grounding Design (CDIL D-22)

[**Redacted**]

5.3.18 Structural, Power, Thermal, and Reliability Analytical Models (CDIL D-23)

BATC shall provide the analytical models used to predict the integrated spacecraft and instrument Structural [**Redacted**] , Power, and Thermal performance.

Satellite thermal performance modeling shall use the instrument thermal model provided by ITT. BATC shall use the integrated Satellite model to:

 

  a. Verify thermal interface requirements documented in the Spacecraft Bus to Instrument ICD are being met. Although BATC shall not be held contractually responsible for non-compliances on the ITT side of the interfaces, any such non-compliances revealed by Satellite thermal modeling shall be reported to DigitalGlobe.

 

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  b. Verify the Bus meets all of its requirements when modeled as a complete Satellite, for example unit temperatures and line of sight stability. BATC shall deliver line of sight motion vs. time profiles to DigitalGlobe (for incorporation into system geolocation budgets).

 

  c. Develop predicted temperature vs. time profiles of key instrument nodes as coordinated with ITT through the established ICD process. BATC shall deliver these temperature profiles to DigitalGlobe and forward a copy to ITT (so that ITT can verify the instrument meets its requirements).

BATC shall also provide the spacecraft bus reliability model down to the component and/or card level. Electronic transfer to DigitalGlobe will constitute delivery.

5.3.19 Coordinate Transformation Document (CDIL D-24)

BATC shall provide the documentation of all coordinate reference frames used in the satellite system including their reference points within the spacecraft. Nominal values for all transformations shall be provided. Reference frames requiring on-orbit calibration shall be noted. The document shall be updated with best-estimates from pre-launch calibrations and measurements.

5.3.20 Flight Software Users Manual (CDIL D-25)

BATC shall provide documentation of the flight software to include flowchart of routines/modules, structure and calling sequences, commands, telemetry, database constants and uploadable parameters, address tables, and log file definitions and locations.

5.3.21 Component Acceptance Data Package (CDIL D-26)

BATC shall provide or make available data acceptance packages for all major components.

5.3.22 [**Redacted**]

[**Redacted**]

5.3.23 Instrument/Sensor Boresight Stability Data (CDIL D-28)

[**Redacted**]

5.3.24 Position and Attitude Accuracy (CDIL D-29)

BATC shall provide detailed analysis and test data showing compliance with position and attitude accuracy requirements.

5.3.25 Satellite to MGB Interface Control Document(s) (CDIL D-32)

BATC shall produce and maintain the Satellite to MGB ICD(s). The ICD will address all interface issues including but not limited to: power, commanding, telemetry, mass and mass properties, mechanical envelope and mounting, thermal, fields-of-view, vibration and jitter isolation/management.

5.3.26 DigitalGlobe to BATC Electrical GSE Interface Control Document (CDIL D-33)

BATC shall produce and maintain an ICD for the STOC-to-NarrowBand Rack interface. This includes but is not limited to: grounding, commanding, telemetry, data formats, etc.

 

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6.0 Product Assurance

6.1 Product Assurance Plan

The Contractor and its subcontractors shall have an established quality control system that meets the requirements of BATC’s Product Assurance Plan and BATC’s Supplier Product Assurance Plan

6.2 BATC Parts Control Board (PCB)

The Parts Control Board (PCB) shall be constructed as follows: A PCB will be established. The responsibility of this PCB is to ensure each EEE part was evaluated for performance relative to the requirements. With the exception of System Safety, the PCB will also be used as the forum to discuss other Systems Assurance/Product Assurance issues i.e., Materials and Processes, Reliability, etc. The PCB is responsible for the review and disposition of any noncompliance with BATC’s Product Assurance Plan.

The PCB consists of:

 

  a. BATC Product Assurance Manager (Chairman)

 

  b. BATC WV3 Product Assurance Specialist or designated alternate

 

  c. Designated technical specialist from the hardware/software product team as needed

 

  d. Other necessary disciplines as needed

 

  e. DigitalGlobe Designated Representative(s). (The DigitalGlobe member is a non-voting adjunct member).

6.2.1 Subcontractor Parts Control Board (PCB)

Subcontractor PCBs shall be established as necessary to implement BATC’s supplied Product Assurance Plan. It is BATC’s responsibility to verify compliance.

6.2.2 PCB Process

Upon identification of a need for a PCB, BATC shall document relevant information in a System Engineering Report (SER) and obtain approval (signatures) from the PCB members. DigtalGlobe shall have PCB approval authority or waiver authority for non-compliances listed in the Specification Addendum, otherwise BATC shall notify DigitalGlobe. The SER shall be released to DigitalGlobe under CDIL D-20 within 5 working days of PCB approval. Any PCB discussions prior to release of the SER may be informal and in most cases shall be delivered to DigitalGlobe electronically via e-mail.

Minimal BATC PCB approval/disposition signatures include BATC PAM and BATC WorldView Product Assurance Specialist or his designated alternate. Once the PCB approves a part, the Parts Engineer will indicate approval on the Advanced or Program Parts List (A/PPL).

6.3 Parts and Materials

6.3.1 Electrical, Electronic, and Electro-mechanical Parts (EEE)Parts Listing (CDIL QA-1)

BATC shall prepare, maintain, and deliver a EEE Parts Listing for all satellite hardware except for Customer Furnished Equipment. This listing shall identify all EEE parts intended to be used by BATC and its vendors. For each part, the following minimum information shall be identified: manufacturer, description, lot date code. Parts shall be qualified as compared to BATC product assurance criteria and the Satellite Specification and the Satellite Specification Addendum. BATC’s internal process and format for EEE Parts Listing may be utilized.

The Parts List shall be maintained and reviewed by BATC as necessary, but minimally it shall be updated and provided to DigitalGlobe at the following:

 

  a. Prior to manufacturing for each box/component At this phase, it is acknowledged by DigitalGlobe and BATC that the list may be incomplete due to part shortages.

 

  b. Prior to box/component level Test Readiness Review

 

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  c. Prior to the integration of any box/component onto the Bus.

6.3.2 Material and Processes Reports (CDIL QA-2)

BATC shall prepare and deliver reports documenting their approval of all materials and processes planned for use on the Bus.

6.4 As-Built Configuration and Conformance

6.2.1 6.4.1 As-Built Configured Article List (CDIL QA-3)

The as-built configured article status shall be maintained throughout the production program in the certification logs and production orders. At the conclusion of integration, the information shall be used to generate the preliminary As-built Configured Article List. After test and modification (if any) the List shall be finalized and presented.

6.2.2 6.4.2 Certificate of Conformance (CDIL QA-4)

A Certificate of Conformance shall be generated and signed off by Product Assurance and Program Management. It details the conformance (and exceptions) to the SOWs, specifications and other contractual documents for the delivered article. This Certificate of Conformance shall be delivered to DigitalGlobe at the Launch Readiness Review.

6.5 Product Assurance Reviews (CDIL QA-5)

The plan shall include a program for the periodic audit of portions of the Contractor’s Product Assurance System in each of the below activity areas to confirm conformance to the requirements. These audits will be conducted by the Program Product Assurance engineer. BATC shall inform DigitalGlobe of the audit results.

 

  a. Reliability

 

  b. Parts Procurement

 

  c. Materials and Processes

 

  d. Non-Conforming Material Control

 

  e. Configuration Management

 

  f. Safety

6.6 Documentation

Documents shall be submitted or made available to DigitalGlobe as indicated in the list provided in Attachment 1.

6.7 Known Non-Compliant Hardware

[**Redacted**]

6.8 Military Standard 461

[**Redacted**]

 

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7.0 Procurement

7.1 General

BATC shall be responsible for the work associated with the procurement of all material and subcontracts required to provide the deliverable items, except for the CFE items identified in Section 10.0. BATC shall procure according to the CSO Supplier Product Assurance Plan. Procurement activities shall be featured in the program master schedule.

7.2 Make/Buy Plans (CDIL PT-1)

BATC shall identify Make/Buy plans for all Satellite components.

7.3 Encryption/Decryption Devices

[**Redacted**]

7.4 Reviews

A series of reviews shall be established with each subcontractor. A schedule of these reviews shall be included in the Review Listings required by paragraph 4.5.3. The reviews will generally be held at the vendor and DigitalGlobe personnel may attend, at their option.

7.5 Program Subcontract Status Report (PSSR) (CDIL PT-2)

BATC shall prepare a Program Subcontract Status Report (PSSR) for the program. The PSSR will contain critical status information on each major subcontract (larger than $1M) relative to:

 

   

Design & development

 

   

Procurement and Production

 

   

Assembly

 

   

Integration

 

   

Test, including any anomalies

 

   

Delivery schedule

 

   

Reviews

7.6 Documentation

Documents shall be submitted or made available to DigitalGlobe as indicated in the list provided in Attachment 1.

7.7 Subcontract Flow-downs

7.7.1 Assignment Clause

[**Redacted**]

7.7.2 Access

[**Redacted**]

 

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8.0 Production Activities

8.1 General

BATC shall appoint a Production engineer responsible for ensuring that BATC’s production capabilities match the requirements of the program. With the support of the Program QA engineer, he shall ensure that the production facilities comply with the Product Assurance requirements.

BATC shall be responsible for the work associated with the production of the deliverable items, except for the CFE items identified in Section 10.0. BATC shall be responsible for the production activities associated with integrating the CFE items as defined in Section 10.

Production activities shall be featured in the program master schedule.

8.2 Production Process

BATC shall produce the deliverable hardware according to applicable BATC standardized procedures. As a minimum, standardized BATC procedures shall be followed for the following topics:

[**Redacted**]

8.3 Access

The production manager shall arrange access for the DigitalGlobe staff to BATC manufacturing areas where manufacturing activities associated with the program are taking place.

8.4 Production Documentation

Production orders and Certification Logs shall document the as-built configuration. These logs shall be available on-site for DigitalGlobe review.

 

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9.0 Integration and Test Activities

9.1 General

For the WV program the Integration and Test activities fall into four logical categories.

 

  a. Box level / Subsystem level testing

 

  b. Bus level integration and testing including integration of the instrument

 

  c. Satellite level testing

 

  d. Mission and Launch Rehearsals

The Integration and Test Manager shall be responsible to ensure that BATC’s integration and test capabilities match the requirements of the program

BATC shall accomplish the work associated with a-d above for all BATC supplied hardware/software. BATC shall accomplish the work associated with b-d above for all CFE.

9.2 Box/Subsystem Level Testing

9.2.1 General

BATC shall perform all box level testing per environmental design and test specification and the box level Requirements Verification and Compliance Matrix.

9.2.2 [**Redacted**]

[**Redacted**]

9.3 WV Bus and Satellite Integration and Test Plans (CDIL PT-3)

BATC shall develop a WV Bus and Satellite Integration and Test Plan (Satellite I&T Plan) for the WV3 satellite. The test plans will include all I&T activities starting from the installation of the first component on to the bus structure through launch.

The WV I&T Plan(s) shall:

[**Redacted 4 Pages**]

9.4 Post-Shipment Instrument Testing

ITT will perform post-shipment functional testing to verify the Instrument survived shipment without damage. ITT will provide the necessary test equipment for the Instrument.

BATC shall provide:

[**Redacted**]

For schedule purposes the Instrument is not considered delivered to BATC upon arrival at BATC facility. Rather the instrument is considered delivered on the date that the Instrument has completed all necessary post-shipment testing and is ready and available for BATC to integrate to the telescope/bus.

9.5 Supporting Documents

BATC shall provide as a minimum the following support documents:

 

  a. All necessary box level test procedures, integration procedures, and system level test procedures. Each procedure shall include a detailed test description explaining the “what, how, and why” of each test.

 

  b. A System Level Test Matrix. The test matrix will identify which System Level Test procedures or portions of those procedures will be accomplished at each test phase. The System Level Test phases include, but are not limited to:

[**Redacted**]

 

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9.6 System Test Reports (CDIL PT-5)

[**Redacted**]

9.6.1 Content

The report shall include a summary of satellite configuration, test objectives, test results, significant hardware/software anomalies if any, resolution of significant anomalies, and a copy of all telemetry plots or other post-test data. The cognizant test engineer and the appropriate subsystem engineer(s) shall sign the report.

9.6.2 Timeliness

BATC shall publish the test reports No Later Than 15 working days after test completion.

9.7 Uninterruptible Power Supply (UPS)

[**Redacted**]

9.8 DigitalGlobe Integration and Test Engineering Access

9.8.1 On-Site and Visiting Engineers

BATC shall provide dedicated cubicle space, furniture, high-speed internet access, and phone lines for three resident DigitalGlobe I&T engineers. These DG on-site engineers will serve as the I&T focal point between DG and BATC. It is anticipated these engineers will be on-site at BATC on a full-time basis. BATC shall provide dedicated cubicle space, furniture, high-speed internet access, and phone lines for one visiting DigitalGlobe engineer.

9.8.2 Access to Live Satellite Telemetry

Once power-on bus integration begins, BATC shall provide DG with access to the live satellite telemetry from the cleanroom. DG will provide the necessary hardware to connect the Mission Control Center (MCC) to BATC GSE. DG will man and operate the DG hardware as necessary to flow the telemetry to the MCC. DigitalGlobe access to telemetry will occur on a non-interference basis to BATC test team.

9.8.3 Test Observation By Other DG Engineers

BATC shall allow other DG satellite and ground system engineers access to the cleanroom to witness satellite testing. BATC is not obligated to coordinate, inform, or schedule testing according to DG engineer availability.

9.8.4 Access to Command and Telemetry Log Files (CDIL PT-6)

BATC shall deliver an archive of all command and telemetry files from satellite integration and test in an electronic format. BATC shall deliver an update weekly. Electronic transfer to the DG server shall constitute delivery. BATC shall maintain information about which command and telemetry database was used in delivered files as well as which test procedures were run in each file.

9.9 Test Reviews

The status of the Satellite shall be reviewed during the test phases of the program. See paragraph 4.5.3.2 for the list of reviews and required content.

9.10 Optional Testing

The following is a list of optional tests to be performed or supported by BATC. These are tests DigitalGlobe may choose to have BATC perform if the schedule permits. BATC should not show these tests in the baseline schedule. In each case after a test option is exercised by DigitalGlobe, BATC has 30 calendar days to prepare for the test. BATC shall provide a separate option price prior to the start of I&T for each of these tests.

[**Redacted**]

 

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10.0 Customer Furnished Equipment and Services

10.1 General

DigitalGlobe has contracts with vendors other than BATC who are responsible for providing portions of the overall system. DigitalGlobe has the responsibility for monitoring, administering, and verifying performance of those subcontracts. This section defines the items and support requirements that DigitalGlobe is responsible for securing and providing to BATC via these other subcontractors. This section also defines the equipment that DigitalGlobe is responsible for providing directly.

The delivery of all items shall be per Attachment 2: Customer Furnished Equipment list. DigitalGlobe will also arrange for the return of loaned equipment, if required, at no cost to BATC. CFE items shall be featured in the program master schedule. Unless otherwise explicitly provided to the contrary in Attachment 2, title to all equipment identified in this Section 10.0 shall remain in DigitalGlobe.

10.2 Flight Equipment

[**Redacted**]

10.2.1 [**Redacted**]

[**Redacted**]

10.2.2 [**Redacted**]

[**Redacted**]

10.2.3 [**Redacted**]

[**Redacted**]

10.2.4 [**Redacted**]

[**Redacted**]

10.2.5 [**Redacted**]

[**Redacted**]

10.2.6 [**Redacted**]

[**Redacted**]

10.3 Simulators (CSIM-1)

[**Redacted**]

10.4 Launch Vehicle Interfaces

10.4.1 Launch Vehicle Interface

DigitalGlobe shall provide a launch vehicle interface adapter to BATC (CLSE-1). BATC shall use this for a fit check and for a separation test as described in paragraph 9.3.e. DigitalGlobe shall provide a match drill template to BATC (CLSE-2).

10.4.2 Launch Vehicle Separation Connectors (CLSE-3)

DigitalGlobe shall provide the flight satellite/launch vehicle separation connectors.

 

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10.5 Ground Support Equipment

10.5.1 Wideband Link RGT Equipment

DigitalGlobe will provide a set of RGT ground equipment for capturing Instrument data in the cleanroom. Nominally, this will include the following equipment and documentation:

[**Redacted**]

10.5.2 Narrowband Link RGT Equipment (CGSE-5)

DigitalGlobe will provide a set of RGT ground equipment for processing the S-band uplink and X-band narrowband downlink in the cleanroom. The capability to bypass the RF sections and operate at a baseband Satellite interface shall be provided by BATC . This may include elements of the Mission Control Center [**Redacted**] as dictated by the architecture of the ground system. DigitalGlobe shall deliver to BATC operating documentation and interface details one month prior to delivery.

This equipment shall include: [**Redacted**]

10.5.3 Special Test Equipment

DigitalGlobe shall provide special WB Link / WB receiver test equipment for WB link development and testing. This will include:

[**Redacted**]

10.5.4 Mission Control Center (CGSE-11)

DigitalGlobe will provide portions of the Mission Control Center (MCC) and software as required to support the Satellite Integration and Test Plan, via data links between the MCC in Longmont, CO and BATC. BATC shall be responsible for work on the Satellite required to resolve problems associated with the Satellite performance and function. All work associated with resolution of DigitalGlobe provided ground equipment and interfaces shall be at DigitalGlobe expense.

10.5.5 [**Redacted**]

[**Redacted**]

10.5.6 [**Redacted**]

[**Redacted**]

10.5.7 [**Redacted**]

[**Redacted**]

10.5.8 MGB Test Equipment (CGSE-15)

DigitalGlobe shall provide a signal generator, up-converter, feedhorn, and control computer.

10.5.9 [**Redacted**] (CGSE – 16)

[**Redacted**]

10.6 Launch Vehicle Data (CLD-1 and CLD-2)

DigitalGlobe shall provide a preliminary and final Coupled Loads Analysis (CLA) to BATC from the Launch Services contractor.

 

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10.7 Instrument Data

DigitalGlobe shall provide the WV3 instrument data and models, as specified in Paragraph 2.2, to support satellite level analysis and modeling for the areas listed below. BATC shall be responsible for additional data to support the provisions of this document and the spacecraft specification.

10.7.1 Instrument Structural Analysis Data (CID-1)

DigitalGlobe shall provide the WV3 instrument structural data and model.

10.7.2 Instrument Thermal Analysis Data (CID-2)

DigitalGlobe shall provide WV3 instrument thermal data and model.

 

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11.0 Storage and Delivery

11.1 General

BATC shall be responsible for storage, if required, and delivery of the WV3 Satellite in accordance with the following paragraphs.

11.2 Satellite Pre-Shipment Storage

In the event that the Satellite is completed prior to the contractually scheduled delivery date, BATC shall provide, at their cost, suitable environmentally controlled storage including temperature and humidity monitoring and recording.

If shipment is delayed due to BATC beyond the contractually scheduled delivery date and the Satellite is complete, and such delay by BATC has caused a loss of available launch opportunity, the Satellite shall be placed in storage at BATC’s expense.

If shipment is delayed due to DigitalGlobe beyond the contractually scheduled delivery date and the Satellite is complete, the Satellite shall be placed in storage at DigitalGlobe’s expense.

11.3 Pre-Shipment Re-Test

Subject to the length of the storage period, appropriate maintenance and power up of those units sensitive to inactivity shall be undertaken. Any items exhibiting signs of deterioration shall be subject to appropriate follow up action according to the circumstances. All instances shall be reported to DigitalGlobe.

A thorough re-test is required should the storage exceed [**Redacted**] . Details shall be provided in the test requirements document. Appropriate follow up action shall be taken, according to the circumstances, should any problems be detected.

The re-test costs shall be at BATC expense if delay and retest were caused by BATC. The re-test costs shall be at DigitalGlobe’s expense if delay and retest were caused by DigitalGlobe.

11.4 Satellite Shipping and Delivery

[**Redacted**]

BATC shall provide shipping from BATC plant to the launch site. BATC shall pack the Satellite and ground support equipment in suitable containers for shipment to the launch site. BATC shall unpack the Satellite and ground support equipment at the payload processing facility at the launch site.

BATC shall provide insurance and security for the satellite and ground support equipment during shipment to the launch site.

BATC shall pack the ground support equipment for return to BATC plant and provide shipping.

BATC shall provide insurance for the ground support equipment during shipment back to BATC plant.

The transportation environment shall be enveloped by the requirements in the Launch Vehicle and Instrument ICD and performance specification. BATC shall be responsible for ensuring the Satellite compatibility with the requirements. BATC shall be responsible for verifying all environmental requirements are met including temperature, humidity, and shock monitoring.

11.5 Satellite Launch Site Storage

BATC shall provide volumetric storage and access requirements to DigitalGlobe for shipping containers required at the launch site. The baseline program assumes no Satellite storage requirements at the launch site. However, if the launch should be delayed once the Satellite has been shipped, BATC shall provide, at DigitalGlobe expense, the support necessary to maintain, store, and retest the Satellite.

 

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12.0 Launch Support Services

BATC shall provide launch support services as defined in the following paragraphs.

12.1 General

[**Redacted**] DigitalGlobe will be responsible for overall coordination of launch activities. BATC shall support this activity as defined in this section of the SOW.

The Satellite shall be compatible with U.S. launch safety requirements. BATC shall generate a WV3 Missile System Pre-launch Safety Package (MSPSP) (CDIL LM-1) to document hazardous items or operations and planned safety procedures for the Satellite.

BATC shall support the safety review processes of the Launch Services Contractor and the Launch site.

12.2 Requirement Definition

BATC shall support the generation and maintenance of the Launch Vehicle ICD as defined in paragraph 5.3.12. BATC shall supply the following information and any other information normally required by the Atlas V Launch Services User’s Guide to DigitalGlobe and the Launch Services contractor:

 

  a. Launch vehicle interface details and requirements.

 

  b. Requirements for launch site support and services including space, power, environment, contamination control, lifting/moving, telecommunications, etc.

 

  c. Statement of compliance with launch site safety requirements.

 

  d. Environmental requirements pre and post installation on launch vehicle.

 

  e. Verification of applicable portions of the Satellite to Launch Vehicle ICD.

 

  f. Launch Site Procedures.

BATC shall, by means of drawings, analysis, or test, be responsible for specifically confirming Satellite compatibility with the launch vehicle requirements defined in the ICD. BATC shall prepare a RVCM, as defined in paragraph 5.3.6, for those portions of the ICD for which it has responsibility.

12.3 Technical Interchange Meetings

BATC shall support up to twenty Technical Interchange Meetings (TIM) with the launch organization . [**Redacted**] In addition, BATC will support informal meetings and teleconferences at DigitalGlobe’s Colorado facilities and BATC facility as required resolving interface and infrastructure issues.

12.4 FEM and CLA-to-Design Load Comparisons (CDIL LM-2)

BATC shall provide preliminary Finite Element Models (FEM) and final FEMs for the WV3 Satellite for the purposes of performing coupled loads analyses. DigitalGlobe is responsible for obtaining valid CLA results from the launch service contractor and delivering those to BATC. BATC shall then compare the results of the coupled loads analyses to the design loads used in spacecraft bus and Instrument structural analysis to confirm that the resulting loads are within the design requirements as specified in the respective ICDs. The deliverables are as follows:

[**Redacted**]

12.5 Export Regulations

All contractors on this program are anticipated to be U.S. companies including the launch service contractor. Therefore we anticipate no exports of hardware, software, or technology to foreign companies. However, if that situation changes, DigitalGlobe shall be the single point of contact for all export issues. Therefore:

BATC shall provide information directly to DigitalGlobe and DigitalGlobe will be responsible for obtaining and documenting all export approvals for all documentation transmitted to the launch vehicle agencies.

 

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WV3 Satellite Statement of Work_

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DigitalGlobe will be responsible for all work associated with compliance to export regulations including licensing, security, customs, document approval, transportation, etc. for documents/data channeled through DigitalGlobe.

It is understood that the Department of State International Traffic in Arms regulations (CFR 22 Part 120 through 130) strictly apply to any data or hardware covered under this SOW.

12.6 Adapter Fit-Check

BATC shall perform a launch vehicle interface check on the satellite as defined in the Test Plan. DigitalGlobe will arrange for the launch services contractor to provide the adapter, interface portions of the separation system, and GSE. If required, DigitalGlobe will also arrange for support from the launch services contractor at no cost to BATC.

12.7 Launch Site Infrastructure

DigitalGlobe shall arrange for and provide all launch site infrastructure necessary for satellite testing and pre-launch processing. This includes lease of a satellite processing facility.

12.8 Launch Site Operations

BATC shall support the launch operations campaign including provision of the test equipment and labor required to perform the launch site unpacking, Satellite checkout as defined by the WV I&T Plan, fueling, final mating to launch vehicle, launch, and repacking for return to BATC plant. Delays associated with BATC performance shall be at BATC expense. Any other delays shall be at DigitalGlobe expense. BATC will be responsible to support meetings for the purpose of coordinating launch site operations including joint operations with the launch services contractor. All efforts associated with reprocessing due to a cancelled or aborted launch shall be at DigitalGlobe expense.

12.9 Fueling

BATC shall prepare a fueling plan and the procedures required for fueling the Satellite using an appropriate fueling cart. BATC shall prepare the fueling equipment for hydrazine loading operations and package for shipment to the launch site. BATC shall be responsible for a single fuel loading operation unless multiple fuelings are required due to reasons under BATC’s control.

BATC shall provide all required consumables, propellant, safety training, and safety equipment including SCAPE gear required to effectively and safely perform satellite fueling operations. DigitalGlobe shall arrange for disposal of all hazardous wastes and any excess materials through its Launch Services provider.

BATC shall provide support to the launch vehicle/range contractor as required to respond to range specific requirements as they pertain to the handling of the hydrazine operations.

 

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WV3 Satellite Statement of Work_

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13.0 Mission Preparation and On-Orbit Commissioning

BATC shall assist with Mission preparation and On-orbit Commissioning by performing the following tasks and engineering services.

13.1 Training (CDIL LM-3 )

13.1.1 Training Materials

BATC shall develop a training package for each satellite subsystem including the operation of the Instrument to address specifically the changes between WV-2 and WV3. The training package will be based on the Subsystem Description Documents (Paragraph 5.3.10 ) and include the same minimum information.

The training packages will be delivered on both paper and electronic media.

13.1.2 Training Sessions

For each subsystem, a cognizant BATC subsystem engineer shall present the training materials from paragraph 13.1.1. DigitalGlobe will provide the conference room and necessary projectors to support the presentation. DigitalGlobe reserves the right to videotape the training sessions for the purpose of training future DigitalGlobe personnel.

13.2 Command and Telemetry Handbook (CDIL LM-4)

BATC shall prepare a command and telemetry handbook. This document shall provide a definitive listing of all satellite telemetry and commands with a full description for each. The handbook shall meet the requirements identified in WV159.

13.3 Bus Subsystem Calibration Tools (CDIL LM-5)

BATC shall provide the subsystem calibration tools necessary for on-orbit calibration activities. Depending upon the final satellite design, these tools include but may not be limited to:

[**Redacted**]

13.4 DigitalGlobe Procedure Development Support

DigitalGlobe will generate the on-orbit procedures for the WV3 satellite(s). BATC shall understand the DigitalGlobe Concept-of-Operations and assist the procedure development. BATC shall review DigitalGlobe developed procedures for technical, operational, and safety concerns. [**Redacted**]

13.5 Commissioning Plan (CDIL LM-6)

DigitalGlobe shall generate the Commissioning Plan for the WV3 satellite. BATC shall assist the commissioning plan development. This includes assisting with the definition of the nominal sequence of events, required prerequisites, allowed out-of-sequence events, and required technical support for each event. DigitalGlobe will provide information about ground contacts, mission control center operations, and other necessary ground information used to create the commissioning plan(s).

The Commissioning Plan shall include subsystem initialization, calibration, and demonstration of performance requirements including, but not limited to, the following:

[**Redacted**]

 

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WV3 Satellite Statement of Work_

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13.6 Anomaly Preparations

DigitalGlobe will generate anomaly resolution flow-charts. BATC shall assist with the anomaly flow-chart development including defining the probable anomalies and proper recovery actions/sequences. BATC shall review DigitalGlobe anomaly resolution flow-charts for technical, operational, and safety concerns.

13.7 Satellite Commissioning

13.7.1 Launch and Early Operations (LEOP) Phase

DigitalGlobe shall direct Satellite Launch and Early Operations. BATC shall provide a dedicated engineer for all satellite subsystems except for the Instrument subsystem. This support will run 24 hours per day for up to 7 days at the DigitalGlobe Mission Control Center in Longmont, CO.

13.7.2 Verification and Calibration (V&C) Phase

DigitalGlobe shall conduct the Verification and Calibration activities necessary to achieve Full Operational Capability (FOC). This includes but is not limited to satellite calibration activities such as star tracker and gyroscope calibrations.

Barring anomalies, V&C activities will nominally occur between 0600 and 1800 hours seven days per week. V&C activities will nominally require 30 days. BATC shall provide a dedicated engineer for all satellite subsystems except for the Instrument subsystem.

BATC shall also provide off-hour, on-call engineering support during V&C. A 30 minute or less call-back response is required.

 

13.7.2.1 Commissioning Reports (CDIL LM-7)

BATC shall produce a Commissioning Report. The report will document spacecraft bus Beginning-of-Life (BOL) performance and will update End-of-Life (EOL) performance predictions for all subsystems for which it has responsibility. At a minimum the report shall include:

 

  a. An explanation of significant deviations from performance metrics as identified in the satellite specification. The explanation shall include the reasons for the performance delta and the anticipated effects, if any, on the subsystem or satellite.

 

  b. An explanation of any known component or sub-component failures encountered during the LEOP or V&C Phases. The explanation shall include the possible causes of the failure, workarounds, updated reliability analysis for the component, subsystem, and satellite, and any impacts to DigitalGlobe’s concept of operation.

13.8 Satellite Simulator

BATC shall provide a high fidelity dynamic satellite simulator. The simulator shall simulate satellite responses to stimuli. BATC shall provide sufficient documentation to accurately capture the design, functionality, capabilities, limitations, maintenance, extension, and operation of the simulator.

13.8.1 Satellite Simulator (CDIL LM-8)

BATC shall deliver a high fidelity satellite simulator per the requirements document [**Redacted**] . [**Redacted**] BATC and DigitalGlobe shall mutually agree upon a computer hardware and operating system, called the computing platform, for use in simulator functional and performance acceptance testing. BATC shall execute spacecraft simulator acceptance testing on the identified platform. DigitalGlobe shall execute the simulator testing on the same platform.

The satellite simulator does not need to include the MGB subsystem.

13.8.2 Documentation (CDIL LM-9)

BATC shall provide a User’s manual with sufficient detail to:

 

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WV3 Satellite Statement of Work_

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Develop simulation scenarios including all configuration files, scripts, procedures, ephemeris, initial conditions, etc

 

   

Start-up, shut-down, and operate the simulation console and all simulator components

 

   

Control the simulation in real-time by setting/adjusting variables

 

   

Inspect low level model telemetry through the simulation console and simulator components directly

 

   

Save, modify, and load simulator state files used to start, pause, resume, and diagnose simulation scenarios

 

   

Understand all log files and log entries

 

   

Understand and recover from all error conditions

 

   

Extend, modify, maintain, build and release the simulator.

 

   

Incorporate a new flight software release into the simulator

In this context, “maintain” refers to the functions required to upgrade to new versions of commercial products such as MatLab or Simulink, alter configuration files, or otherwise customize the implementation.

13.8.3 Source Code (CDIL LM-10)

Per the terms of the software license agreement set forth in the Agreement, BATC shall provide all BATC developed bus simulator software components in source format (non binary). Source code shall be delivered in originating and native format. BATC does not need to provide development tools or COTS software, but BATC shall provide COTS software tool configuration including supplier, part number, and revision levels of tools used (e.g. compilers, linkers, and other development tools) and all reasonable data/information necessary for DigitalGlobe to enhance, modify, compile, and deploy the simulator.

13.8.4 Delivery Schedule

BATC shall provide the simulator, manuals, and source code per Attachment 1. BATC shall deliver an updated simulator based upon LEOP/commissioning on-orbit performance. At a minimum, the following subsystem models will be updated: thermal, power, and ADCS models.

13.8.5 Technical Interchange Meetings and Design Reviews

BATC shall include DigitalGlobe in technical interchange meetings and design reviews such that DigitalGlobe can explain the intent behind various simulator requirements. BATC and DigitalGlobe shall refine high level requirements to detailed requirements during technical interchange meetings. BATC shall hold preliminary and critical design reviews for the Satellite Simulator. BATC shall hold intermediate Technical Interchange Meetings for the following modules at a minimum: the console, sensor and actuator models, redundancy modeling, fault modeling, thermal modeling, and power modeling.

13.9 Maneuver Planners

[**Redacted**]

13.9.1 [**Redacted**]

[**Redacted**]

 

13.9.2 [**Redacted**]

[**Redacted**]

 

13.9.3 [**Redacted**]

[**Redacted**]

 

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13.10 Software Test Bench

BATC shall maintain a test bench suitable for the development and troubleshooting of the satellite computer Flight Software. The bench will include at a minimum:

[**Redacted**]

13.11 Ground Stations

DigitalGlobe is responsible for all Ground Station equipment. DigitalGlobe operators will be the lead operators of the Ground Segment.1

13.12 Telemetry Packet Creation and Mapping Tools (CDIL LM-15)

BATC shall provide the documentation, software, and training necessary for making changes to the telemetry received from the satellite. This includes changes to both telemetry packets and the mapping of those packets into various telemetry streams under CCSDS Grade C protocol.

Initial delivery shall coincide with initial delivery of the Command & Telemetry Handbook (C&TH). BATC shall update if necessary at a. launch minus 6 months, b. final pre-launch C&TH delivery, and c. launch plus 6 months. Training shall occur coincident with Training Sessions specified in section 13.1 with delta training, if needed, at the final pre-launch C&TH delivery.

13.13 Telemetry Monitor and Response (CDIL LM-16)

BATC shall provide the documentation, software, and training necessary for making changes to flight software telemetry monitors and response actions on the satellite. This includes creation of new telemetry monitors and response actions, and changes to existing monitors and response actions.

Initial delivery shall coincide with initial delivery of the Command & Telemetry Handbook (C&TH). BATC shall update if necessary at a. launch minus 6 months, b. final pre-launch C&TH delivery, and c. launch plus 6 months. Training shall occur coincident with Training Sessions specified in section 13.1 with delta training, if needed, at the final pre-launch C&TH delivery.

14.0 Communications Flexibility and TT&C Definition

BATC shall work with DigitalGlobe to set/finalize satellite ID’s by CDR.

15.0 Facilities

BATC shall provide all facilities necessary to perform the scope of this SOW.

 

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WV3 Satellite Statement of Work_

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ATTACHMENT 1 CONTRACT DATA ITEMS LIST

 

Data

Item

  

Title

  

SOW
Ref

  

Initial Submittal

  

Updates

  

Comments

PROGRAM MANAGEMENT

PM-1    Program Management Structure    4.2    [**Redacted**]    As req’d   
PM-2    Master Program Schedule    4.4    [**Redacted**]    monthly   
PM-3    Component/Subsystem Design Review Listing    4.5.4    [**Redacted**]    As req’d   
PM-4    Component/Subsystem Test Readiness / Data Review Listing    4.5.5    [**Redacted**]    As req’d   
PM-5    Documentation Listing    4.6.3    [**Redacted**]   

No later than

Bi-monthly

  
PM-6    Action Item List    4.7    [**Redacted**]    As req’d   
PM-7    Historical Record of Payments & Payments Forecast    4.8.1 & 4.8.2    [**Redacted**]    monthly   

DESIGN

D-1    Satellite to Instrument ICD    5.3.1    [**Redacted**]    As req’d   
D-2    Satellite to Ground Station Narrowband ICD    5.3.2    [**Redacted**]    As req’d   
D-3    Satellite to Ground Station Wideband Link ICD    5.3.3    [**Redacted**]    As req’d   
D-4    Satellite Environmental Design and Test Specification    5.3.4    [**Redacted**]    As req’d   
D-5    Contamination Control Plan    5.3.5    [**Redacted**]    As req’d   
D-6    Satellite Level Requirements Verification/Compliance Matrix    5.3.6    [**Redacted**]    As req’d   
D-7    Box Level Requirements Verification/Compliance Matrix    5.3.7    [**Redacted**]    As req’d   
D-8    Drawings    5.3.8    [**Redacted**]    with EOs   
D-9    Performance Compliance Matrix    5.3.9.1    [**Redacted**]    Quarterly   
D-10    Risk Management Report    5.3.9.2    [**Redacted**]    Monthly   
D-11    Subsystem Description Docs    5.3.10    [**Redacted**]   

Launch –4 m;

Launch + 4 m

   Updates only as required
D-12    Thermal Analysis and Reports    5.3.11.a    [**Redacted**]    As req’d   
D-13    Structural Analysis    5.3.11.b    [**Redacted**]    As req’d   
D-14    Control System Analysis    5.3.11.c    [**Redacted**]    As req’d   
D-15    Failure Modes and Effects and Criticality Analysis (FMECA)    5.3.11.d    [**Redacted**]    As req’d   
D-16    Satellite Reliability Analysis    5.3.11.e    [**Redacted**]    As req’d   
D-17    Satellite Imaging Performance    5.3.11.h    [**Redacted**]    As req’d   
D-18    Critical Items List    5.3.13    [**Redacted**]    As req’d   
D-19    Component Heritage Summary    5.3.14    [**Redacted**]    As req’d   
D-20    System Engineering Reports    5.3.16    [**Redacted**]      
D-21    Flight Software Code    5.3.16    [**Redacted**]    As req’d Final @ PSR   
D-22    Composite Grounding Design    5.3.17    [**Redacted**]    As req’d   

 

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Attch 1 - 1


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WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

 

Data

Item

  

Title

  

SOW
Ref

  

Initial Submittal

  

Updates

  

Comments

D-23

   Structural, Power, Thermal, and Reliability Analytical Models    5.3.18    [**Redacted**]    L+3 m   

D-24

   Coordinate Transformation Document    5.3.19    [**Redacted**]    L – 4m   

D-25

   Flight Software Users Manual    5.3.20    [**Redacted**]    As req’d   

D-26

   Component Acceptance Data Package    5.3.21    [**Redacted**]    As req’d   

D-27

   Jitter Analysis and Test Data    5.3.22    [**Redacted**]    As req’d   

D-28

   Telescope Boresight Stability Data    5.3.23    [**Redacted**]    As req’d   

D-29

   Position and Attitude Accuracy    5.3.24    [**Redacted**]    As req’d   

D-30

   PDR Data Package    4.5.3    [**Redacted**]    As req’d   

D-31

   CDR Data Package    4.5.3    [**Redacted**]    As req’d   

D-32

   Satellite to MGB ICD    5.3.25    [**Redacted**]    As req’d   

D-33

   Electrical GSE ICD    5.3.26    [**Redacted**]    As req’d   

D-34

   Satellite Requirements Review    4.5.3.1    [**Redacted**]      

D-35

   Battery Life Prediction    5.3.11.g    [**Redacted**]    L+ 1m   

PRODUCT ASSURANCE

QA-1

   EEE Parts List    6.2.1    [**Redacted**]      

QA-2

   Material Identification and Use Listing    6.2.2    [**Redacted**]    See para 6.3.2   

QA-3

   As built configured article list    6.3.1    [**Redacted**]   

At Launch

Readiness

Review

  

QA-4

   Certification of Conformance    6.3.2    [**Redacted**]      

QA-5

   Product Assurance Reviews    6.4    [**Redacted**]      

PROCUREMENT, PRODUCTION & TEST

PT-1

   Make / Buy Plans    7.2    [**Redacted**]    As req’d   

PT-2

   Program Subcontract Status Report    7.5    [**Redacted**]    monthly   

PT-3

   WV I&T Plan    9.3    [**Redacted**]    As req’d   

PT-4

   Battery Maintenance Plan    9.3.e    [**Redacted**]    As req’d   

PT-5

   System Test Reports    9.6    [**Redacted**]      

PT-6

   I&T Command and Telemetry Log Files    9.8.4    [**Redacted**]    weekly   

PT-7

   Reserved    Na    [**Redacted**]      

PT-8

   Instrument Integration Readiness Review Data Package    4.5.3    [**Redacted**]      

PT-9

   Satellite Environmental Testing Readiness Review Data Package    4.5.3    [**Redacted**]      

PT-10

   Pre-Ship Review Data Package    4.5.3    [**Redacted**]      

LAUNCH AND MISSION

LM-1

   Missile Systems Pre-Launch Safety Package (MSPSP)    12.1    [**Redacted**]   

L-52 wks TBD

L-26 wks TBD

  

LM-2

   Preliminary WV3 FEM    12.4.a    [**Redacted**]      
   Preliminary CLA-to-WV3 Design Loads Comparison    12.4.b    [**Redacted**]      

 

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Attch 1 - 2


LOGO

 

WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

Data

Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

   Final WV3 FEM    12.4.c    [**Redacted**]      
   Final CLA-to-WV3 Design Loads Comparison    12.4.d    [**Redacted**]      

LM-3

   Training Materials and sessions    13.1.1    [**Redacted**]    As revised   

LM-4

   Command &Telemetry Handbook    13.2    [**Redacted**]    As revised   

LM-5

   Calibration Tools    13.3    [**Redacted**]   

As revised &

L+3 m

  

LM-6

   Commissioning Plan    13.5    [**Redacted**]    As revised   

LM-7

   Commissioning Report    13.7.2.1    [**Redacted**]      

LM-8

   Satellite Simulator    13.8.1    [**Redacted**]   

See Para

3.1.b

  

LM-9

   Satellite Simulator Documentation    13.8.2    [**Redacted**]    With LM-8   

LM-10

   Satellite Simulator Source Code    13.8.3    [**Redacted**]    With LM-8   

LM-11

   High Fidelity Maneuver Planner    13.9.1    [**Redacted**]      

LM-12

   Peak Estimator Algorithm    13.9.2    [**Redacted**]      

LM-13

   Integrative Maneuver Model    3    [**Redacted**]      

LM-14

   Satellite Launch Readiness Review Data Package    4.5.3    [**Redacted**]      

LM-15

   Telemetry Packet Creation and Mapping Tools    13.12    [**Redacted**]    See 13.12   

LM-16

   Telemetry Monitor and Response    13.13    [**Redacted**]    See 13.13   

[**Redacted**]

[**Redacted**]

   [**Redacted**]    4.5.3.1    [**Redacted**]      

[**Redacted**]

   [**Redacted**]    4.5.3.1    [**Redacted**]      

[**Redacted**]

   [**Redacted**]    4.5.3.1    [**Redacted**]      

[**Redacted**]

   [**Redacted**]    4.5.3.1    [**Redacted**]      

[**Redacted**]

   [**Redacted**]    4.5.3.1    [**Redacted**]      

[**Redacted**]

   [**Redacted**]    4.5.3.11.i    [**Redacted**]    As rqd   

[**Redacted**]

   [**Redacted**]    4.5.3.11.j    [**Redacted**]      

[**Redacted**]

   [**Redacted**]    4.5.3.11.k    [**Redacted**]      

 

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Attch 1 - 3


LOGO

 

WV3 Satellite Statement of Work_

Doc Number 10329656

 
 

 

Data

Item

  

Title

  

SOW Ref

  

Initial Submittal

  

Updates

  

Comments

[**Redacted**]

   [**Redacted**]    4.5.3.11.l    [**Redacted**]      

[**Redacted**]

   [**Redacted**]    4.5.3.11.m    [**Redacted**]      

All items are provided for DigitalGlobe information only. Approvals are not required except for ICDs, changes to ICDs, and as otherwise noted.

ATP +1m is 1 month after Authorization to Proceed.

 

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WV3 Satellite Statement of Work_WV862

Rev 1.0: 26 January 2007

 
 

 

ATTACHMENT 2 CUSTOMER FURNISHED EQUIPMENT LIST

 

Item

  

Title

  

SOW
Ref

  

Date

  

Comment

FLIGHT HARDWARE

CFHW-1

   [**Redacted**]    10.2.1    [**Redacted**]   

CFHW-2

   [**Redacted**]    10.2.2    [**Redacted**]    Flight and corresponding ground keys.

CFHW-3

   [**Redacted**]    10.2.3    [**Redacted**]   

CFHW-4

   [**Redacted**]    10.2.4    [**Redacted**]   

CFHW-5

   [**Redacted**]    10.2.5    [**Redacted**]   

CFHW-6

   [**Redacted**]    10.2.6    [**Redacted**]   

[**Redacted**]

           

CSIM-1

   [**Redacted**]    10.3    [**Redacted**]    Remains the property of DG

[**Redacted**]

           

CLSE-1

   [**Redacted**]    10.4.1    [**Redacted**]   

CLSE-2

   [**Redacted**]    10.4.1    [**Redacted**]   

CLSE-3

   [**Redacted**]    10.4.2    [**Redacted**]   

[**Redacted**]

           

CGSE-1

   [**Redacted**]    10.5.1.a    [**Redacted**]    Remains the property of DG

CGSE-2

   [**Redacted**]    10.5.1.b    [**Redacted**]    Remains the property of DG

CGSE-3

   [**Redacted**]    10.5.1.c    [**Redacted**]    Remains the property of DG

CGSE-4

   [**Redacted**]    10.5.1.d    [**Redacted**]    Remains the property of DG

CGSE-5

   [**Redacted**]    10.5.2.    [**Redacted**]    Remains the property of DG

CGSE-6

   [**Redacted**]    10.5.2.0    [**Redacted**]    Remains the property of DG

CGSE-7

   [**Redacted**]    10.5.2.0    [**Redacted**]    Remains the property of DG

CGSE-8

   [**Redacted**]    10.5.3.a    [**Redacted**]    Remains the property of DG

CGSE-9

   [**Redacted**]    10.5.3.b    [**Redacted**]    Remains the property of DG

CGSE-10

   [**Redacted**]    10.5.3.c    [**Redacted**]    Remains the property of DG

CGSE-11

   [**Redacted**]    10.5.4    [**Redacted**]    Remains the property of DG

CGSE-12

   [**Redacted**]    10.5.5    [**Redacted**]    Remains the property of DG

CGSE-13

   [**Redacted**]    10.5.6    [**Redacted**]    Remains the property of DG

CGSE-14

   [**Redacted**]    10.5.7    [**Redacted**]    Remains the property of DG

CGSE-15

   [**Redacted**]    10.5.8    [**Redacted**]    Remains the property of DG

CGSE-16

   [**Redacted**]    10.5.9    [**Redacted**]    Remains the property of DG
LAUNCH VEHICLE DATA ITEM

CLD-1

   WV3 Preliminary CLA    10.6    [**Redacted**]   

CLD-2

   WV3 Final CLA    10.6    [**Redacted**]   
INSTRUMENT DATA ITEM

CID-1

   WV3 Instrument Structural Data    10.7.1    [**Redacted**]   

CID-2

   WV3 Instrument Thermal Data    10.7.2    [**Redacted**]   

DigitalGlobe will provide this equipment in accordance with the requirements of the Agreement.

 

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1


Attachment 2

DigitalGlobe WorldView-3 Satellite Specification, Rev 8.0

Dated 2 November 2011

ITAR Controlled Document


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THE EXHIBIT MARKED BY [**Redacted**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION.

 

LOGO   Exhibit 2 to Contract 60150

WorldView-3 Satellite

Specification

 

Document #

   10329655

Revision #

   8.0

Release Date

   2 Nov 2011

Prepared by

   George Hunyadi

Approved by

   Keith Constantinides

This Document Is ITAR Controlled

This document contains Technical Data as defined and controlled under the International Traffic In Arms Regulations (ITAR). Transfer of this data by any means to a foreign person, whether in the United States or abroad, without an export license or other approval from the U.S. Department of State is prohibited.

RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION

This document contains information proprietary and confidential to DigitalGlobe , to its subsidiaries, or to a third party to whom DigitalGlobe may have a legal obligation to protect such information from unauthorized disclosure, use or duplication. Any disclosure, use or duplication of this document or of any of the information contained herein for other than the specific purpose for which it was disclosed is expressly prohibited, except as DigitalGlobe may otherwise agree to in writing. This document may only be used for the purpose for which it is provided. All copies of this document are the sole property of DigitalGlobe and will be returned promptly upon request.


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WorldView-3 Satellite Specification

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Rev 8.0: 2 Nov 2011

 
 

 

Change Record

 

Revision

  

Date

  

Sections

  

Description of Change

1.0

   20 Aug 2010    All    Initial Release

[**Redacted**]

        

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

Table of Contents

 

1. SCOPE

     1   

1.1 P URPOSE

     1   

1.2 S YSTEM O VERVIEW

     1   

1.3 D OCUMENT O VERVIEW

     1   

2. APPLICABLE DOCUMENTS

     1   

2.1 G OVERNMENT D OCUMENTS

     2   

2.1.1 [**Redacted**]

     2   

2.1.2 [**Redacted**]

     2   

2.2 N ON - GOVERNMENT D OCUMENTS

     2   

2.2.1 [**Redacted**]

     2   

2.2.2 [**Redacted**]

     2   

2.2.3 [**Redacted**]

     2   

2.3 R EFERENCE D OCUMENTS

     2   

3. REQUIREMENTS

     2   

3.1 S ATELLITE D EFINITION

     2   

3.1.1 Satellite Diagrams

     2   

3.1.1.1 Component Tree

     2   

3.1.1.2 Coordinate System

     2   

3.1.2 Satellite Interfaces

     3   

3.1.2.1 Non-interference with Outside Systems

     3   

3.1.2.1.1 [**Redacted**

     3   

3.1.2.1.2 [**Redacted**]

     3   

3.1.2.1.3 [**Redacted**]

     3   

3.1.2.2 Satellite-Global Positioning System Interfaces

     3   

3.1.2.2.1 Compatibility

     3   

3.1.2.3 Satellite-Ground Interfaces

     3   

3.1.2.3.1 Compatibility

     3   

3.1.2.3.2 Remote Ground Terminal Locations

     3   

3.1.2.3.3 Command Uplink

     3   

3.1.2.3.4 Narrowband Telemetry Downlink

     3   

3.1.2.3.5 Wideband Data Downlink

     4   

3.1.2.4 Satellite-Launch Vehicle Interfaces

     4   

3.1.2.4.1 Compatibility

     4   

3.1.2.4.2 [**Redacted**]

     4   

3.1.2.4.3 Umbilical

     4   

3.1.3 Customer Furnished Equipment

     4   

3.1.3.1 Instrument

     4   

3.1.3.1.1 Physical, Structural and Mechanical Requirements

     4   

3.1.3.1.2 Thermal Interfaces

     5   

3.1.3.1.3 Power Interfaces

     5   

3.1.3.1.4 Command and Telemetry Interfaces

     5   

3.1.3.1.5 Image Data Interfaces

     6   

3.1.3.1.6 EOA Thermal Control Interfaces

     6   

3.1.3.1.7 [**Redacted**]

     6   

3.1.3.2 MGB

     6   

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

3.1.3.3 [**Redacted**]

     6   

3.1.3.3.1 [**Redacted**]

     6   

3.1.3.3.2 [**Redacted**]

     7   

3.1.3.3.3 [**Redacted**]

     7   

3.1.3.3.4 [**Redacted**]

     7   

3.1.3.3.5 [**Redacted**]

     8   

3.1.3.3.6 [**Redacted**]

     8   

3.1.4       [**Redacted**]

     8   

3.1.4.2    [**Redacted**]

     8   

3.1.4.3    [**Redacted**]

     8   

3.1.4.3.1 [**Redacted**]

     8   

3.1.4.3.2 [**Redacted**]

     8   

3.1.4.4    [**Redacted**]

     8   

3.1.4.4.1 [**Redacted**]

     8   

3.1.4.4.2 [**Redacted**]

     8   

3.1.4.4.3 [**Redacted**]

     8   

3.1.4.4.4 [**Redacted**]

     8   

3.1.4.4.6 [**Redacted**]

     9   

3.2 S ATELLITE C HARACTERISTICS

     9   

3.2.1 Performance

     9   

3.2.1.1 General Mission Requirements

     9   

3.2.1.1.1 Mission Life

     9   

3.2.1.1.2 Orbits

     9   

3.2.1.2 Satellite Operating Modes

     9   

3.2.1.2.1 Normal Operating Modes

     9   

3.2.1.2.2 Special / Contingency Modes

     10   

3.2.1.2.3 Intermediate and Transitional Modes

     11   

3.2.1.3 Pre-Launch Operations

     11   

3.2.1.3.1 Ground Storage

     11   

3.2.1.3.2 Launch Delay

     11   

3.2.1.4 Early Orbit Operations

     11   

3.2.1.4.1 Autonomous Operations After Separation

     11   

3.2.1.4.2 First [**Redacted**]

     12   

3.2.1.4.3 Commissioning

     12   

3.2.1.5 Mission Operations

     12   

3.2.1.5.1 Viewing Angles

     12   

3.2.1.5.2 Imaging and Downlink Operations

     12   

3.2.1.5.3 Stereo Imaging

     12   

3.2.1.5.4 Off-Nadir Imaging

     12   

3.2.1.5.5 [**Redacted**]

     13   

3.2.1.5.6 [**Redacted**]

     13   

3.2.1.6 Instrument Requirements

     13   

3.2.1.6.1 Integrated Bus/Instrument Performance Effects

     13   

3.2.1.6.2 [**Redacted**]

     13   

3.2.1.6.3 [**Redacted**]

     13   

3.2.1.6.4 Instrument Cleanliness

     14   

 

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3.2.1.7 Bus Subsystem Requirements

     14   

3.2.1.7.1 [**Redacted**]

     15   

3.2.1.7.2 ADCS

     16   

3.2.1.7.3 Propulsion

     18   

3.2.1.7.4 Flight Software

     18   

3.2.1.7.5 C&DH

     19   

3.2.1.7.6 Narrowband Communications

     23   

3.2.1.7.7 [**Redacted**]

     24   

3.2.1.7.8 EPDS

     27   

3.2.1.7.9 Structures and Mechanisms

     28   

3.2.1.7.10 Thermal Control

     29   

3.2.1.7.11 Direct Tasking

     30   

3.2.2 Physical Characteristics

     33   

3.2.2.1 Size Constraints

     33   

3.2.2.2 Mass Constraints

     33   

3.2.2.3 Shipping Constraints

     33   

3.2.3 Reliability

     33   

3.2.3.1 End of Life Ps

     33   

3.2.3.2 [**Redacted**]

     33   

3.2.3.3 [**Redacted**]

     34   

3.2.3.4 Cycle-Limited Items

     34   

3.2.3.4.1 [**Redacted**]

     34   

3.2.3.4.2 [**Redacted**]

     34   

3.2.4 Availability and Maintainability

     34   

3.2.4.1 Fault Recovery Timeline

     34   

3.2.4.2 Environmental Conditions

     34   

3.2.4.2.1 Launch Induced Environments

     34   

3.2.4.2.2 On-Orbit Environments

     34   

3.2.4.2.3 Pre-Launch Environments

     34   

3.3 S ATELLITE D ESIGN A ND C ONSTRUCTION

     34   

3.3.1 General

     34   

3.3.2 SEUs

     35   

3.3.3 Immunity to Latch-Up

     35   

3.3.4 Cleanliness and Contamination Control

     35   

3.3.4.1 [**Redacted**]

     35   

3.3.4.2 [**Redacted**]

     35   

3.3.4.3 [**Redacted**]

     35   

3.3.4.4 [**Redacted**]

     35   

3.3.5 Safety

     35   

3.3.6 [**Redacted**]

     35   

4. VERIFICATION

     35   

5. QUALITY ASSURANCE

     35   

 

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List of Tables

[**Redacted**]

List of Figures

[**Redacted**]

 

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V


1. SCOPE

1.1 Purpose

This document describes the requirements for design and implementation of the DigitalGlobe WorldView-3 Satellite, being constructed to support DigitalGlobe commercial imaging operations.

1.2 System Overview

Ball Aerospace & Technology Corporation (BATC) is providing the integrated WorldView-3 imaging satellite to DigitalGlobe, Inc. As the Space Segment Integrator (SSI), BATC is manufacturing a Spacecraft Bus that can accommodate the panchromatic + multi-spectral WorldView-3 Instrument [**Redacted**] . This will be the same Bus design as used for predecessor WorldView Satellites. The [**Redacted**] is being supplied by ITT Industries Space Systems Division (ITT) to DigitalGlobe, with miscellaneous support units / functions provided by BATC. All ITT equipment will be provided as Customer Furnished Equipment (CFE) to BATC for Satellite integration. [**Redacted**] As the SSI, BATC will then perform Satellite level testing, prepare the Satellite for launch, and support on-orbit checkout of the Satellite.

The Satellite will be in a sun-synchronous orbit at an altitude between 450 and 830 km with a descending equator crossing time between 10:00 AM and 2:00 PM. [**Redacted**] Image data is recorded by the Spacecraft Bus and is normally downlinked to DigitalGlobe ground stations. However, direct downlink to user sites may also be performed in certain circumstances. Direct downlink is via the normal wideband downlink.

A key feature of the WordView-3 Satellite is Direct Tasking, where imaging and downlink parameters are directly uplinked from a customer’s ground station to the satellite, and image data is directly downlinked to a customer’s ground station, on the same and/or successive passes. Direct Tasking supports an expanded customer base and fulfills these customers’ desires to compress the overall planning-tasking-collection-downlink timeline and to not expose their task list to outside parties (including DigitalGlobe) prior to image collection. Full command authority is maintained by DigitalGlobe, with key commands needed to initiate the image and downlink operations uploaded from DigitalGlobe ground stations.

1.3 Document Overview

This document specifies functional, performance and interface requirements for the integrated Satellite and the Spacecraft Bus, including external Satellite interfaces, Instrument-Bus interfaces and Instrument integration, Bus and Satellite test, launch, and operational requirements. Separate Interface Control Documents (ICDs) detail the specifics of the Instrument-Bus interfaces and Integration and Test processes. Satisfaction of the Satellite-level requirements contained in this specification assume the Instrument provided as CFE meets its requirements, which are documented separately. As the SSI, BATC will refer to the separate Instrument Specifications as necessary to maintain the Spacecraft Bus to Instrument ICDs and develop an integration and test plan sufficient to ensure the integrated Satellite meets its system-level functional and performance requirements.

This specification may contain requirements that have not been fully defined. These open requirements are indicated by a TBR, and/or TBD:

TBR – To Be Resolved: Indicates parameters that exist, but may change after discussions with Contractor and others (e.g.: DigitalGlobe).

TBD – To Be Determined: Indicates parameters that have not yet been determined.

 

2. APPLICABLE DOCUMENTS

This document is the Satellite Specification. This specification defines the technical requirements called out in the Contract and a Statement of Work (SOW). The Contract and SOW define schedule requirements, deliverable items and programmatics. However, in the event of a conflict between a specific requirement herein and documents, then the Contract, the Statement of Work, this document, and Applicable documents shall govern in this order. If the revision is not specifically noted, the latest revision of each document applies.

At contract signing, the Environmental Design and Test Specification and Interface Control Documents from predecessor DigitalGlobe WorldView satellite programs listed below shall be considered the baseline release for WV-3. It is anticipated that the WV-3 versions of these documents will require few modifications from the predecessor baselines, with changes focused in a few key areas as driven by WV-3 unique requirements (for example enhanced Instrument thermal control and updated power values). The first release of the WV-3 version of each document shall supersede the predecessor version, which shall no longer be considered an Applicable Document.


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Although the Satellite Integrating Contractor physically maintains many of these ICDs, their development is inherently a cooperative process. Accordingly, the latest released ICD revision shall always apply, where release is predicated on mutual agreement between all involved parties; for example the Instrument to Spacecraft ICD requires consensus between the Satellite Integrating Contractor, the Instrument Contractor, and DigitalGlobe.

2.1 Government Documents

2.1.1 [**Redacted**]

2.1.2 [**Redacted**]

2.2 Non-Government Documents

2.2.1 [**Redacted**]

2.2.2 [**Redacted**]

2.2.3 [**Redacted**]

2.3 Reference Documents

[**Redacted**]

 

3. REQUIREMENTS

Remarks contained as Rationale/Info shall NOT be considered a formal part of this specification and are provided for reference only.

[**Redacted**]

3.1 Satellite Definition

This Section defines fundamental terminology and identifies the basic Satellite functions along with the provider of each function. It also provides external interface requirements and internal interface requirements for the equipment to be provided [**Redacted**] to the SSI.

Satellite Diagrams

 

3.1.1.1  Component Tree

[**Redacted**] defines the major elements, subsystems, assemblies and units/functions of the Satellite and shows how they are allocated between DigitalGlobe’s contractors. The figure also indicates items that are delivered to the SSI [**Redacted 1 Page**].

 

3.1.1.2  Coordinate System

The base coordinate system used for all major Satellite element and segment mechanical interfaces shall be as shown in [**Redacted**] , for example, Instrument to Spacecraft Bus and Satellite to Launch Vehicle.

Other coordinate systems may be used as appropriate within elements and/or subsystems; [**Redacted**] . The relationships between the base coordinate system and other coordinate systems shall be explicitly shown in the appropriate documents (drawings, interface control documents, etc.).

[**Redacted**]

 

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3.1.2 Satellite Interfaces

3.1.2.1 Non-interference with Outside Systems

3.1.2.1.1 [**Redacted**]

The Satellite shall not interfere with [**Redacted**].

3.1.2.1.2 [**Redacted**]

During normal operations, RF emissions from the Satellite shall not exceed the limits specified in the [**Redacted**] .

3.1.2.1.3 [**Redacted**]

All RF emissions shall use the frequency allocation of [**Redacted**] , with out-of-band emissions compliant with [**Redacted**].

3.1.2.2 Satellite-Global Positioning System Interfaces

3.1.2.2.1 Compatibility

The Spacecraft Bus shall be compatible with standard GPS interfaces as defined in [**Redacted**] .

3.1.2.3 Satellite-Ground Interfaces

The following paragraphs define high-level requirements for Satellite-Ground compatibility; detailed interface requirements shall be defined in the Narrowband and Wideband Satellite-Ground ICD.

[**Redacted**]

3.1.2.3.1 Compatibility

The Satellite Narrowband and Wideband Communications Subsystems shall be compatible with [**Redacted**] .

3.1.2.3.2 Remote Ground Terminal Locations

Remote Ground Terminals (RGTs) will be located as follows:

[**Redacted**]

3.1.2.3.3 Command Uplink

3.1.2.3.3.1 Effective Isotropic Radiated Power

The minimum Effective Isotropic Radiated Power (EIRP) of the command uplink antenna will be [**Redacted** ].

3.1.2.3.3.2 Axial Ratio

The command uplink antenna will transmit using [**Redacted**] .

3.1.2.3.4 Narrowband Telemetry Downlink

3.1.2.3.4.1 Figure of Merit (G/T)

The minimum G/T of the Narrowband receive antenna will be as follows across the frequency range of [**Redacted**] under all conditions, for the RGT locations defined in Section 3.1.2.3.2 Remote Ground Terminal Locations. These values include the effects of antenna pointing error and atmospheric conditions.

[**Redacted**]

3.1.2.3.4.2 Axial Ratio

The Narrowband receive antenna will receive using [**Redacted**] .

3.1.2.3.4.3 Implementation Loss

The demodulator implementation loss for the Narrowband telemetry receiver will be [**Redacted**] .

 

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WorldView-3 Satellite Specification

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3.1.2.3.5 Wideband Data Downlink

3.1.2.3.5.1 Figure of Merit (G/T)

The minimum G/T of the Wideband receive antenna will be as follows across the frequency range of [**Redacted**] under all conditions, for the RGT locations defined in Section 3.1.2.3.2 Remote Ground Terminal Locations. These values include the effects of antenna pointing error and atmospheric conditions.

[**Redacted**]

3.1.2.3.5.2 Axial Ratio

The Wideband receive antenna will receive using [**Redacted**] .

3.1.2.3.5.3 Implementation Loss

The demodulator implementation loss for the wideband telemetry receiver will be [**Redacted**] .

 

3.1.2.4 Satellite-Launch Vehicle Interfaces

The following paragraphs define high-level requirements for Satellite – Launch Vehicle compatibility; detailed interface requirements shall be defined in the Mission Specification.

 

3.1.2.4.1 Compatibility

The Satellite design shall be compatible with the [**Redacted**]

 

3.1.2.4.2 [**Redacted**]

The Satellite shall accommodate [**Redacted**].

 

3.1.2.4.3 Umbilical

The Satellite shall accommodate an umbilical to support all required functions for launch mode, including at a minimum the following critical electrical functions:

[**Redacted**]

3.1.3 Customer Furnished Equipment

Instrument

The Instrument will be provided to the SSI [**Redacted**] . The SSI shall provide interfaces as specified herein, with detailed interface requirements provided in accordance with the [**Redacted**] .

 

3.1.3.1.1 Physical, Structural and Mechanical Requirements

3.1.3.1.1.1 Configuration

The Spacecraft Bus shall accommodate the following major Instrument assemblies and/or units:

[**Redacted**]

3.1.3.1.1.2 Size

The Spacecraft Bus shall be capable of supporting the Instrument assemblies/units as specified in the Spacecraft Bus to Instrument ICDs.

3.1.3.1.1.3 Mass Properties

[**Redacted**]

3.1.3.1.1.4 EOA-Mounted Spacecraft Bus Equipment

The SSI shall provide the following equipment to be mounted on the EOA:

[**Redacted**]

3.1.3.1.1.5 EOA Fields of View

The Spacecraft Bus shall provide the Instrument with [**Redacted**] .

3.1.3.1.1.6 EOA Purge Fitting

The Satellite shall be configured to provide a purge fitting [**Redacted**] .

 

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WorldView-3 Satellite Specification

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3.1.3.1.1.7 Assembly, Integration and Test

 

a) To the maximum extent possible, the Satellite configuration shall permit independent integration of all Instrument assemblies/units and access to internal Instrument test ports and harness connections.
b) The Satellite configuration shall allow clear access to Instrument equipment essential to integration and test activities, for example: test ports, purge lines, aperture cover, interface connectors, etc.

3.1.3.1.1.8 EOA Vibration Environment

The SI shall ensure that the [**Redacted**]

3.1.3.1.1.9 [**Redacted**]

The Spacecraft Bus shall provide radiation shielding for the [**Redacted**] .

 

3.1.3.1.2 Thermal Interfaces

The Spacecraft Bus shall perform the following thermal functions, with interfaces to the Instrument as specified in the Spacecraft Bus to Instrument ICDs:

[**Redacted**]

 

3.1.3.1.3 Power Interfaces

The Spacecraft Bus shall provide electrical power to the Instrument as specified below, with the breakdown of individual unit powers and other characteristics as specified in the Spacecraft Bus to Instrument ICDs.

Instrument Power Feeds

The Spacecraft Bus shall provide power to all Instrument units as follows:

[**Redacted**]

3.1.3.1.3.2 Voltage

The Spacecraft Bus shall present power at the Instrument interfaces as follows:

[**Redacted**]

[**Redacted**]

3.1.3.1.3.4 Average Operating Power

During normal operations, the Spacecraft Bus shall be able to perform [**Redacted**]

3.1.3.1.3.5 Survival Power

When in Emergency Mode, the Spacecraft Bus shall provide power as specified in [**Redacted**] via the Essential Bus, as specified in Section 3.1.3.1.3.1 Instrument Power Feeds.

3.1.3.1.3.6 Maximum Power

 

a) The Spacecraft Bus shall be capable of supporting the sustained maximum Instrument power specified in [**Redacted**] .

 

b) The Spacecraft Bus shall [**Redacted**]

 

3.1.3.1.4 Command and Telemetry Interfaces

The Spacecraft Bus shall provide the following command and telemetry interfaces to the Instrument, all of which shall be cross-strapped between the primary and redundant Spacecraft Bus electronics and primary and redundant Instrument electronics:

[**Redacted**]

3.1.3.1.4.1 Instrument Commanding

Using the specified data interfaces, the Spacecraft Bus shall forward commands to the Instrument, [**Redacted**] as documented in the Spacecraft Bus to Instrument ICDs.

3.1.3.1.4.2 Image Start and Stop Commands

The commands for image [**Redacted**] shall be issued from the Spacecraft Bus [**Redacted**] .

3.1.3.1.4.3 Image Duration

 

a) The minimum Image duration possible shall be no more than [**Redacted**] .

 

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WorldView-3 Satellite Specification

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b) There shall be [**Redacted**] .

 

c) Image durations shall be commandable in [**Redacted**] .

[**Redacted**]

3.1.3.1.4.4 Instrument Telemetry

Using the specified data interfaces, the Spacecraft Bus shall receive telemetry from the Instrument as documented in the Spacecraft Bus to Instrument ICDs. The following rules shall be applied to Instrument telemetry:

[**Redacted**]

3.1.3.1.4.5 [**Redacted**]

The Spacecraft Bus shall provide a [**Redacted**] as follows:

[**Redacted**]

 

3.1.3.1.5 Image Data Interfaces

The Spacecraft Bus shall provide image data interfaces [**Redacted**]

3.1.3.1.5.1 General Interface Definition

The Spacecraft Bus to Instrument data interface shall be as follows:

[**Redacted**]

3.1.3.1.5.2 Maximizing Storage and Downlink Efficiency

The Spacecraft Bus to Instrument data interface shall be capable of supporting the following Instrument configurations and shall ensure [**Redacted**]

 

3.1.3.1.6 EOA Thermal Control Interfaces

[**Redacted**]

3.1.3.1.6.1 [**Redacted**]

[**Redacted**]

3.1.3.1.6.2 [**Redacted**]

[**Redacted**]

3.1.3.1.6.3 [**Redacted**]

[**Redacted**]

 

3.1.3.1.7 [**Redacted**]

The [**Redacted**] system will be provided to the SSI [**Redacted**] . The Spacecraft Bus shall interface to the [**Redacted**] system as specified in [**Redacted**] .

 

3.1.3.2 MGB

The MGB will be provided to the SSI [**Redacted**] . The SSI shall meet the MGB requirements specified in the MGB Requirements Documents and Interface Control Documents.

 

3.1.3.3 [**Redacted**]

[**Redacted**]

 

3.1.3.3.1 [**Redacted**]

3.1.3.3.1.1 [**Redacted**]

[**Redacted**]

3.1.3.3.1.2 [**Redacted**]

 

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WorldView-3 Satellite Specification

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[**Redacted**]

3.1.3.3.1.3 [**Redacted**]

[**Redacted**]

3.1.3.3.1.4                         

[**Redacted**]

 

3.1.3.3.2 [**Redacted**]

[**Redacted**]

 

3.1.3.3.3 [**Redacted**]

[**Redacted**]

3.1.3.3.3.1                         

[**Redacted**]

3.1.3.3.3.2                         

[**Redacted**]

3.1.3.3.3.3                         

[**Redacted**] .

3.1.3.3.3.4                         

[**Redacted**]

 

3.1.3.3.4 [**Redacted**]

[**Redacted**]

3.1.3.3.4.1                         

[**Redacted**]

3.1.3.3.4.2 [**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

3.1.3.3.4.5 [**Redacted**]

[**Redacted**]

 

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3.1.3.3.5 [**Redacted**]

[**Redacted**]

3.1.3.3.5.1 [**Redacted**]

[**Redacted**]

3.1.3.3.6 [**Redacted**]

[**Redacted**]

 

3.1.4 [**Redacted**]

[**Redacted**]

 

3.1.4.1 [**Redacted**]

[**Redacted**]

3.1.4.2 [**Redacted**]

[**Redacted**]

3.1.4.3 [**Redacted**]

[**Redacted**]

3.1.4.3.1 [**Redacted**]

[**Redacted**]

3.1.4.3.2 [**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

3.1.4.4.1 [**Redacted**]

[**Redacted**]

3.1.4.4.2 [**Redacted**]

[**Redacted**]

3.1.4.4.2.1

[**Redacted**]

3.1.4.4.3 [**Redacted**]

[**Redacted**]

3.1.4.4.4 [**Redacted**]

 

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[**Redacted**]

3.1.4.5 [**Redacted**]

[**Redacted**]

3.2 Satellite Characteristics

This Section defines the characteristics of the Satellite required to support the mission with respect to performance, physical characteristics, reliability, availability, and environmental conditions. The SSI shall derive and otherwise define lower level requirements necessary to implement the requirements of this specification, including those that are passed to the Instrument Contractor via the Spacecraft Bus to Instrument ICD, the Environmental Design and Test Specification, and other relevant documents.

3.2.1 Performance

3.2.1.1 General Mission Requirements

3.2.1.1.1 Mission Life

The Satellite shall meet all on-orbit performance requirements for a Mission Life of [**Redacted**]. The end of this period is defined as End of Life (EOL).

[**Redacted**]

3.2.1.1.2 Orbits

3.2.1.1.2.1 General Orbit Compatibility

The Satellite shall be capable of operating at any equatorial altitude between [ **Redacted**]

3.2.1.1.2.2 Reserved

3.2.1.1.2.3 Mission Orbit

The Mission Orbit shall be defined as:

[**Redacted**]

3.2.1.1.2.4 Reserved

3.2.1.1.2.5 Insertion Orbit and Dispersions

The Satellite shall be compatible with being inserted directly into any of the orbits defined under General Orbit Compatibility, [**Redacted**]

 

3.2.1.2 Satellite Operating Modes

 

3.2.1.2.1 Normal Operating Modes

The Satellite shall, at a minimum, provide the operating modes defined in Table 3-4 Normal Operating Modes , with the following additional requirements:

[**Redacted**]

 

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Table 3-4 Normal Operating Modes

 

Mode

 

Basic Satellite State

 

Satellite Pointing

Cruise Mode

  [**Redacted**]   [**Redacted**]

[**Redacted**]

    [**Redacted**]

[**Redacted**]

  [**Redacted**]   [**Redacted**]

[**Redacted**]

    [**Redacted**]

 

3.2.1.2.2 Special / Contingency Modes

The Satellite shall, at a minimum, provide the modes defined in [**Redacted**] , with the following additional requirements:

[**Redacted**]

Table3-5 Special / Contingency Modes

 

Mode

 

Basic Satellite State

 

Satellite Pointing

[**Redacted**]

  [**Redacted**]   [**Redacted**]

[**Redacted**]

  [**Redacted**]   [**Redacted**]

[**Redacted**]

  [**Redacted**]  

 

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Table 3-6 Simultaneous Operations

 

Simultaneous Operations

   Normal Operating Modes   Special / Contingency Modes
   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]

Recording Image Data [**Redacted**]

       [**Redacted**]   [**Redacted**]        

Recording Ancillary Data

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]      

Transmitting recorded Image and Ancillary Data

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]      

Recording Satellite state of health data

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]  

Transmitting stored state-of-health data

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]  

Transmitting real-time state-of-health data

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]  

Preserving stored Image and Ancillary Data

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]  

Preserving stored state-of-health data

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]   [**Redacted**]

Receiving and executing real-time commands

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]

Receiving and storing stored commands

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]     [**Redacted**]  

Executing stored commands

   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]   [**Redacted**]  

[**Redacted**]

 

3.2.1.2.3 Intermediate and Transitional Modes

Additional intermediate and transitional modes may be defined for the Satellite and Spacecraft Bus.

[**Redacted**]

 

3.2.1.3 Pre-Launch Operations

 

3.2.1.3.1 Ground Storage

The Satellite shall be capable of being stored under proper conditions for up to [**Redacted**] without the need for refurbishment.

 

3.2.1.3.2 Launch Delay

 

a) The Satellite shall be capable of remaining loaded with propellant for a minimum of [**Redacted**] prior to launch, while maintaining safety and status monitoring.

 

b) The Satellite shall be capable of launch for up to [**Redacted**] following the integration of the Satellite to the Launch Vehicle without the need for demate, while maintaining safety and status monitoring.

 

c) The Satellite shall be designed to permit [**Redacted**] .

 

3.2.1.4 Early Orbit Operations

 

3.2.1.4.1 Autonomous Operations After Separation

Following the separation event, the Satellite shall autonomously:

 

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[**Redacted**]

 

3.2.1.4.2 First [**Redacted**]

Following the Autonomous Operations after Separation, the Satellite shall pose no constraints on operation such that:

[**Redacted**]

 

3.2.1.4.3 Commissioning

The Satellite shall pose no constraints on operation such that total Satellite on-orbit performance can be fully verified as specified in the Statement of Work.

 

3.2.1.5 Mission Operations

 

3.2.1.5.1 Viewing Angles

Viewing angles referred to in the [**Redacted**] and elsewhere in this specification shall be as defined below.

[**Redacted**]

3.2.1.5.1.1 Nominal Field of Regard

The Nominal Field of Regard shall be defined as a [**Redacted**]

3.2.1.5.1.2 Maximum Field of Regard

The Maximum Field of Regard shall be defined as a [**Redacted**]

3.2.1.5.1.3 [**Redacted**]

[**Redacted**]

3.2.1.5.1.4 [**Redacted**]

[**Redacted**]

[**Redacted**]

The Satellite shall allow operation of the [**Redacted**]

 

3.2.1.5.2 Imaging and Downlink Operations

The Satellite shall be capable of performing the imaging and downlink operations specified below assuming [**Redacted**]

3.2.1.5.2.1 [**Redacted**]

[**Redacted 1 Page**]

Wideband and Narrowband Downlinks

It shall be possible to perform both Wideband and Narrowband downlinks as follows:

[**Redacted**]

Instrument Mass Properties for

For purposes of verifying the Satellite’s ability to perform the DIS, [ **Redacted**]

[**Redacted**]

 

3.2.1.5.3 Stereo Imaging

 

a) The Satellite shall be capable of collecting the stereo imagery [**Redacted**]

 

b) The Satellite shall be capable of collecting stereo imagery [**Redacted**]

 

3.2.1.5.4 Off-Nadir Imaging

The Satellite shall be capable of supporting off-nadir image collections as follows:

 

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[**Redacted**]

 

3.2.1.5.5 Special Imaging

3.2.1.5.5.1 Minimum Capabilities

[**Redacted**]

3.2.1.5.5.2 [**Redacted**]

[**Redacted**]

 

3.2.1.5.6 [**Redacted**]

[**Redacted**]

 

3.2.1.6 Instrument Requirements

 

3.2.1.6.1 Integrated Bus/Instrument Performance Effects

The SSI shall perform appropriate integrated Satellite-level analyses and design work in order to ensure the Satellite meets the following performance requirements. LOS motion shall be calculated using an Instrument Finite Element Model (FEM) provided by the Instrument Contractor as defined under Applicable Documents, which shall be assumed to meet the following requirements:

[**Redacted**]

3.2.1.6.1.1 [**Redacted**]

[**Redacted**]

3.2.1.6.1.2 [**Redacted**]

[**Redacted**]

 

3.2.1.6.2 [**Redacted**]

[**Redated**]

3.2.1.6.2.1 [**Redated**]

[**Redacted**]

3.2.1.6.2.2 [**Redacted**]

[**Redacted**]

 

3.2.1.6.3 [**Redacted**]

[**Redacted**]

3.2.1.6.3.1 [**Redacted**]

[**Redacted**]

 

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3.2.1.6.3.2 [**Redacted**]

[**Redacted**]

3.2.1.6.3.3 [**Redacted**]

[**Redacted**]

3.2.1.6.3.4 [**Redacted**]

[**Redacted**]

3.2.1.6.3.4.1 [**Redacted**]

[**Redacted**]

3.2.1.6.3.4.2 [**Redacted**]

[**Redacted**]

3.2.1.6.3.4.3 [**Redacted**]

[**Redacted**]

3.2.1.6.3.5 [**Redacted**]

[**Redacted**]

3.2.1.6.3.5.1 [**Redacted**]

[**Redacted**]

3.2.1.6.3.5.2 [**Redacted**]

[**Redacted**]

[**Redacted**]

 

3.2.1.6.4 Instrument Cleanliness

[**Redacted**]

[**Redacted**]

[**Redacted**]

3.2.1.7 Bus Subsystem Requirements

 

In addition to supporting all subsystem-level requirements derived from the Satellite-level requirements specified in the above sections, Spacecraft Bus subsystems shall meet the specific requirements contained within this section.

 

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3.2.1.7.1 [ **Redacted** ]

3.2.1.7.1.1 [**Redacted**]

[**Redacted**]

3.2.1.7.1.2 [**Redacted**]

[**Redacted**]

3.2.1.7.1.3 [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.1 [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.2 [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.3 [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.4 [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.5 [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.6 [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.7 [**Redacted**]

[**Redacted**]

3.2.1.7.1.3.8 [**Redacted**]

[**Redacted**]

3.2.1.7.1.4 [**Redacted**]

3.2.1.7.1.4.1 [**Redacted**]

[**Redacted**]

 

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3.2.1.7.1.4.2 [**Redacted**]

[**Redacted**]

3.2.1.7.1.4.3 [**Redacted**]

[**Redacted**]

3.2.1.7.1.4.4 [**Redacted**]

[**Redacted**]

 

3.2.1.7.2 ADCS

3.2.1.7.2.1 [**Redacted**]

[**Redacted**]

3.2.1.7.2.2 [**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

3.2.1.7.2.2.5 [**Redacted**]

[**Redacted**]

3.2.1.7.2.3 [**Redacted**]

[**Redacted**]

3.2.1.7.2.4 [**Redacted**]

[**Redacted**]

[**Redacted**]

 

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3.2.1.7.2.5 [**Redacted**]

3.2.1.7.2.6 [**Redacted**]

[**Redacted**]

3.2.1.7.2.7 [**Redacted**]

[**Redacted**]

3.2.1.7.2.8 [**Redacted**]

[**Redacted**]

3.2.1.7.2.9 [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.1 [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.2 [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.3 [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.4 [**Redacted**]

[**Redacted**]

3.2.1.7.2.9.5 [**Redacted**]

[**Redacted**]

3.2.1.7.2.10 [**Redacted**]

[**Redacted**]

3.2.1.7.2.11 Solar Arrays

In all modes of operation except Launch Mode, the ADCS shall be capable of pointing the Solar Array as follows:

[**Redacted**]

3.2.1.7.2.12 Wideband Antenna

While in Cruise Mode, Earth or Fixed Frame Imaging Mode, or maneuvering to/from Images, the ADCS shall be capable of pointing the Wideband Antenna as follows:

[**Redacted**]

 

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3.2.1.7.3 Propulsion

3.2.1.7.3.1 Minimum Delta-V Capability

The Propulsion subsystem shall provide at least [**Redacted**]

3.2.1.7.3.2 Propellant Budget

The SSI shall develop and maintain a [**Redacted**]

3.2.1.7.3.3 Inefficiencies of Operation

The propellant budget shall, at a minimum, account for the following inefficiencies of operation:

[**Redacted**]

3.2.1.7.3.4 Thruster Orientation

[**Redacted**]

3.2.1.7.3.5 [**Redacted**]

[**Redacted**]

 

3.2.1.7.4 Flight Software

3.2.1.7.4.1 [**Redacted**]

The Flight Software shall provide the capability to [**Redacted**].

The design of the Satellite flight software shall be [**Redacted**] .

3.2.1.7.4.2.1 Module Size

The patching or replacing of any single Satellite flight software module shall not require more than [**Redacted**] or the [**Redacted**] shall be uploadable in no more than [**Redacted**] split across multiple contacts [**Redacted**].

Parameterization

The design of the Satellite flight software shall incorporate parameterization to support operational flexibility and command versatility.

[**Redacted**]

3.2.1.7.4.3.1 Parameter Range and Resolution

Parameters shall have enough range and resolution to permit operation of the Satellite to the requirements of this specification without having to patch the Satellite Flight software.

3.2.1.7.4.3.2 [**Redacted**]

[**Redacted**]

 

[**Redacted**]

3.2.1.7.4.4.1 [**Redacted**]

[**Redacted**]

 

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3.2.1.7.4.4.2 [**Redacted**]

[**Redacted**]

3.2.1.7.4.5 [**Redacted**]

[**Redacted**]

3.2.1.7.4.6 [**Redacted**]

[**Redacted**]

3.2.1.7.4.7 [**Redacted**]

[**Redacted**]

[**Redacted**]

3.2.1.7.4.8 [**Redacted**]

[**Redacted**]

3.2.1.7.4.9 [**Redacted**]

[**Redacted**]

3.2.1.7.4.10 [**Redacted**]

[**Redacted**]

3.2.1.7.4.11 [**Redacted**]

[**Redacted**]

 

3.2.1.7.5 C&DH

3.2.1.7.5.1 Commands

3.2.1.7.5.1.1 Command Formats

Commands shall be formatted as specified in the [**Redacted**] .

3.2.1.7.5.1.2 Command Length

Commands shall be [**Redacted**] to assure compatibility with [**Redacted**] with [**Redacted**] and

[**Redacted**].

3.2.1.7.5.1.3 [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.4 [**Redacted**]

[**Redacted**]

 

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3.2.1.7.5.1.5 [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.6 [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.7 [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.8 [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.9 [**Redacted**]

[**Redacted**]

3.2.1.7.5.1.10 Unique Satellite Identification

The Satellite identification used for command verification and acceptance shall be unique for each redundancy string and shall be different than IDs used on previous DigitalGlobe satellites.

[**Redacted**]

3.2.1.7.5.2 State-of-Health Telemetry

3.2.1.7.5.2.2 Telemetry Content

The C&DH subsystem shall collect and format housekeeping telemetry for the Spacecraft Bus [**Redacted**] sufficient to provide the following capabilities on the ground:

[**Redacted**]

Telemetry Format

The C&DH subsystem shall format and transmit the [**Redacted**] as follows:

[**Redacted**]

[**Redacted**]

3.2.1.7.5.2.4 [**Redacted**]

[**Redacted**]

3.2.1.7.5.2.5 [**Redacted**]

[**Redacted**]

 

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3.2.1.7.5.2.6 Unique Satellite Identification

All telemetry data shall periodically include a Satellite identification that is different than IDs used on previous DigitalGlobe satellites.

[**Redacted**]

3.2.1.7.5.2.7 Storage Capacity

The C&DH subsystem shall be capable of storing at least 36 hours of telemetry at an average rate of

[**Redacted**] .

[**Redacted**]

3.2.1.7.5.2.8 [**Redacted**]

[**Redacted**]

3.2.1.7.5.2.9 [**Redacted**]

[**Redacted**]

3.2.1.7.5.3 [**Redacted**]

[**Redacted**]

3.2.1.7.5.4 Ancillary Data

During normal operations, the C&DH subsystem shall collect Ancillary Data from Bus and Instrument equipment and forward it [**Redacted**]

3.2.1.7.5.4.1 Standard Content

The standard content of the two Ancillary Data streams shall be as defined in [**Redacted**] .

[**Redacted**]

 

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Table 3-1 Standard Ancillary Data Content

 

Data Type

  

Description

   Frequency    Minimum Rate

Continuous Ancillary Data Stream

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]

[**Redacted**]

Image Ancillary Data Stream

[**Redacted**]

   [**Redacted**]    [**Redacted**]    [**Redacted**]

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

   [**Redacted**]    [**Redacted**]   

[**Redacted**]

3.2.1.7.5.4.2 Format

The C&DH subsystem shall format the [**Redacted**]

3.2.1.7.5.4.3 Redefinable Content

It shall be possible to independently re-define the content of [**Redacted**] , subject to data bandwidth constraints.

[**Redacted**]

3.2.1.7.5.4.4 [**Redacted**]

[**Redacted**]

Data Transfer

The C&DH subsystem shall transfer the Ancillary Data to the MDR as follows:

[**Redacted**]

3.2.1.7.5.4.6 [**Redacted**]

[**Redacted**]

3.2.1.7.5.4.7 [**Redacted**]

[**Redacted**]

3.2.1.7.5.5 Command & Telemetry Protocol

The satellite shall meet the requirements for the satellite command and telemetry protocol as specified in the

[**Redacted**]

 

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3.2.1.7.6 Narrowband Communications

3.2.1.7.6.1 Command Uplink

3.2.1.7.6.1.1 Uplink Bit Rate

The Command Uplink shall operate at one of two selectable rates, including all headers and other formatting, as follows:

[**Redacted**]

3.2.1.7.6.1.2 Bit Error Rate

The Command Uplink shall provide a bit error rate not to exceed [**Redacted**] .

3.2.1.7.6.1.3 Availability

The Command Uplink shall provide an availability of at least [**Redacted**] .

3.2.1.7.6.1.4 Elevation Angle

The Command Uplink shall operate at elevation angles of [**Redacted**] .

3.2.1.7.6.1.5 Link Margin

The Command Uplink shall meet all performance and functional requirements specified herein at EOL with a link margin of at least [**Redacted**] .

3.2.1.7.6.1.6 [**Redacted**]

[**Redacted**]

Modulation

The Command Uplink shall be modulated using [**Redacted**] .

3.2.1.7.6.1.8 Radio Frequency

The nominal Command Uplink carrier frequency shall be [**Redacted**] .

3.2.1.7.6.1.9 Antenna Coverage

Command Uplink antenna coverage shall be provided as follows:

[**Redacted**]

c) Provides realistic allowances for blockages by the Instrument.

3.2.1.7.6.1.10 Antenna Polarization

The Command Uplink antenna shall use [**Redacted**] .

3.2.1.7.6.1.11 Idle Patterns

[**Redacted**]

Telemetry Downlink

Telemetry Bit Rate

The Telemetry Downlink shall be at the following selectable rates, including all header and other formatting required to structure the commands:

[**Redacted**]

3.2.1.7.6.2.2 Telemetry Bit Rate

The Telemetry Downlink shall be at a rate of [**Redacted**].

3.2.1.7.6.2.3 Bit Error Rate

The Telemetry Downlink shall provide a bit error rate not to exceed [**Redacted**] .

3.2.1.7.6.2.4 Availability

The Telemetry Downlink shall provide an availability of at least [**Redacted**] .

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

3.2.1.7.6.2.5 Elevation Angle

The Telemetry Downlink shall operate at elevation angles of [**Redacted**] .

3.2.1.7.6.2.6 Link Margin

The Telemetry Downlink shall meet all performance and functional requirements specified herein at EOL with a link margin of at least [**Redacted**] .

3.2.1.7.6.2.7 [**Redacted**]

[**Redacted**]

3.2.1.7.6.2.8 [**Redacted**]

[**Redacted**]

3.2.1.7.6.2.9 Modulation

a) The Telemetry Downlink shall use [**Redacted**] modulation as specified in the [**Redacted**] .

 

b) Any processing of the original data stream before transmission shall result in a [**Redacted**] .

3.2.1.7.6.2.10 Radio Frequency

The nominal Telemetry Downlink carrier frequency shall be [**Redacted**] .

3.2.1.7.6.2.11 Antenna Coverage: Special / Contingency Modes

 

a) Telemetry Downlink antenna coverage shall support all RF performance requirements specified herein (e.g. all downlink rates, both real-time and stored telemetry, BER, availability, elevation angle, etc.) with a [**Redacted**] when transmitting within [**Redacted**] .

 

b) A minimum elevation angle up to [**Redacted**] shall be permitted.

 

c) It shall be permissible to require ground commands in order to [**Redacted**] for operation in this mode, for example to switch from [**Redacted**] to [**Redacted**]

3.2.1.7.6.2.12 Antenna Coverage: Normal Operating Modes

Telemetry Downlink antenna coverage shall support all RF performance requirements specified herein (e.g. all downlink rates, BER, link margin, etc.) as follows:

[**Redacted**]

3.2.1.7.6.2.13 Antenna Polarization

The Telemetry Downlink antenna shall use [**Redacted** ]

3.2.1.7.6.2.14 Adjustable RF Output Power

The Telemetry Downlink shall provide the capability to adjust RF output power levels by ground command (real-time or stored), in increments sufficient to meet the link margin and interference limits specified in Sections 3.2.1.7.6.2.6 Link Margin and 3.1.2.1 Non-interference with Outside Systems, at any altitude over the range specified in Section 3.2.1.1.2.1 General Orbit Compatibility.

[**Redacted**]

 

3.2.1.7.7 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1 [**Redacted**]

[**Redacted**]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

3.2.1.7.7.1.1 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.2 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.3 [**Redacted**]

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3.2.1.7.7.1.4 [**Redacted**]

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3.2.1.7.7.1.5 [**Redacted**]

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3.2.1.7.7.1.6 [**Redacted**]

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3.2.1.7.7.1.7 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.8 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.9 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.10 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.11 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.12 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.13 [**Redacted**]

[**Redacted**]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

3.2.1.7.7.1.14 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.15 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.16 [**Redacted**]

[**Redacted**]

3.2.1.7.7.1.17 [**Redacted**]

[**Redacted**]

3.2.1.7.7.2 [**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

3.2.1.7.7.2.8 [**Redacted**]

3.2.1.7.7.2.9 [**Redacted**]

[**Redacted**]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

3.2.1.7.7.2.10 [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.11 [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.12 [**Redacted**]

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3.2.1.7.7.2.13 [**Redacted**]

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3.2.1.7.7.2.14 [**Redacted**]

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3.2.1.7.7.2.15 [**Redacted**]

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3.2.1.7.7.2.16 [**Redacted**]

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3.2.1.7.7.2.17 [**Redacted**]

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3.2.1.7.7.2.18 [**Redacted**]

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3.2.1.7.7.2.19 [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.20 [**Redacted**]

[**Redacted**]

3.2.1.7.7.2.21 [**Redacted**]

[**Redacted**]

 

3.2.1.7.8 EPDS

3.2.1.7.8.1 Functional Requirements

The EPDS shall perform the following functions under the Conditions and Operational Scenarios specified below:

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

a) Provide sufficient power to all Spacecraft Bus and Instrument equipment to

[**Redacted**]

3.2.1.7.8.2 Realistic Worst Case Conditions

EPDS performance shall be evaluated under realistic worst-case conditions [**Redacted**], including, but not limited to:

[**Redacted**]

3.2.1.7.8.3 Operational Scenarios

EPDS performance shall be evaluated using the following operational scenarios for the range of orbits specified in Section 3.2.1.1.2.1 General Orbit Compatibility. For requirements verification, it is acceptable to perform in-depth analysis [**Redacted**]

3.2.1.7.8.4 Instrument Power

The EPDS shall provide power to the Instrument as specified in Section 3.1.3.1.3 Power Interfaces.

3.2.1.7.8.5 [**Redacted**]

[**Redacted**]

3.2.1.7.8.6 [**Redacted**]

[**Redacted**]

3.2.1.7.8.7 [**Redacted**]

[**Redacted**]

3.2.1.7.8.8 [**Redacted**]

[**Redacted**]

3.2.1.7.9 Structures and Mechanisms

3.2.1.7.9.1 Functional Requirements

The Structure shall perform the following functions:

 

a) Support all Bus and [**Redacted**] equipment through all mission phases, including pre-launch, launch, initialization, normal operations, and EOL disposal.

b) [**Redacted**]

3.2.1.7.9.2 Factors and Margins of Safety

[**Redacted**]

3.2.1.7.9.3 Mechanisms

3.2.1.7.9.3.1 [**Redacted**]

[**Redacted**]

3.2.1.7.9.3.2 Accessibility

Deployment devices shall be accessible with minimum disturbance to the relative position of the mechanisms or their thermal control hardware.

3.2.1.7.9.3.3 Thermal Constraints

There shall be no thermal constraints against the operation of any mechanism at any time during the Satellite Mission Life such that:

[**Redacted**]

3.2.1.7.9.3.4 [**Redacted**]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

[**Redacted**]

3.2.1.7.9.3.5 [**Redacted**]

[**Redacted**]

3.2.1.7.10 Thermal Control

3.2.1.7.10.1 Functional Requirements

The Thermal Control subsystem shall autonomously perform the following functions under the Conditions and Operational Scenarios specified below:

[**Redacted**]

3.2.1.7.10.2 Realistic Worst Case Conditions

Thermal Control Subsystem performance shall be evaluated under realistic worst-case conditions (i.e. precluding combinations of conditions that can not physically occur), including, but not limited to:

[**Redacted**]

3.2.1.7.10.3 Operational Scenarios

The Thermal Control Subsystem performance shall be evaluated using the following operational scenarios for the range of orbits specified in Section 3.2.1.1.2.1 General Orbit Compatibility. For requirements verification, it is acceptable to perform in-depth analysis

[**Redacted**]

3.2.1.7.10.4 [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.1 [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.2 [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.3 [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.4 [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.5 [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.6 [**Redacted**]

[**Redacted**]

3.2.1.7.10.4.7 [**Redacted**]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

[**Redacted**]

3.2.1.7.10.4.8 [**Redacted**]

3.2.1.7.10.4.9 [**Redacted**]

[**Redacted**]

3.2.1.7.10.5 [**Redacted**]

[**Redacted**]

3.2.1.7.11 Direct Tasking

The Satellite shall provide Direct Tasking capabilities as specified below, with the following definitions of key terms:

[**Redacted**]

3.2.1.7.11.1 [**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

[**Redacted**]

3.2.1.7.11.1.5 [**Redacted**]

[**Redacted**]

3.2.1.7.11.1.6 [**Redacted**]

[**Redacted**]

3.2.1.7.11.1.7 [**Redacted**]

[**Redacted**]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

3.2.1.7.11.2 [**Redacted**]

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3.2.1.7.11.2.1 [**Redacted**]

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3.2.1.7.11.2.2 [**Redacted**]

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3.2.1.7.11.2.3 [**Redacted**]

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3.2.1.7.11.2.4 [**Redacted**]

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3.2.1.7.11.2.5 [**Redacted**]

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3.2.1.7.11.3.1 [**Redacted**]

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3.2.1.7.11.3.2 [**Redacted**]

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3.2.1.7.11.3.3 [**Redacted**]

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3.2.1.7.11.3.4 [**Redacted**]

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3.2.1.7.11.3.5 [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.6 [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.7 [**Redacted**]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

[**Redacted**]

3.2.1.7.11.3.8 [**Redacted**]

[**Redacted**]

3.2.1.7.11.3.9 [**Redacted**]

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3.2.1.7.11.3.10 [**Redacted**]

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3.2.1.7.11.4 [**Redacted**]

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3.2.1.7.11.4.1 [**Redacted**]

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3.2.1.7.11.4.2 [**Redacted**]

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3.2.1.7.11.4.3 [**Redacted**]

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3.2.1.7.11.4.4 [**Redacted**]

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3.2.1.7.11.4.5 [**Redacted**]

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3.2.1.7.11.4.6 [**Redacted**]

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3.2.1.7.11.4.7 [**Redacted**]

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3.2.1.7.11.4.8 [**Redacted**]

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3.2.1.7.11.4.9 [**Redacted**]

[**Redacted**]

3.2.1.7.11.5 [**Redacted**]

3.2.1.7.11.5.1 [**Redacted**]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

[**Redacted**]

3.2.1.7.11.5.2 [**Redacted**]

[**Redacted**]

3.2.1.7.11.5.3 [**Redacted**]

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3.2.1.7.11.5.4 [**Redacted**]

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3.2.1.7.11.5.5 [**Redacted**]

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3.2.1.7.11.5.6 [**Redacted**]

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3.2.1.7.11.5.7 [**Redacted**]

[**Redacted**]

3.2.2 Physical Characteristics

3.2.2.1 Size Constraints

The size of the integrated Satellite shall be compatible with the specified Launch Vehicles and Shipping Constraints.

 

3.2.2.2 Mass Constraints

The total Satellite mass (including all parts of the Launch Vehicle adapter / separation mechanism that remain with the Satellite after separation) shall not exceed the limits established by the [**Redacted**] and the

[**Redacted**].

[**Redacted**]

 

3.2.2.3 Shipping Constraints

The Satellite and associated Ground Support Equipment (GSE), including the shipping container, shall be designed to allow transportation to the Launch Site via the [**Redacted**] or by [**Redacted**] and [**Redacted**] .

Reliability

  End of Life Ps

[**Redacted**]

 

3.2.3.2 [**Redacted**]

[**Redacted]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

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3.2.3.3 [**Redacted**]

[**Redacted**]

3.2.3.4 Cycle-Limited Items

Items whose life is limited by the total number of operating cycles shall meet all on-orbit performance requirements after operating for [**Redacted**] the predicted number of cycles, including all cycles incurred during both the Mission Life and during ground testing. Cycle-limited items shall include at a minimum:

[**Redacted**]

3.2.3.4.1 [**Redacted**]

[**Redacted**]

3.2.3.4.2 [**Redacted**]

[**Redacted**]

3.2.4 Availability and Maintainability

3.2.4.1 Fault Recovery Timeline

The Satellite equipment provided by the SSI shall be designed to allow recovery from any fault conditions and single event upsets or latch-ups within [**Redacted**] of ground operator intervention, with the exception of [**Redacted**] , which shall take no longer than [**Redacted**]

3.2.4.2 Environmental Conditions

The Satellite shall meet all functional and performance requirements after exposure to the following environments.

3.2.4.2.1 Launch Induced Environments

[**Redacted**]

3.2.4.2.2 On-Orbit Environments

On-orbit environments shall be consistent with operation in the Mission Orbit for the Mission Life and shall include, at a minimum:

[**Redacted**]

3.2.4.2.3 Pre-Launch Environments

Except for any specific testing aimed at verifying the design margins, the Satellite shall not be subjected to any environments that exceed the launch and on-orbit environments. This includes integration and test activities, transportation, launch site processing, and the period the Satellite is within the Launch Vehicle Fairing prior to launch.

3.3 Satellite Design and Construction

3.3.1 General

The Satellite Design and Construction shall be performed per standard SSI practices in accordance with the Environmental Design and Test Specification and the DigitalGlobe Space Segment Specification Addendum, including at a minimum the following items:

[**Redacted**]

 

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WorldView-3 Satellite Specification

Doc’t # 10329655

Rev 8.0: 2 Nov 2011

 
 

 

3.3.2 SEUs

[**Redacted**]

3.3.3 Immunity to Latch-Up

[**Redacted**]

3.3.4 Cleanliness and Contamination Control

[**Redacted**]

3.3.4.1 [**Redacted**]

[**Redacted**]

3.3.4.2 [**Redacted**]

[**Redacted**]

3.3.4.3 [**Redacted**]

[**Redacted**]

3.3.4.4 [**Redacted**]

[**Redacted**]

3.3.5 Safety

The Satellite shall be designed to allow for safe handling, operation, transportation, fuel loading and pressurization through all mission phases. It shall comply with the specific requirements of [**Redacted**] , including at a minimum:

[**Redacted**]

 

3.3.6 [**Redacted**]

[**Redacted**]

 

4. VERIFICATION

Requirements verification shall be performed per standard SSI practices, in accordance with the DigitalGlobe Space Segment Specification Addendum and the Statement of Work.

 

5. QUALITY ASSURANCE

Quality Assurance shall be performed per standard SSI practices, in accordance with the DigitalGlobe Space Segment Specification Addendum and the Statement of Work.

 

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35


Attachment 3

WorldView3 Payment Milestone Schedule, Rev 4.0

Dated 24 October 2011


WorldView 3 Payment Milestone Schedule

Exhibit 3 to WV3 Satellite Agreement # 60150

 

Item
#

  

Invoice Date

   Line
Item
  

Description

   Completed   

Milestone Value

  

Cumulative
Milestones

  

Termination
Liability

1

   [**Redacted**]       Milestone 1 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]            

2

   [**Redacted**]       Milestone 2 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      

3

   [**Redacted**]       Milestone 3 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      

4

   [**Redacted**]       Milestone 4 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      

5

   [**Redacted**]       Milestone 5 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      

6

   [**Redacted**]       Milestone 6 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      

7

   [**Redacted**]       Milestone 7 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      

8

   [**Redacted**]       Milestone 8 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      a    [**Redacted**]       [**Redacted**]      
      b    [**Redacted**]       [**Redacted**]      
      c    [**Redacted**]       [**Redacted**]      
      d    [**Redacted**]       [**Redacted**]      

9

   [**Redacted**]       Milestone 9 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      9a    [**Redacted**]       [**Redacted**]      
      9b    [**Redacted**]       [**Redacted**]      
      9c    [**Redacted**]       [**Redacted**]      
      9d    [**Redacted**]       [**Redacted**]      

10

   [**Redacted**]       Milestone 10 Total Value       [**Redacted**]    [**Redacted**]    [**Redacted**]
      10a    [**Redacted**]       [**Redacted**]      
      10b    [**Redacted**]       [**Redacted**]      
      10c    [**Redacted**]       [**Redacted**]      
      10d    [**Redacted**]       [**Redacted**]      


 

11

   [**Redacted**]       Milestone 11 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      11a    [**Redacted**]    [**Redacted**]      
      11b    [**Redacted**]    [**Redacted**]      
      11c    [**Redacted**]    [**Redacted**]      
      11d    [**Redacted**]    [**Redacted**]      
      11e    [**Redacted**]    [**Redacted**]      

12

   [**Redacted**]       Milestone 12 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      12a    [**Redacted**]    [**Redacted**]      
      12b    [**Redacted**]    [**Redacted**]      
      12c    [**Redacted**]    [**Redacted**]      
      12d    [**Redacted**]    [**Redacted**]      
      12e    [**Redacted**]    [**Redacted**]      

13

   [**Redacted**]       Milestone 13 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      13a    [**Redacted**]    [**Redacted**]      
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14

   [**Redacted**]       Milestone 14 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
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15

   [**Redacted**]       Milestone 15 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
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      15e    [**Redacted**]    [**Redacted**]      
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16

   [**Redacted**]       Milestone 16 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      16a    [**Redacted**]    [**Redacted**]      
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      16d    [**Redacted**]    [**Redacted**]      
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17

   [**Redacted**]       Milestone 17 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      17a    [**Redacted**]    [**Redacted**]      
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      17d    [**Redacted**]    [**Redacted**]      

18

   [**Redacted**]       Milestone 18 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      18a    [**Redacted**]    [**Redacted**]      
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      18c    [**Redacted**]    [**Redacted**]      
      18d    [**Redacted**]    [**Redacted**]      

19

   [**Redacted**]       Milestone 19 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      19a    [**Redacted**]    [**Redacted**]      
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      19e    [**Redacted**]    [**Redacted**]      


20    [**Redacted**]       Milestone 20 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      20a    [**Redacted**]    [**Redacted**]      
      20b    [**Redacted**]    [**Redacted**]      
      20c    [**Redacted**]    [**Redacted**]      
      20d    [**Redacted**]    [**Redacted**]      
21    [**Redacted**]       Milestone 21 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      21a    [**Redacted**]    [**Redacted**]      
      21b    [**Redacted**]    [**Redacted**]      
      21c    [**Redacted**]    [**Redacted**]      
      21d    [**Redacted**]    [**Redacted**]      
      21e    [**Redacted**]    [**Redacted**]      
22    [**Redacted**]       Milestone 22 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      22a    [**Redacted**]    [**Redacted**]      
      22b    [**Redacted**]    [**Redacted**]      
      22c    [**Redacted**]    [**Redacted**]      
      22d    [**Redacted**]    [**Redacted**]      
      22e    [**Redacted**]    [**Redacted**]      
23    [**Redacted**]       Milestone 23 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      23a    [**Redacted**]    [**Redacted**]      
      23b    [**Redacted**]    [**Redacted**]      
      23c    [**Redacted**]    [**Redacted**]      
      23d    [**Redacted**]    [**Redacted**]      
      23e    [**Redacted**]    [**Redacted**]      
      23f    [**Redacted**]    [**Redacted**]      
24    [**Redacted**]       Milestone 24 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      24a    [**Redacted**]    [**Redacted**]      
      24b    [**Redacted**]    [**Redacted**]      
      24c    [**Redacted**]    [**Redacted**]      
      24d    [**Redacted**]    [**Redacted**]      
      24e    [**Redacted**]    [**Redacted**]      
25    [**Redacted**]       Milestone 25 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      25a    [**Redacted**]    [**Redacted**]      
      25b    [**Redacted**]    [**Redacted**]      
      25c    [**Redacted**]    [**Redacted**]      
      25d    [**Redacted**]    [**Redacted**]      
      25e    [**Redacted**]    [**Redacted**]      
26    [**Redacted**]       Milestone 26 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      26a    [**Redacted**]    [**Redacted**]      
      26b    [**Redacted**]    [**Redacted**]      
      26c    [**Redacted**]    [**Redacted**]      
      26d    [**Redacted**]    [**Redacted**]      
      26e    [**Redacted**]    [**Redacted**]      
27    [**Redacted**]       Milestone 27 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      27a    [**Redacted**]    [**Redacted**]      
      27b    [**Redacted**]    [**Redacted**]      
      27c    [**Redacted**]    [**Redacted**]      
      27d    [**Redacted**]    [**Redacted**]      


28    [**Redacted**]       Milestone 28 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      28a    [**Redacted**]    [**Redacted**]      
      28b    [**Redacted**]    [**Redacted**]      
      28c    [**Redacted**]    [**Redacted**]      
      28d    [**Redacted**]    [**Redacted**]      
      28e    [**Redacted**]    [**Redacted**]      
      28f    [**Redacted**]    [**Redacted**]      
29    [**Redacted**]       Milestone 29 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      29a    [**Redacted**]    [**Redacted**]      
      29b    [**Redacted**]    [**Redacted**]      
      29c    [**Redacted**]    [**Redacted**]      
      29d    [**Redacted**]    [**Redacted**]      
      29e    [**Redacted**]    [**Redacted**]      
30    [**Redacted**]       Milestone 30 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      30a    [**Redacted**]    [**Redacted**]      
      30b    [**Redacted**]    [**Redacted**]      
      30c    [**Redacted**]    [**Redacted**]      
      30d    [**Redacted**]    [**Redacted**]      
31    [**Redacted**]       Milestone 31 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      31a    [**Redacted**]    [**Redacted**]      
      31b    [**Redacted**]    [**Redacted**]      
      31c    [**Redacted**]    [**Redacted**]      
      31d    [**Redacted**]    [**Redacted**]      
32    [**Redacted**]       Milestone 32 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      32a    [**Redacted**]    [**Redacted**]      
      32b    [**Redacted**]    [**Redacted**]      
      32c    [**Redacted**]    [**Redacted**]      
      32d    [**Redacted**]    [**Redacted**]      
33    [**Redacted**]       Milestone 33 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      33a    [**Redacted**]    [**Redacted**]      
      33b    [**Redacted**]    [**Redacted**]      
      33c    [**Redacted**]    [**Redacted**]      
      33d    [**Redacted**]    [**Redacted**]      
      33e    [**Redacted**]    [**Redacted**]      
34    [**Redacted**]       Milestone 34 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      34a    [**Redacted**]    [**Redacted**]      
      34b    [**Redacted**]    [**Redacted**]      
      34c    [**Redacted**]    [**Redacted**]      
      34d    [**Redacted**]    [**Redacted**]      
      34e    [**Redacted**]    [**Redacted**]      
      34f    [**Redacted**]    [**Redacted**]      
35    [**Redacted**]       Milestone 35 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      35a    [**Redacted**]    [**Redacted**]      
      35b    [**Redacted**]    [**Redacted**]      
      35c    [**Redacted**]    [**Redacted**]      
      35d    [**Redacted**]    [**Redacted**]      
      35e    [**Redacted**]    [**Redacted**]      
36    [**Redacted**]       Milestone 36 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      36a    [**Redacted**]    [**Redacted**]      
      36b    [**Redacted**]    [**Redacted**]      
      36c    [**Redacted**]    [**Redacted**]      
      36d    [**Redacted**]    [**Redacted**]      
      36e    [**Redacted**]    [**Redacted**]      


 

37    [**Redacted**]       Milestone 37 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      37a    [**Redacted**]    [**Redacted**]      
      37b    [**Redacted**]    [**Redacted**]      
      37c    [**Redacted**]    [**Redacted**]      
      37d    [**Redacted**]    [**Redacted**]      
      37e    [**Redacted**]    [**Redacted**]      
38    [**Redacted**]       Milestone 38 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      38a    [**Redacted**]    [**Redacted**]      
      38b    [**Redacted**]    [**Redacted**]      
      38c    [**Redacted**]    [**Redacted**]      
      38d    [**Redacted**]    [**Redacted**]      
      38e    [**Redacted**]    [**Redacted**]      
      38f    [**Redacted**]    [**Redacted**]      
39    [**Redacted**]       Milestone 39 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      39a    [**Redacted**]    [**Redacted**]      
      39b    [**Redacted**]    [**Redacted**]      
      39c    [**Redacted**]    [**Redacted**]      
      39d    [**Redacted**]    [**Redacted**]      
40    [**Redacted**]       Milestone 40 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      40a    [**Redacted**]    [**Redacted**]      
      40b    [**Redacted**]    [**Redacted**]      
      40c    [**Redacted**]    [**Redacted**]      
      40d    [**Redacted**]    [**Redacted**]      
      40e    [**Redacted**]    [**Redacted**]      
41    [**Redacted**]       Milestone 41 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      41a    [**Redacted**]    [**Redacted**]      
      41b    [**Redacted**]    [**Redacted**]      
      41c    [**Redacted**]    [**Redacted**]      
      41d    [**Redacted**]    [**Redacted**]      
42    [**Redacted**]       Milestone 42 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      42a    [**Redacted**]    [**Redacted**]      
      42b    [**Redacted**]    [**Redacted**]      
      42c    [**Redacted**]    [**Redacted**]      
      42d    [**Redacted**]    [**Redacted**]      
43    [**Redacted**]       Milestone 43 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      43a    [**Redacted**]    [**Redacted**]      
      43b    [**Redacted**]    [**Redacted**]      
      43c    [**Redacted**]    [**Redacted**]      
      43d    [**Redacted**]    [**Redacted**]      
      43e    [**Redacted**]    [**Redacted**]      
44    [**Redacted**]       Milestone 44 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      44a    [**Redacted**]    [**Redacted**]      
      44b    [**Redacted**]    [**Redacted**]      
      44c    [**Redacted**]    [**Redacted**]      
      44d    [**Redacted**]    [**Redacted**]      
45    [**Redacted**]       Milestone 45 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      45a    [**Redacted**]    [**Redacted**]      
      45b    [**Redacted**]    [**Redacted**]      
46    [**Redacted**]       Milestone 46 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      46a    [**Redacted**]    [**Redacted**]      


 

      46b    [**Redacted**]    [**Redacted**]      
      46c    [**Redacted**]    [**Redacted**]      
      46d    [**Redacted**]    [**Redacted**]      
47    [**Redacted**]       Milestone 47 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      47a    [**Redacted**]    [**Redacted**]      
48    [**Redacted**]       Milestone 48 Total Value    [**Redacted**]    [**Redacted**]    [**Redacted**]
      48a    [**Redacted**]    [**Redacted**]      
      48b    [**Redacted**]    [**Redacted**]      
      48c    [**Redacted**]    [**Redacted**]      
         TOTALS    $217,277,399    $217,277,399    $217,277,399


Attachment 4

WorldView3 Satellite Simulator Specification, Rev 3.0

Dated 24 October 2011

ITAR Controlled Document

[**Redacted**]


Attachment 5

[**Redacted**]


Attachment 6

[**Redacted**]

Exhibit 10.6.1

FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #1

[**REDACTED**]

To

Firm Fixed Price Agreement No. 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitalGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

This modification is associated with delivery [**REDACTED**] as outlined in 7.6 of the SOW for the WorldView 3 Instrument (SOW), Revision #3.0, dated November 4, 2010.

Both DG and SSD hereby agree to amend the referenced Agreement as follows:

 

  1) Replace SOW Revision #2.0 with SOW Revision #3.0 (Document #10329744) dated November 4, 2010.

 

  2) Replace Exhibit #2 entitled Milestone Payment and Termination Liability Schedule and replace it will the revised payment schedule referenced as Exhibit #2 (of the same name) Identified as Attachment 1 of this modification.

The amount of this firm fixed price modification is $4,860,933.

The total contract price is herein changed from $126,500,000 to $131,360,933.

All other terms and conditions of the Agreement not noted as changed remain in lull force and effect.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a legally binding agreement.

 

ITT Space Systems, LLC    DigitalGlobe, Inc.

/s/ [**REDACTED**]

  

/s/ Neal T. Anderson

Signature    Signature

[**REDACTED**]

  

Neal T. Anderson

Name    Name

[**REDACTED**]

  

Vice President – Technology Development


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

        Title    
Date:  

30 Nov 2010

  Date:  

30 Nov 2010


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Exhibit #2_Revision #1 – Milestone Payment and Termination Liability Schedule

 

MONTH

  

Finish
Dates

 

P S

UID

 

Name

 

TOTAL FOR
    MONTH

 

Current
AMOUNT

 

DELTA

 

AMOUNT [**]

 

NEW TOTAL
FOR MONTH

**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
**    **   **   **   **   **   **   **   **
        

 

 

 

 

 

 

 

 

 

Grand
Total
         $126,500.00   126,500,000   4,860,933   131,360,933   $131,360,933
        

 

 

 

 

 

 

 

 

 


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #2

[**REDACTED**]

To

Firm Fixed Price Agreement No. 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitalGlobe, Inc. (DO), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260; Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

The parties hereby agree to amend the Agreement as follows:

1) Add the following deliverables, as applicable, to the SOW and Instrument Specification:

 

  a. [**REDACTED**]

 

  b. [**REDACTED**]

 

  c. [**REDACTED**]

 

  d. [**REDACTED**]

2) Add the attached [**REDACTED**] requirements as Appendix A of the Instrument Specification.

3) Adjusted Payment Milestone Schedule (attached)

 

Original Contract Value

     FFP       $  131,360,933   

This Modification [**REDACTED**]

     FFP       $ 3,541,000   
     

 

 

 

Adjusted TOTAL Contract Value

      $ 134,901,933   
     

 

 

 

The total contract price Is herein changed from $131,360,933 to $134,901,933.

All changes contained herein will he incorporated in the respective SOW and/or Instrument Specification and the changes must be mutually agreed to and as specified in WV3 Instrument. Purchase Agreement #60151 (Document #10329740).

All other terms and conditions of the Agreement not noted as changed herein remain in full force and effect.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a binding agreement.

 

ITT Space Systems, LLC    DigitalGlobe, Inc.


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

/s/ [**REDACTED**]

 

/s/ Jeff S. Culwell

Signature   Signature
[**REDACTED**]  

Jeff S. Culwell

  Name
[**REDACTED**]  

Vice President

    Title
Date:  

12/16/2010

  Date:  

12/15/2010


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

[**REDACTED**]

DIGITALGLOBE, INC. PROPRIETARY DATA

 

1 of 2


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

[**REDACTED**]

DIGITALGLOBE, INC, PROPRIETARY DATA

 

2 of 2


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

 

MONTH

  

Finish
Dates

 

P S

UID

 

Name

 

TOTAL FOR
MONTH

   

Current
AMOUNT

 

DELTA

   

AMOUNT w/
Spares [**]

 

NEW TOTAL
FOR NOV. 2010

   

DELTA

   

AMOUNT [**]

   

NEW TOTAL FOR
      DEC. 2010

 

**

   **   **   **     **      **     **      **     **        **        **        **   

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   **   **   **     **      **     **      **     **        **        **        **   

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   **   **   **     **      **     **      **     **        **        **        **   

**

   **   **   **     **      **     **      **     **        **        **        **   

**

   **   **   **     **      **     **      **     **        **        **        **   

**

   **   **   **     **      **     **      **     **        **        **        **   

**

   **   **   **     **      **     **      **     **        **        **        **   

**

   **   **   **     **      **     **      **     **        **        **        **   

**

   **   **   **     **      **     **      **     **        **        **        **   

**

   **   **   **     **      **     **      **     **        **        **        **   
        

 

 

   

 

 

 

 

   

 

 

 

 

   

 

 

   

 

 

   

 

 

 

Grand Total

         $ 126,500.00      **     4,860,933      **   $ 131,360,933        3,541,000        134,901,933      $ 134,901,933   
        

 

 

   

 

 

 

 

   

 

 

 

 

   

 

 

   

 

 

   

 

 

 
               **            $ (134,901,933  
            

 

 

         

 

 

   


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #3

To

Firm Fixed Price Agreement No. 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitalGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

This Modification is associated with an update of “Exhibit 1 WV3 SOW for ITT” to reflect an update of the WV3 Instrument Specification from Rev. 2 to Rev. 3.

Both DG and ITT hereby agree to amend the referenced Agreement as follows:

 

  1) Replace SOW Revision 3.0 with SOW Revision 4.0 (Document #10329744) dated January 20, 2011.

This documentation update does not affect the total contract price herein.

All other terms and conditions of the Agreement not noted as changed remain in full force and effect.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a legally binding agreement.

 

ITT Space Systems, LLC   DigitalGlobe, Inc.

/s/ [**REDACTED**]

 

/s/ Steve Linn

Signature   Signature

[**REDACTED**]

 

Steve Linn

Name   Name

[**REDACTED**]

 

Sr Director – Space Systems

    Title
Date:  

January 25, 2011

  Date:  

Jan 25, 2011


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #4

[**REDACTED**]

To

Firm Fixed Price Agreement No. 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitalGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260; Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

The parties hereby agree to amend the Agreement as Mows:

1) Update and replace the Technical Specification #3.0 (document #10329744) dated 1/7/2011

2) Replace Exhibit #2 (Milestone Payment and Termination Liability Schedule) with the revised milestone payment scheduled referenced hereto as Exhibit #2 dated 2/5/2011 (attached)

 

Original Contract Value

     FFP       $  134,901,933   

This Modification [**REDACTED**]

     FFP       $ 188,000   
     

 

 

 

Adjusted TOTAL Contract Value

      $ 135,089,933   
     

 

 

 

The total contract price is herein changed from $134,901,933 to $135,089,933

All other terms and conditions of the Agreement not noted as changed herein remain in full force and effect.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a binding agreement.

 

ITT Space Systems, LLC   DigitalGlobe, Inc.

/s/  [**REDACTED**]

 

/s/ Neal T. Anderson

Signature   Signature
[**REDACTED**]   Name: Neal T. Anderson
[**REDACTED**]   Title: VP, Tech. Dev.
Date:  

3/17/2011

  Date:  

16 Mar 2011


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

WV3 Milestone Payment Plan
EDC - Effective Date of Contract

Nominal

Date

  

Date

  

Milestone

Value

**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
     

 

   GRAND TOTAL    $135,259,933
     

 


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

ITT WV3 Termination Liability Schedule   3/16/2011

 

Date

   Gross TL

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #5

[**REDACTED**]

To

Firm Fixed Price Agreement No 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitalGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260; Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 140 St. Paul Street, P.O. Box 601188, Rochester, New York 14506-0488.

The parties hereby agree to amend the Agreement as follows:

1) Update and replace the Technical Specification #3.0 (document #10329744) dated 1/17/2011

2) Replace Exhibit #2 (Milestone Payment and Termination Liability Schedule) with the revised milestone payment scheduled referenced hereto as Exhibit #2 dated 2/5/2011 (attached)

 

Original Contract Value

     FFP       $ 135,089,933   

This Modification [**REDACTED**]

     FFP       $ 170,000   
     

 

 

 

Adjusted Total Contract Value

      $ 135,259,933   
     

 

 

 

The total contract price is herein changed from $135,089,933 to $135,259,933

All other terms and conditions of the Agreement not noted as changed herein remain in full force and effect.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a binding agreement.

 

ITT Space Systems, LLC   DigitalGlobe, Inc.

/s/ [**REDACTED**]

 

/s/ Neal T. Anderson

Signature   Signature
[**REDACTED**]   Name: Neal T. Anderson
[**REDACTED**]   Title: VP, Tech. Dev.
Date:  

3/17/2011

  Date:  

16 Mar 2011


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

WV3 Milestone Payment Plan
EDC - Effective Date of Contract

Nominal

Date

  

Date

  

Milestone

Value

**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
**    **    $**
     

 

   GRAND TOTAL    $135,259,933
     

 


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

ITT WV3 Termination Liability Schedule   3/16/2011

 

Date

  

Gross TL

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

**

   **

 

ITT Proprietary  
Competition Sensitive   Page 1 of 1


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #7

[**REDACTED**]

to

Firm Fixed Price Agreement No. 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitalGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260: Longmont, Colorado 80503; and ITT Space Systems, ILC (ITT), a limited liability company organized and existing under the laws of the Stale of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

The parties hereby agree to amend the Agreement as follows:

1) As stipulated in the attached SOW.

 

Original Contract Value

   FFP    $ 135,259,933   

This Modification [ **REDACTED** ]

   FFP    $ 400,000   
     

 

 

 

Adjusted Total Contract Value

      $ 135,659,933   
     

 

 

 

The total contract price Is herein changed from $135,259,933 to $135,659,933

All other terms and conditions of the Agreement not noted as changed herein remain in full force and effect.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a binding agreement.

 

ITT Space Systems, LLC   DigitalGlobe, Inc.

    /s/ [**REDACTED**]

   

    /s/ Neal T. Anderson

Signature     Signature
[**REDACTED**]     Name: Neal T. Anderson
[**REDACTED**]     Title: VP, Technology Development
Date:  

5/02/2011

  Date:  

5-02-11


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

**REDACTED**


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #8

[**REDACTED**]

To

Firm Fixed Price Agreement No. 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitalGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260; Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

The parties hereby agree to amend the Agreement as follows:

 

Original Contract Value    FFP    $  135,659,933   
This Modification [**REDACTED**]    FFP    $ 781,000   
     

 

 

 
Adjusted TOTAL Contract Value       $ 136,440,933   
     

 

 

 

The total contract price is herein changed from $135,659,933 to $136,440,933

All other terms and conditions of the Agreement not noted as changed herein remain in full force and effect.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a binding agreement.

 

ITT Space Systems, LLC   DigitalGlobe, Inc.

/s/ [**REDACTED**]

 

/s/ Neal T. Anderson

Signature   Signature
[**REDACTED**]   Name:    Neal T. Anderson
[ **REDACTED** ]   Title:    VP, Technology Development
Date:  

5/20/2011

  Date:   

5-20-11


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #9

[ **REDACTED** ]

To

Firm Fixed Price Agreement No. 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitalGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

The parties hereby agree to amend the Agreement as follows:

WorldView-3 Instrument Specification

Document #10329742

Revision #4

All other terms and conditions of the Agreement not noted as changed herein remain in full force and effect.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a binding agreement.

 

ITT Space Systems, LLC   DigitalGlobe, Inc.

/s/ [**REDACTED**]

 

/s/ Neal T. Anderson

Signature   Signature
[**REDACTED**]   Name: Neal T. Anderson
[**REDACTED**]   Title: VP, Technology Development
Date:  

Nov. 15, 2011

  Date:  

14 November 2011


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #10

[**REDACTED**]

To

Firm Fixed Price Agreement No 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitalGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

The parties hereby agree to amend the Agreement as follows:

 

Original Contract Value

   FFP    $ 136,440,933   

This modification [ **REDACTED** ]

   FFP    $ 3,800,000   
     

 

 

 

Adjusted TOTAL Contract Value

      $ 140,240,933   
     

 

 

 

Statement of Work as appears on ATP Letter dated June 7, 2011:

[ **REDACTED** ]

Updates to exhibit 2 —WV instrument Milestone Schedule:

[ **REDACTED** ]

[ **REDACTED** ]

[ **REDACTED** ]

All other terms and conditions of the Agreement not noted as changed herein remain in full force and effect.


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #10

[**REDACTED**]

Page 2

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a binding agreement.

 

ITT Space Systems, LLC   DigitalGlobe, Inc.

/s/ [**REDACTED**]

 

/s/ Neal Anderson

Signature   Signature
[**REDACTED**]   Name:   Neal Anderson
[**REDACTED**]   Title:   VP, Technology Development
Date:  

13 June 2011

  Date:  

13 June 2011


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #11

[ **REDACTED** ]

To

Firm Fixed Price Agreement No. 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) Is entered into by and between DigitalGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

The parties hereby agree to amend the Agreement as follows:

 

   

[ **REDACTED** ]

 

   

[ **REDACTED** ]

 

   

[ **REDACTED** ]

 

Original Contract Value

     FFP       $  140,240,933   

This Modification [ **REDACTED** ]

     FFP       $ 336,000   
     

 

 

 

Adjusted TOTAL Contract Value

      $ 140,576,933   
     

 

 

 

This modification will result in additional mutually agreeable payment milestone(s).

All other terms and conditions of the Agreement not rioted as changed herein remain in full force and effect. The Technical Specifications and the Statement of Work will be modified to reflect any and all changes associated with this activity.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a binding agreement.

 

ITT Space Systems, LLC   DigitalGlobe, Inc.

/s/ [ **REDACTED** ]

 

/s/ Neal T. Anderson

Signature   Signature
[ **REDACTED** ]   Name: Neal T. Anderson
[ **REDACTED** ]   Title: VP, Technology Development
Date: Nov. 15, 2011                               Date: 14 November 2011                

 


FOIA CONFIDENTIAL TREATMENT REQUESTED

PORTIONS OF THIS EXHIBIT MARKED BY ** OR BY [**REDACTED**] HAVE BEEN OMITTED PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION

 

Modification #12

[**REDACTED**]

To

Firm Fixed Price Agreement No. 60151

This Modification to Firm Fixed Price Agreement number 60151 (“the Agreement”) is entered into by and between DigitaiGlobe, Inc. (DG), a corporation organized and existing under the laws of the State of Delaware, with a place of business at 1601 Dry Creek Drive, Suite 260, Longmont, Colorado 80503; and ITT Space Systems, LLC (ITT), a limited liability company organized and existing under the laws of the State of Delaware, with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New York 14606-0488.

The parties hereby agree to amend the Agreement as follows:

 

   

[ **REDACTED**]

 

   

Acceptance of Technical Specification Revision #5

 

Original Contract Value

     FFP       $ 140,576,933   

This Modification [ **REDACTED** ]

     FFP       $ 112,000   
     

 

 

 

Adjusted TOTAL Contract Value

      $ 140,688,933   
     

 

 

 

The proposed payment milestone(s) will be: [ **REDACTED**]

All other terms and conditions of the Agreement not noted as changed herein remain in full force and effect. The Technical Specifications and the Statement of Work will be modified to reflect any and all changes associated with this activity.

This Modification is hereby executed and agreed to by the undersigned parties effective the last date written below as signified by the signatures and shall be a binding agreement.

 

ITT Space Systems, LLC   DigitalGlobe, Inc.

/s/ [**REDACTED**]

 

/s/ Neal T. Anderson

Signature   Signature
[ **REDACTED** ]   Name: Neal Anderson
[ **REDACTED** ]   Title: Vice President, Technology Development
Date:  

11/2/2011

  Date:   

11/3/2011

Exhibit 10.10

FIRST AMENDMENT TO LEASE

This First Amendment to Lease (this “Amendment”) is made as of the 14 th day of October, 2011 by and among HUB PROPERTIES TRUST, a Maryland real estate investment trust (“ Landlord ”) and DIGITALGLOBE, INC., a Delaware corporation (“ Tenant ”).

WHEREAS, K/B FUND IV (“ Original Landlord ”) and Tenant entered into that certain Office Lease, dated March 19, 2004 (the “ Lease ”) for the lease of certain premises (the “ Premises ”) known as Suite 260 and located in a portion of the building (the “ Building ”) located at 1601 Dry Creek Drive, Longmont, Colorado, as more particularly described in the Lease; and

WHEREAS, Landlord has succeeded to the interest of the Original Landlord under the Lease; and

WHEREAS, Tenant has elected to convert certain Storage Space in the Building to Office Space, upon the terms and conditions hereinafter set forth;

NOW, THEREFORE, in consideration of the foregoing and for other consideration, the mutual receipt and sufficiency of which are hereby acknowledged, Landlord and Tenant agree that the Lease is hereby amended as follows:

1. Capitalized terms not otherwise defined in this Amendment shall have the meanings attributed to such terms in the Lease.

2. With respect to the portion of the Lease Term commencing on the Conversion Date (as hereinafter defined), the Rentable Area of Office Space shall be expanded to include 20,015 square feet of Office Space to be converted by Tenant from Storage Space (the “ Conversion Space ”), such that the Rentable Area shall be 174,003 square feet of office space, substantially as shown cross-hatched or outlined on Exhibit A attached hereto, and 11,263 square feet of storage space, substantially as shown cross-batched or outlined on Exhibit A-1 attached hereto, provided that the Rentable Area of Office Space and the Rentable Area of Storage Space shall be subject to adjustment as set forth in Section 8 below. Landlord and Tenant shall execute a document confirming the Conversion Date after it has occurred, but the failure of Landlord and Tenant to execute or deliver such document shall have no effect upon such date.

3. With respect to the portion of the Lease Term commencing on the Conversion Date, Base Annual. Rent for Office Space shall be as follows:

 

Dates

   PSF of Rentable
Area of Office
Space per annum
     Base Annual
Rent
     Monthly
Installments
 

Conversion Date — 8/31/12

   $ 11.00       $ 1,914,033.00       $ 159,502.75   

9/01/12-8/31/13

   $ 11.50       $ 2,001,034.50       $ 166,752.88   

9/01/13-8/31/14

   $ 12.00       $ 2,088,036.00       $ 174,003.00   

9/01/14-8/31/1.5

   $ 12.50       $ 2,175,037.50       $ 181,253.13   


For purposes of the schedule set forth above, if the Conversion Date is any day other than the first day of a calendar month, then the monthly payment of Base Annual Rent for Office Space for such month in which the Conversion Date occurs shall be an amount which is equal to the sum of (i) $141,155.67 multiplied by the number of days from the first day of such month through the day immediately preceding the Conversion Date and (ii) $159,502.75 (being the Monthly Installment of Base Annual Rent for Office Space due from and after the Conversion Date for the month in which the Conversion Date occurs, which amount shall be adjusted as set forth in Section 8 below) multiplied by the number of days from the Conversion Date through the last day of the month in which the Conversion Date occurs (inclusive of both dates in clauses (i) and (ii)).

4. With respect to the portion of the Lease Term commencing on the Conversion Date, Base Annual Rent for Storage Space shall be as follows:

 

Dates

   PSF of Rentable
Area of Storage
Space per annum
     Base Annual
Rent
     Monthly
Installments
 

Conversion Date — 8/31/12

   $ 2.25       $ 25,341.75       $ 2,111.81   

9/01/12-8/31/13

   $ 2.32       $ 26,130.16       $ 2,177.51   

9/01/13-8/31/14

   $ 2.39       $ 26,918.57       $ 2,243.21   

9/01/14-8/31/15

   $ 2.46       $ 27,706.98       $ 2,308.92   

For purposes of the schedule set forth above, if the Conversion Date is any day other than the first day of a calendar month, then the monthly payment of Base Annual Rent for Storage Space for such month in which the Conversion Date occurs shall be an amount which is equal to the sum of (i) $5,864.63 multiplied by the number of days from the first day of such month through the day immediately preceding the Conversion Date and (ii) $2,111.81 (being the Monthly Installment of Base Annual Rent for Storage Space due from and after the Conversion Date for the month in which the Conversion Date occurs, which amount shall be adjusted as set forth in Section 8 below) multiplied by the number of days from the Conversion Date through the last day of the month in which the Conversion Date occurs (inclusive of both dates in clauses (i) and (ii)).

5. With respect to the portion of the Lease Term commencing on the Conversion Date, Tenant’s Proportionate Share of Operating Costs for Office Space, as set forth in Section 4(a) of the Lease, shall be 31,802%.

6. The “ Conversion Date ” shall be the earlier of (i) March 1, 2012 or (ii) the date on which Tenant’s Conversion Work, as defined below, is substantially complete, as defined below.

7. Tenant shall be responsible for making any alterations or improvements necessary to cause the Conversion Space to be usable as general office space, subject to Landlord’s


approval as hereinafter provided, at Tenant’s sole cost and expense except that Landlord shall provide Tenant with the Conversion Allowance as a contribution towards the costs of Tenant’s Conversion Work, as hereinafter defined. Promptly after the date of this Amendment, Tenant shall cause its architect (who shall be licensed in the State of Colorado) to prepare schematic diagrams and a set of drawings (such schematic diagrams and drawings being hereinafter referred to as “ Tenant’s Conversion Plans ”) to be used by Tenant for the design and permitting of Tenant’s Conversion Work, which Tenant’s Conversion Plans shall show the alterations and improvements that Tenant intends to make to the Conversion Space, and Tenant shall deliver Tenant’s Conversion Plans to Landlord no later than two (2) weeks prior to the date on which Tenant intends to commence Tenant’s Conversion Work. Landlord shall respond to Tenant’s Conversion Plans (either by approval, request for additional information, request for revision or communication of a reason for failure to approve) within five (5) business days (meaning all calendar days except Saturdays and Sundays and holidays observed by banks in the State of Colorado) after the date of Landlord’s receipt of Tenant’s Conversion Plans (or any resubmission), plus such additional period of time as may be necessary for review of Tenant’s Conversion Plans by a third-party architect, engineer or other consultant if Landlord determines that any aspect of Tenant’s Conversion Plans requires such third-party review. Unless Landlord shall have unconditionally approved all of Tenant’s Conversion Plans, Tenant shall deliver to Landlord such additional information, documentation and/or revisions to Tenant’s Conversion Plans as are necessary to obtain Landlord’s approval of Tenant’s Conversion Plans and this process shall continue until Tenant’s Conversion Plans are approved by Landlord.

After approval of Tenant’s Conversion Plans by Landlord and receipt of all applicable permits from the local governing authority, copies of which shall be delivered to Landlord prior to the commencement of Tenant’s Conversion Work, Tenant shall cause its contractor(s) and subcontractor(s) to perform the work specified therein (“ Tenant’s Conversion Work ”) in accordance with Tenant’s Conversion Plans, diligently and continuously until Tenant’s Conversion Work is substantially complete. Tenant’s Conversion Work shall be performed in compliance with the provisions and requirements of Exhibit B to the Lease and all other applicable provisions of the Lease; in a good and workmanlike manner; by contractors and subcontractors approved by Landlord; in compliance with all applicable laws, codes, regulations, permits and approvals; at such times and in such manner so as not to disturb other tenants of the Building or Building operations; and in accordance with any reasonable directions that may be given, from time to time, by Landlord’s agent. Tenant’s contractors and subcontractors shall carry the insurance required by Section (c) of Exhibit B of the Lease and shall, prior to commencing any work, submit certificates of insurance to Landlord’s agent evidencing that all such required insurance is in effect.

Tenant’s Conversion Work shall be deemed to be substantially complete on the first day as of which Tenant’s Conversion Work has been completed except for items of work (and, if applicable, adjustment of equipment and fixtures) which can be completed after occupancy has been taken without causing undue interference with Tenant’s use of the Conversion Space as office space (i.e. so-called “punch list” items) and any new or amended certificate of occupancy, letter of completion or similar documentation from the City of Longmont necessary as a result of such Tenant Conversion Work has been issued.

Provided the Lease is in full force and effect and Tenant is not in default hereunder, then Landlord will provide Tenant with the Conversion Allowance in an amount not to exceed $12.73


per square foot of Conversion Space, which shall be used and disbursed in accordance with the provisions and procedures set forth in Exhibit B to the Lease relating to the Office Space, except that prior to the release of the remainder of the Conversion Allowance Tenant shall deliver to Landlord, in addition to the items required by Section (a)(ii) of Exhibit B of the Lease, a record set of plans incorporating and documenting each change that is a variance from the approved Tenant’s Conversion Plans, which record set shall be provided to Landlord in hard copy and Auto CADD format.

Both Landlord and Tenant shall appoint one individual as its “ Construction Representative ” who is authorized to act on its behalf in connection with any matters arising pursuant to this Section 7. The Construction Representative may be changed from time to time by notice hereunder from the then current Construction Representative to the other party’s Construction Representative or by notice from Landlord or Tenant pursuant to Section 19(c) of the Lease. The initial Construction Representatives shall be Sandy Grasso (Landlord) and Robin Kirchenbauer (Tenant). Notwithstanding Section 19(c) of the Lease, any notices or other communication under this Section 7 may be made by letter or other writing sent by U.S. mail, facsimile or email, provided the communication is made by one party’s Construction Representative to the other party’s Construction Representative.

8. The parties acknowledge that the square footage of the Conversion Space, as set forth in this Amendment, is an estimate only, and that upon delivery of the record set of plans to Landlord, as required by Section 7 above, the parties shall execute a confirmatory document or amendment to the Lease setting forth the actual square footage of the Conversion Space and the necessary adjustments to the Rentable Area of Office Space, Rentable Area of Storage Space, Base Annual Rent for Office Space, Base Annual Rent for Storage Space and Tenant’s Proportionate Share of Operating Costs for Office Space to reflect such actual square footage.

9. The parties acknowledge the existence of asbestos in the floor adhesive in the Conversion Space which was not previously required to be abated by Landlord. In connection with the performance of Tenant’s Conversion Work, Tenant, using industry accepted standards, shall remove such asbestos from the Conversion Space (the “Remediation Work”). The Remediation Work shall be performed in compliance with all Hazardous Materials Laws and the Remediation Plan, as defined below. Following such necessary actions, Tenant shall provide written evidence of such actions to Landlord.

Tenant shall obtain a bid for the performance of the Remediation Work and shall submit same to Landlord for Landlord’s review and approval, which shall include approval of the proposed contactor, remediation plan and price (collectively, the “Remediation Plan”). Upon Landlord’s approval of the Remediation Plan, Tenant shall cause the Remediation Work to be performed to completion in accordance with the approved Remediation Plan. Upon completion of the Remediation Work and submission to Landlord of (i) an itemized statement of the costs of the Remediation Work, (ii) complete copies of paid bills for the Remediation Work, (iii) full and final lien waivers from all contractors, subcontractors and suppliers in connection with the Remediation Work, as applicable, and (iv) evidence that any required governmental inspections and approvals have been successfully completed, Landlord shall reimburse Tenant for the cost of the performance of the Remediation Work in an amount not to exceed the amount set forth in the approved Remediation Plan.


10. Section 14 of the Lease is hereby amended to reflect that Landlord’s Address for Notices shall be:

Hub Properties Trust

c/o Reit Management & Research LLC

5627 Oberlin Drive, Suite 124

San Diego, CA 92121

Attention: Vice President, Southwest Region

with a copy to:

Reit Management & Research LLC

Two Newton Place

255 Washington Street, Suite 300

Newton, MA 02458

Attention: Jennifer B. Clark

11. Section 15 of the Lease is hereby amended to reflect that the Place of Payment shall be:

Hub Properties Trust

P.O. Box 845911

Boston, MA 02284-5911

12. Tenant warrants and represents that it has dealt with no broker in connection with the consummation of this Amendment other than CB Richard Ellis, and in the event of any brokerage claims or liens against Landlord or the Property predicated upon or arising out of prior dealings with Tenant, other than by CB Richard Ellis, Tenant agrees to defend the same and indemnify and hold Landlord harmless against any such claim, and to discharge any such lien.

13. In addition to all other limitations contained in the Lease, as amended hereby, Landlord hereby notifies Tenant that the Declaration of Trust of Hub Properties Trust provides, and Tenant agrees, that no trustee, officer, shareholder, employee or agent of Hub Properties Trust shall be held to any personal liability, jointly or severally, for any obligation of, or claim against, Hub Properties Trust.

14. As amended hereby, the Lease is hereby ratified and confirmed.

[Remainder of page intentionally left blank.]


IN WITNESS WHEREOF, the parties hereunto have executed this Amendment as of the date first written above.

 

LANDLORD:
HUB PROPERTIES TRUST
By:  

/s/ David M. Lepore

  David M. Lepore
  Senior Vice President
TENANT:
DIGITALGLOBE, INC.
By:  

/s/ Scott Hicar

  Name:   Scott Hicar
  Title:   CIO

Exhibit 10.26

Approved by DigitalGlobe, Inc. Board on June 14, 2007

Approved by Stockholders June 21, 2007

Amended by DigitalGlobe, Inc. Board on March 6, 2008

DIGITALGLOBE, INC.

2007 EMPLOYEE STOCK OPTION PLAN

 

 

Plan Document

 

 


Approved by DigitalGlobe, Inc. Board on June 14, 2007

Approved by Stockholders June 21, 2007

Amended by DigitalGlobe, Inc. Board on March 6, 2008

DIGITALGLOBE, INC.

2007 EMPLOYEE STOCK OPTION PLAN

 

 

Plan Document

 

 

1. Establishment, Purpose, and Types of Awards

DigitalGlobe (the “ Company ”) hereby establishes this “ 2007 Employee Stock Option Plan ” (hereinafter referred to as the “ Plan ”), in order to provide equity-based incentives and awards to select employees, directors, consultants, and advisors of the Company and its Affiliates. The Plan permits the granting of the following types of awards (“ Awards ”), Options (Section 6), Stock Appreciation Rights (Section 7), and Restricted Shares, Restricted Share Units and Unrestricted Shares (Section 8). To the extent required by Applicable Law, security holders will be provided with Company financial statements at least annually.

Except as provided in an Award Agreement, the Plan shall not affect any stock options, equity-based compensation, or other benefits that the Company or its Affiliates may have provided, or may separately provide in the future pursuant to any agreement, plan, or program that is independent of this Plan.

2. Defined Terms

Terms in the Plan that begin with an initial capital letter have the defined meaning set forth in Appendix A , unless defined elsewhere in this Plan or the context of their use clearly indicates a different meaning.

3. Shares Subject to the Plan

Subject to the provisions of Section 11 of the Plan, the maximum number of Shares that the Company may issue for all Awards is 25,000,000 Shares (which shall be adjusted upward by 2% on each anniversary of the effective date of the Plan during the term of the Plan). Shares that are subject to an Award that for any reason expires, is forfeited, is cancelled, or becomes unexercisable, and Shares that are for any other reason not paid or delivered under this Plan shall again, except to the extent prohibited by Applicable Law, be available for subsequent Awards under the Plan. In addition, the Committee may make future Awards with respect to Shares that the Company retains from otherwise delivering pursuant to an Award under this Plan either (i) as payment of the exercise price of an Award, or (ii) in order to satisfy the withholding or employment taxes due upon grant, exercise, vesting or distribution of an Award. Notwithstanding the foregoing, but subject to adjustments pursuant to Section 11 below, the number of Shares that are available for ISO Awards shall be determined, to the extent required under applicable tax laws, by reducing the number of Shares designated in the first sentence of this paragraph by the number of Shares granted pursuant to Awards (whether or not Shares are issued pursuant to such Awards), provided that any Shares that are either issued or purchased under the Plan and forfeited back to the Plan, or surrendered in payment of the Exercise Price for an Award shall be available for issuance pursuant to future ISO Awards.


4. Administration

(a)  General . The Committee shall administer the Plan in accordance with its terms, provided that the Board may act in lieu of the Committee on any matter. The Committee shall hold meetings at such times and places as it may determine and shall make such rules and regulations for the conduct of its business as it deems advisable. In the absence of a duly appointed Committee, the Board shall function as the Committee for all purposes of the Plan.

(b)  Committee Composition . The Board shall appoint the members of the Committee. If and to the extent permitted by Applicable Law, the Committee may authorize one or more Reporting Persons (or other officers) to make Awards to Eligible Persons who are not Reporting Persons (or other officers whom the Committee has specifically authorized to make Awards). The Board may at any time appoint additional members to the Committee, remove and replace members of the Committee with or without cause, and fill vacancies on the Committee.

(c)  Powers of the Committee . Subject to the provisions of the Plan, the Committee shall have the authority, in its sole discretion:

(i) to grant Awards;

(ii) to determine Eligible Persons to whom Awards shall be granted from time to time and the number of Shares, to be covered by each Award;

(iii) to determine, from time to time, the Fair Value of Shares;

(iv) to determine, and to set forth in Award Agreements, the terms and conditions of all Awards, including any applicable exercise or purchase price, the installments and conditions under which an Award shall become vested (which may be based on performance), terminated, expired, cancelled, or replaced, and the circumstances for vesting acceleration or waiver of forfeiture restrictions, and other restrictions and limitations;

(v) to approve the forms of Award Agreements and all other documents, notices and certificates in connection therewith which need not be identical either as to type of Award or among Participants (The initial form of Award Agreement is set forth in Exhibit “1.” Modification to the Exhibits shall not constitute an amendment to the Plan);

(vi) to construe and interpret the terms of the Plan and any Award Agreement, to determine the meaning of their terms, and to prescribe, amend, and rescind rules and procedures relating to the Plan and its administration;

(vii) in order to fulfill the purposes of the Plan and without amending the Plan, to modify, to cancel, or to waive the Company’s rights with respect to any Awards, to adjust or to modify Award Agreements for changes in Applicable Law, and to recognize differences in foreign law, tax policies, or customs; and

(viii) to make all other interpretations and to take all other actions that the Committee may consider necessary or advisable to administer the Plan or to effectuate its purposes.

 

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Subject to Applicable Law and the restrictions set forth in the Plan, the Committee may delegate administrative functions to individuals who are Reporting Persons, officers, or Employees of the Company or its Affiliates.

Notwithstanding any provision to the contrary in the Plan, the Committee shall have the discretion to grant options under the Plan that, to the extent so designated in the applicable Award Agreement, shall be treated as if such options were granted under the Earthwatch Incorporated 1999 Equity Incentive Plan, as in effect from time to time (a copy of the Equity Incentive Plan in effect on April 1, 2007 is attached as Exhibit “2”), instead of the Plan.

(d)  Deference to Committee Determinations . The Committee shall have the discretion to interpret or construe ambiguous, unclear, or implied (but omitted) terms in any fashion it deems to be appropriate in its sole discretion, and to make any findings of fact needed in the administration of the Plan or Award Agreements. The Committee’s prior exercise of its discretionary authority shall not obligate it to thereafter exercise its authority in a like fashion. The Committee’s interpretation and construction of any provision of the Plan, or of any Award or Award Agreement, shall be final, binding, and conclusive. The validity of any such interpretation, construction, decision or finding of fact shall not be given de novo review if challenged in court, by arbitration, or in any other forum, and shall be upheld unless clearly made in bad faith or materially affected by fraud.

(e)  No Liability; Indemnification . Neither the Board nor any Committee member, nor any Person acting at the direction of the Board or the Committee, shall be liable for any act, omission, interpretation, construction or determination made in good faith with respect to the Plan, any Award or any Award Agreement. The Company and its Affiliates shall pay or reimburse any member of the Committee, as well as any Director, Employee, or Consultant who takes action on behalf of the Plan, for all expenses incurred with respect to the Plan, and to the full extent allowable under Applicable Law shall indemnify each and every one of them for any claims, liabilities, and costs (including reasonable attorney’s fees) arising out of their good faith performance of duties on behalf of the Plan.

5. Eligibility

(a)  General Rule . Subject to the express provisions of the Plan, the Committee shall determine from the class of Eligible Persons those individuals to whom Awards under the Plan may be granted, the number of Shares subject to each Award, the price (if any) to be paid for the Shares or the Award. The Committee may grant ISOs only to Employees (including officers who are Employees) of the Company or any Affiliate that is a “parent corporation” or “subsidiary corporation” within the meaning of Section 424 of the Code, and may grant all other Awards to any Eligible Person. A Participant who has been granted an Award may be granted an additional Award or Awards if the Committee shall so determine, if such person is otherwise an Eligible Person and if otherwise in accordance with the terms of the Plan.

(b)  Documentation of Awards . Each Award shall be evidenced by an Award Agreement signed by the Company and, if required by the Committee, by the Participant. The Award Agreement shall set forth the material terms and conditions of the Award established by the Committee, and each Award shall be subject to the terms and conditions set forth in this Plan unless otherwise specifically provided in an Award Agreement, as permitted by this Plan.

 

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(c)  Limits on Awards . During the term of the Plan, no Participant may receive Options or other Awards that relate to more than 20% of the total number of Shares reserved for Awards pursuant to Section 3 above, as adjusted pursuant to Section 11 below.

(d)  Replacement Awards . Subject to Applicable Laws (including any associated Shareholder approval requirements), the Committee may, in its sole discretion and upon such terms as it deems appropriate, require as a condition of the grant of an Award to a Participant that the Participant surrender for cancellation some or all of the Awards that have previously been granted to the Participant under this Plan or otherwise. An Award that is conditioned upon such surrender may or may not be the same type of Award, may cover the same (or a lesser or greater) number of Shares as such surrendered Award, may have other terms that are determined without regard to the terms or conditions of such surrendered Award, and may contain any other terms that the Committee deems appropriate. In the case of Options, these other terms may not involve an Exercise Price that is lower than the exercise price of the surrendered Option unless the Company’s shareholders approve the grant itself or the program under which the grant is made pursuant to the Plan.

6. Option Awards

(a)  Types; Documentation . Subject to Section 5(a), the Committee may in its discretion grant Options pursuant to Award Agreements that are delivered to Participants. Each Option shall be designated in the Award Agreement as an ISO or a Non-ISO, and the same Award Agreement may grant both types of Options. At the sole discretion of the Committee, any Option may be exercisable, in whole or in part, immediately upon the grant thereof, or only after the occurrence of a specified event, or only in installments, which installments may vary. Options granted under the Plan may contain such terms and provisions not inconsistent with the Plan that the Committee shall deem advisable in its sole and absolute discretion.

(b)  ISO $100,000 Limitation . To the extent that the aggregate Fair Value of Shares with respect to which Options designated as ISOs first become exercisable by a Participant in any calendar year (under this Plan and any other plan of the Company or any Affiliate) exceeds $100,000, such excess Options shall be treated as Non-ISOs. For purposes of determining whether the $100,000 limit is exceeded, the Fair Value of the Shares subject to an ISO shall be determined as of the Grant Date. In reducing the number of Options treated as ISOs to meet the $100,000 limit, the most recently granted Options shall be reduced first. In the event that Section 422 of the Code is amended to alter the limitation set forth therein, the limitation of this Section 6(b) shall be automatically adjusted accordingly.

(c)  Term of Options . Each Award Agreement shall specify a term at the end of which the Option automatically expires, subject to earlier termination provisions contained in Section 6(h) hereof; provided, that, the term of any Option may not exceed ten years from the Grant Date. In the case of an ISO granted to an Employee who is a Ten Percent Holder on the Grant Date, the term of the ISO shall not exceed five years from the Grant Date.

(d)  Exercise Price . The exercise price of an Option shall be determined by the Committee in its sole discretion and shall be set forth in the Award Agreement, provided that —

 

  (i) the per Share exercise price shall not be less than the Fair Value per Share on the Grant Date, and

 

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  (ii) the per Share exercise price shall not be less than 110% of the Fair Value per Share on the Grant Date for any Options granted to (a) an Employee who is a Ten Percent Holder on the Grant Date or (b) any person who owns securities possessing more than 10% of the total combined voting power (as defined in Section 194.5 of the California Corporations Code) of all classes of securities of the Company or its parent or subsidiaries possessing voting power.

(e)  Exercise of Option . The times, circumstances and conditions under which an Option shall be exercisable shall be determined by the Committee in its sole discretion and set forth in the Award Agreement. The Committee shall have the discretion to determine whether and to what extent the vesting of Options shall be tolled during any unpaid leave of absence; provided, however, that in the absence of such determination, vesting of Options shall be tolled during any such leave approved by the Company.

(f)  Methods of Exercise . Prior to its expiration pursuant to the terms of the applicable Award Agreement, and subject to the times, circumstances and conditions for exercise contained in the applicable Award Agreement, each Option may be exercised, in whole or in part (provided that the Company shall not be required to issue fractional shares), by delivery of written notice of exercise to the secretary of the Company (in the form approved by the Committee) accompanied by the full exercise price of the Shares being purchased. In the case of an ISO, the Committee shall determine the acceptable methods of payment on the Grant Date and it shall be included in the applicable Award Agreement (The initial form of exercise is attached as Exhibit “3”). The methods of payment that the Committee may in its discretion accept or commit to accept in an Award Agreement include:

(i) cash or check payable to the Company (in U.S. dollars);

(ii) other Shares that (A) are owned by the Participant who is purchasing Shares pursuant to an Option, (B) have a Fair Value on the date of surrender equal to the aggregate exercise price of the Shares as to which the Option is being exercised, (C) were not acquired by such Participant pursuant to the exercise of an Option, unless such Shares have been owned by such Participant for at least six months or such other period as the Committee may determine, (D) are all, at the time of such surrender, free and clear of any and all claims, pledges, liens and encumbrances, or any restrictions which would in any manner restrict the transfer of such Shares to or by the Company (other than such restrictions as may have existed prior to an issuance of such Shares by the Company to such Participant), and (E) are duly endorsed for transfer to the Company;

(iii) a cashless exercise program that the Committee may approve, from time to time, pursuant to which a Participant may concurrently provide irrevocable instructions (A) to such Participant’s broker or dealer to effect the immediate sale of the purchased Shares and remit to the Company, out of the sale proceeds available on the settlement date, sufficient funds to cover the exercise price of the Option plus all applicable taxes required to be withheld by the Company by reason of such exercise, and (B) to the Company to deliver the certificates for the purchased Shares directly to such broker or dealer in order to complete the sale; or

(iv) any combination of the foregoing methods of payment.

 

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The Company shall not be required to deliver Shares pursuant to the exercise of an Option until payment of the full exercise price therefore is received by the Company.

(g)  Vesting . Unless otherwise provided in an Award Agreement, 1/4 (25%) of the Options granted pursuant to an Award Agreement shall vest on the first anniversary of the date of grant and 1/36th of the remaining 75% shall vest thereafter on each of the first 36 monthly anniversaries of the date of grant, subject to the Participant remaining in Continuous Service on each such vesting date. The Committee may, in its sole discretion, waive any vesting provisions contained in an Award Agreement, but any such waiver must be in writing.

(h)  Termination of Continuous Service . The Committee may establish and set forth in the applicable Award Agreement the terms and conditions on which an Option shall remain exercisable, if at all, following termination of a Participant’s Continuous Service. The Committee may waive or modify these provisions at any time. To the extent that a Participant is not entitled to exercise an Option at the date of his or her termination of Continuous Service, or if the Participant (or other person entitled to exercise the Option) does not exercise the Option to the extent so entitled within the time specified in the Award Agreement or below (as applicable), the Option shall terminate and the Shares underlying the unexercised portion of the Option shall revert to the Plan and become available for future Awards. In no event may any Option be exercised after the expiration of the Option term as set forth in the Award Agreement.

The following provisions shall apply to the extent an Award Agreement does not specify the terms and conditions upon which an Option shall terminate when there is a termination of a Participant’s Continuous Service:

(i) Termination other than Upon Disability or Death or for Cause . In the event of termination of a Participant’s Continuous Service (other than as a result of Participant’s death, disability, or termination for Cause), the Participant shall have the right to exercise an Option at any time within 30 days following such termination (or such earlier date on which the Option expires) to the extent the Participant was entitled to exercise such Option at the date of such termination.

(ii) Disability . In the event of termination of a Participant’s Continuous Service as a result of his or her being Disabled, the Participant shall have the right to exercise an Option at any time within six months following such termination (or such earlier date on which the Option expires) to the extent the Participant was entitled to exercise such Option at the date of such termination.

(iii) Death . In the event of the death of a Participant during the period of Continuous Service since the Grant Date of an Option, or within 12 months following termination of the Participant’s Continuous Service, the Option may be exercised, at any time within 12 months following the date of the Participant’s death (or such earlier date on which the Option expires), by the Participant’s estate or by a person who acquired the right to exercise the Option by bequest or inheritance, but only to the extent the right to exercise the Option had vested at the date of death or, if earlier, the date the Participant’s Continuous Service terminated.

 

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(iv) Cause . If the Committee determines that a Participant’s Continuous Service terminated due to Cause or that the Company had Cause to terminate the Participant’s Continuous Service or would have had Cause if the Company had then known all of the relevant facts, the Participant shall forfeit the right to exercise any Option as of the time that the Committee determines that Cause first existed, and it shall be considered immediately null and void.

If there is a Securities and Exchange Commission blackout period that prohibits the buying or selling or Shares during any part of the ten (10) day period before the expiration of any Option based on the termination of a Participant’s Continuous Service (as described above), the period for exercising the Options shall be extended until ten (10) days beyond when such blackout period ends. Notwithstanding any provision hereof or within an Award Agreement, no Option shall ever be exercisable after the expiration date of its original term as set forth in the Award Agreement.

7. Share Appreciation Rights (SARs)

(a)  Grants . The Committee may in its discretion grant Share Appreciation Rights to any Eligible Person in any of the following forms:

(i) SARs related to Options . The Committee may grant SARs either concurrently with the grant of an Option or with respect to an outstanding Option, in which case the SAR shall extend to all or a portion of the Shares covered by the related Option. An SAR shall entitle the Participant who holds the related Option, upon exercise of the SAR and surrender of the related Option, or portion thereof, to the extent the SAR and related Option each were previously unexercised, to receive payment of an amount determined pursuant to Section 7(e) below. Any SAR granted in connection with an ISO will contain such terms as may be required to comply with the provisions of Section 422 of the Code and the regulations promulgated thereunder.

(ii) SARs Independent of Options . The Committee may grant SARs which are independent of any Option subject to such conditions as the Committee may in its discretion determine and set forth in the applicable Award Agreement.

(iii) Limited SARs . The Committee may grant SARs exercisable only upon or in respect of a Change in Control or any other specified event, and such limited SARs may relate to or operate in tandem or combination with or substitution for Options or other SARs, or on a stand-alone basis, and may be payable in cash or Shares based on the spread between the exercise price of the SAR, and (A) a price based upon or equal to the Fair Value of the Shares during a specified period, at a specified time within a specified period before, after or including the date of such event, or (B) a price related to consideration payable to Company’s shareholders generally in connection with the event.

(b) Exercise Price . The per Share exercise price of an SAR shall be determined in the sole discretion of the Committee, shall be set forth in the applicable Award Agreement, and shall be no less than the Fair Value of one Share. The exercise price of an SAR related to an Option shall be the same as the exercise price of the related Option.

 

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(c)  Exercise of SARs . An SAR may not have a term exceeding ten years from its Grant Date. Unless the Award Agreement otherwise provides, an SAR related to an Option will be exercisable at such time or times, and to the extent, that the related Option will be exercisable; provided that the Award Agreement shall not, without the approval of the shareholders of the Company, provide for a vesting period for the exercise of the SAR that is more favorable to the Participant than the exercise period for the related Option. An SAR granted independently of any other Award will be exercisable pursuant to the terms of the Award Agreement. Whether an SAR is related to an Option or is granted independently, the SAR may only be exercised when the Fair Value of the Shares underlying the SAR exceeds the exercise price of the SAR.

(d)  Effect on Available Shares . All SARs that may be settled in Shares shall be counted in full against the number of Shares available for awards under the Plan, regardless of the number of Shares actually issued upon settlement of the SARs.

(e)  Payment . Upon exercise of an SAR related to an Option and the attendant surrender of an exercisable portion of any related Award, the Participant will be entitled to receive payment of an amount determined by multiplying —

(i) the excess of the Fair Value of a Share on the date of exercise of the SAR over the exercise price per Share of the SAR, by

(ii) the number of Shares with respect to which the SAR has been exercised.

(iii) Notwithstanding the foregoing, an SAR granted independently of an Option (i) may limit the amount payable to the Participant to a percentage, specified in the Award Agreement but not exceeding one-hundred percent (100%), of the amount determined pursuant to the preceding sentence, and (ii) shall be subject to any payment or other restrictions that the Committee may at any time impose in its discretion, including restrictions intended to conform the SARs with Section 409A of the Code.

(f)  Form and Terms of Payment . Unless otherwise provided in an Award Agreement, all SARs shall be settled in Shares as soon as practicable after exercise. Subject to Applicable Law, the Committee may, in its sole discretion, provide in an Award Agreement that the amount determined under Section 7(e) above shall be settled solely in cash, solely in Shares (valued at their Fair Value on the date of exercise of the SAR), or partly in cash and partly in Shares, with cash paid in lieu of fractional shares.

(g)  Termination of Employment or Consulting Relationship . The Committee shall establish and set forth in the applicable Award Agreement the terms and conditions under which an SAR shall remain exercisable, if at all, following termination of a Participant’s Continuous Service. The provisions of Section 6(h) above shall apply to the extent an Award Agreement does not specify the terms and conditions upon which an SAR shall terminate when there is a termination of a Participant’s Continuous Service.

 

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8. Restricted Shares, Restricted Share Units, and Unrestricted Shares

(a)  Grants . The Committee may in its sole discretion grant restricted shares (“ Restricted Shares ”) to any Eligible Person and shall evidence such grant in an Award Agreement that is delivered to the Participant and that sets forth the number of Restricted Shares, the purchase price for such Restricted Shares (if any), and the terms upon which the Restricted Shares may become vested. In addition, the Company may in its discretion grant to any Eligible Person the right to receive Shares after certain vesting requirements are met (“ Restricted Share Units ”), and shall evidence such grant in an Award Agreement that is delivered to the Participant which sets forth the number of Shares (or formula, that may be based on future performance or conditions, for determining the number of Shares) that the Participant shall be entitled to receive upon vesting and the terms upon which the Shares subject to a Restricted Share Unit may become vested. The Committee may condition any Award of Restricted Shares or Restricted Share Units to a Participant on receiving from the Participant such further assurances and documents as the Committee may require to enforce the restrictions. In addition, the Committee may grant Awards hereunder in the form of unrestricted shares (“ Unrestricted Shares ”), which shall vest in full upon the date of grant or such other date as the Committee may determine or which the Committee may issue pursuant to any program under which one or more Eligible Persons (selected by the Committee in its sole discretion) elect to pay for such Shares or to receive Unrestricted Shares in lieu of cash bonuses that would otherwise be paid.

(b)  Vesting and Forfeiture . The Committee shall set forth in an Award Agreement granting Restricted Shares or Restricted Share Units, the terms and conditions under which the Participant’s interest in the Restricted Shares or the Shares subject to Restricted Share Units will become vested and non-forfeitable. Except as set forth in the applicable Award Agreement or as the Committee otherwise determines, upon termination of a Participant’s Continuous Service for any reason, the Participant shall forfeit his or her Restricted Shares and Restricted Share Units; provided that if a Participant purchases the Restricted Shares and forfeits them for any reason, the Company shall return the purchase price to the Participant only if and to the extent set forth in an Award Agreement.

(c)  Issuance of Restricted Shares Prior to Vesting . The Company shall issue stock certificates that evidence Restricted Shares pending the lapse of applicable restrictions, and that bear a legend making appropriate reference to such restrictions. Except as set forth in the applicable Award Agreement or as the Committee otherwise determines, the Company or a third party that the Company designates shall hold such Restricted Shares and any dividends that accrue with respect to Restricted Shares pursuant to Section 8(e) below.

(d)  Issuance of Shares upon Vesting . As soon as practicable after vesting of a Participant’s Restricted Shares (or of the right to receive Shares underlying Restricted Share Units) and the Participant’s satisfaction of applicable tax withholding requirements, the Company shall release to the Participant, free from the vesting restrictions, one Share for each vested Restricted Share (or issue one Share free of the vesting restriction for each vested Restricted Share Unit), unless an Award Agreement provides otherwise. No fractional shares shall be distributed, and cash shall be paid in lieu thereof.

(e) Dividends Payable on Vesting . Whenever Shares are released to a Participant or duly-authorized transferee pursuant to Section 8(d) above as a result of the vesting of Restricted Shares or

 

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the Shares underlying Restricted Share Units are issued to a Participant pursuant to Section 8(d) above, such Participant or duly authorized transferee shall also be entitled to receive (unless otherwise provided in the Award Agreement), with respect to each Share released or issued a number of Shares equal to the sum of (i) any stock dividends, which were declared and paid to the holders of Shares between the Grant Date and the date such Share is released from the vesting restrictions in the case of Restricted Shares or issued in the case of Restricted Share Units, and (ii) a number of Shares equal to the Shares that the Participant could have purchased at Fair Value on the payment date of any cash dividends for Shares if the Participant had received such cash dividends with respect to each Restricted Share or Share subject to a Restricted Share Unit Award between its Grant Date and its settlement date.

(f)  Section 83(b) Elections . A Participant may make an election under Section 83(b) of the Code (the “ Section 83(b) Election ”) with respect to Restricted Shares. If a Participant who has received Restricted Share Units promptly provides the Committee with written notice of his or her intention to make a Section 83(b) Election with respect to the Shares subject to such Restricted Share Units, the Committee may in its discretion convert the Participant’s Restricted Share Units into Restricted Shares, on a one-for-one basis, in full satisfaction of the Participant’s Restricted Share Unit Award. The Participant may then make a Section 83(b) Election with respect to those Restricted Shares.

9. Taxes

(a)  General . As a condition to the issuance or distribution of Shares pursuant to the Plan, the Participant (or in the case of the Participant’s death, the person who succeeds to the Participant’s rights) shall make such arrangements as the Company may require for the satisfaction of any applicable federal, state, local or foreign withholding tax obligations that may arise in connection with the Award and the issuance of Shares. The Company shall not be required to issue any Shares until such obligations are satisfied, and may unilaterally withhold Shares for this purpose. If the Committee allows or effectuates the withholding or surrender of Shares to satisfy a Participant’s tax withholding obligations, the Committee shall not allow Shares to be withheld in an amount that exceeds the minimum statutory withholding rates for federal and state tax purposes, including payroll taxes.

(b)  Default Rule for Employees . In the absence of any other arrangement authorized by the Committee or set forth in the Award Agreement, and to the extent permitted under Applicable Law, each Participant shall be deemed to have elected to have the Company withhold from the Shares or cash to be issued pursuant to an Award that number of Shares having a Fair Value determined as of the applicable Tax Date (as defined below) or cash equal to the minimum applicable tax withholding and employment tax obligations associated with an Award. If such withholding of Shares is not permitted for any reason, the Company shall satisfy any required withholding through withholding from cash compensation otherwise payable to the Participant. For purposes of this Section 9, the Fair Value of the Shares to be withheld shall be determined on the date that the amount of tax to be withheld is to be determined under the Applicable Law (the “ Tax Date ”).

(c) Surrender of Shares . If permitted by the Committee, in its discretion, a Participant may satisfy the minimum applicable tax withholding and employment tax obligations associated with an Award by surrendering Shares to the Company (including Shares that would otherwise be issued pursuant to the Award) that have a Fair Value determined as of the applicable Tax Date equal to the

 

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amount required to be withheld. In the case of Shares previously acquired from the Company that are surrendered under this Section 9, such Shares must have been owned by the Participant for more than six months on the date of surrender (or such longer period of time the Company may in its discretion require).

(d)  Income Taxes and Deferred Compensation . Participants are solely responsible and liable for the satisfaction of all taxes and penalties that may arise in connection with Awards (including any taxes arising under Section 409A of the Code), and the Company shall not have any obligation to indemnify or otherwise hold any Participant harmless from any or all of such taxes. The Committee shall have the discretion to organize any deferral program, to require deferral election forms, and to grant or to unilaterally modify any Award in a manner that (i) conforms with the requirements of Section 409A of the Code, (ii) that voids any Participant election to the extent it would violate Section 409A of the Code, and (iii) for any distribution election that would violate Section 409A of the Code, to make distributions pursuant to the Award at the earliest to occur of a distribution event that is allowable under Section 409A of the Code or any distribution event that is both allowable under Section 409A of the Code and is elected by the Participant, subject to any valid second election to defer, provided that the Committee permits second elections to defer in accordance with Section 409A(a)(4)(C). The Committee shall have the sole discretion to interpret the requirements of the Code, including Section 409A, for purposes of the Plan and all Awards.

10. Non-Transferability of Awards

(a)  General . Except as set forth in this Section 10, or as otherwise approved by the Committee, Awards may not be sold, pledged, assigned, hypothecated, transferred or disposed of in any manner other than by will or by the laws of descent or distribution. The designation of a beneficiary by a Participant will not constitute a transfer (the initial beneficiary designation form is attached as Exhibit “4”). An Award may be exercised, during the lifetime of the holder of an Award, only by such holder, the duly-authorized legal representative of a Participant who is Disabled, or a transferee permitted by this Section 10.

(b)  Limited Transferability Rights . Notwithstanding anything else in this Section 10, the Committee may in its discretion provide in an Award Agreement that an Award in the form of a Non-ISO, or Restricted Shares may be transferred, on such terms and conditions as the Committee deems appropriate, either (i) by instrument to the Participant’s “Immediate Family” (as defined below), or (ii) by instrument to an inter vivos or testamentary trust (or other entity) in which the Award is to be passed to the Participant’s designated beneficiaries. Any transferee of the Participant’s rights shall succeed and be subject to all of the terms of the applicable Award Agreement and the Plan. “ Immediate Family ” means any child, stepchild, grandchild, parent, stepparent, grandparent, spouse, former spouse, sibling, niece, nephew, mother-in-law, father-in-law, son-in-law, daughter-in-law, brother-in-law, or sister-in-law, and shall include adoptive relationships.

11. Adjustments Upon Changes in Capitalization, Merger or Certain Other Transactions

(a) Changes in Capitalization . The Committee shall equitably adjust the number of Shares covered by each outstanding Award, and the number of Shares that have been authorized for issuance under the Plan but as to which no Awards have yet been granted or that have been returned to the Plan upon cancellation, forfeiture, or expiration of an Award, as well as the price per Share covered by each such outstanding Award, to reflect any increase or decrease in the number of

 

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issued Shares resulting from a stock-split, reverse stock-split, stock dividend, combination, recapitalization or reclassification of the Shares, or any other increase or decrease in the number of issued Shares effected without receipt of consideration by the Company. In the event of any such transaction or event, the Committee may provide in substitution for any or all outstanding Awards under the Plan such alternative consideration (including securities of any surviving entity) as it may in good faith determine to be equitable under the circumstances and may require in connection therewith the surrender of all Awards so replaced. In any case, such substitution of securities shall not require the consent of any person who is granted Awards pursuant to the Plan. Except as expressly provided herein, or in an Award Agreement, if the Company issues for consideration shares of stock of any class or securities convertible into shares of stock of any class, the issuance shall not affect, and no adjustment by reason thereof shall be required to be made with respect to the number or price of Shares subject to any Award.

(b)  Dissolution or Liquidation . In the event of the dissolution or liquidation of the Company other than as part of a Change in Control, each Award will terminate immediately prior to the consummation of such action, subject to the ability of the Committee to exercise any discretion authorized in the case of a Change in Control.

(c)  Change in Control . Unless otherwise provided in the applicable Award Agreement, on a Change in Control (i) 50% of the then-outstanding unvested Awards held by each Participant who, as of the Change in Control, has at least one year of Continuous Service shall vest; and (ii) 25% of the then-outstanding unvested Stock Awards held by each Participant who, as of the Change in Control, has less than one year of Continuous Service shall vest. In addition the Committee may in its sole and absolute discretion and authority, without obtaining the approval or consent of the Company’s shareholders or any Participant with respect to his or her outstanding Awards, take one or more of the following actions:

(i) arrange for or otherwise provide that each outstanding Award shall be assumed or a substantially similar award shall be substituted by a successor corporation or a parent or subsidiary of such successor corporation (the “ Successor Corporation ”);

(ii) provide that repurchase rights of the Company with respect to Shares issued upon exercise of an Award shall lapse as to the Shares subject to such repurchase right;

(iii) arrange or otherwise provide for the payment of cash or other consideration to Participants in exchange for the satisfaction and cancellation of outstanding Awards;

(iv) provide that to the extent that an Award is not exercised prior to consummation of a transaction in which the Award is not being assumed or substituted, such Award shall terminate upon such consummation; or

(v) make such other modifications, adjustments or amendments to outstanding Awards or this Plan as the Committee deems necessary or appropriate.

(d) Certain Distributions . In the event of any distribution to the Company’s shareholders of securities of any other entity or other assets (other than dividends payable in cash or stock of the Company) without receipt of consideration by the Company, the Committee may, in its discretion, appropriately adjust the price per Share covered by each outstanding Award to reflect the effect of such distribution.

 

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12. Time of Granting Awards .

The date of grant (“ Grant Date ”) of an Award shall be the date on which the Committee makes the determination granting such Award or such other date as is determined by the Committee, provided that in the case of an ISO, the Grant Date shall be the later of the date on which the Committee makes the determination granting such ISO or the date of commencement of the Participant’s employment relationship with the Company.

13. Modification of Awards and Substitution of Options .

(a)  Modification, Extension, and Renewal of Awards . Within the limitations of the Plan, the Committee may modify an Award to accelerate the rate at which an Option or SAR may be exercised (including without limitation permitting an Option or SAR to be exercised in full without regard to the installment or vesting provisions of the applicable Award Agreement or whether the Option or SAR is at the time exercisable, to the extent it has not previously been exercised), to accelerate the vesting of any Award, to extend or renew outstanding Awards or to accept the cancellation of outstanding Awards to the extent not previously exercised. However, the Committee may not cancel an outstanding Option whose exercise price is greater than Fair Value at the time of cancellation for the purpose of reissuing the Option to the Participant at a lower exercise price or granting a replacement award of a different type. Notwithstanding the foregoing provision, no modification of an outstanding Award shall materially and adversely affect such Participant’s rights thereunder (with such an affect being presumed to arise from a modification that would trigger a violation of Section 409A of the Code), unless either (i) the Participant provides written consent, or (ii) before a Change in Control, the Committee determines in good faith that the modification is not materially adverse to the Participant. Nothing in this Section shall prohibit the Committee from taking any action authorized pursuant to Section 11. Furthermore, neither the Company nor the Committee shall, without shareholder approval, allow for a “repricing” within the meaning of federal securities laws applicable to proxy statement disclosures.

(b)  Substitution of Options . Notwithstanding any inconsistent provisions or limits under the Plan, in the event the Company or an Affiliate acquires (whether by purchase, merger or otherwise) all or substantially all of outstanding capital stock or assets of another corporation or in the event of any reorganization or other transaction qualifying under Section 424 of the Code, the Committee may, in accordance with the provisions of that Section, substitute Options for options under the plan of the acquired company provided (i) the excess of the aggregate fair value of the shares subject to an option immediately after the substitution over the aggregate option price of such shares is not more than the similar excess immediately before such substitution, and (ii) the new option does not give persons additional benefits, including any extension of the exercise period.

14. Term of Plan .

The Plan shall continue in effect for a term of 10 years from its effective date as determined under Section 18 below, unless the Plan is sooner terminated under Section 15 below.

 

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15. Amendment and Termination of the Plan .

(a)  Authority to Amend or Terminate . Subject to Applicable Laws, the Board may from time to time amend, alter, suspend, discontinue, or terminate the Plan.

(b)  Effect of Amendment or Termination . No amendment, suspension, or termination of the Plan shall materially and adversely affect Awards already granted (with such an affect being presumed to arise from a modification that would trigger a violation of Section 409A of the Code) unless either it relates to an adjustment pursuant to Section 11 or modification pursuant to Section 13(a) above, or it is otherwise mutually agreed between the Participant and the Committee, which agreement must be in writing and signed by the Participant and the Company. Notwithstanding the foregoing, the Committee may amend the Plan to eliminate provisions which are no longer necessary as a result of changes in tax or securities laws or regulations, or in the interpretation thereof.

16. Conditions Upon Issuance of Shares .

Notwithstanding any other provision of the Plan or any agreement entered into by the Company pursuant to the Plan, the Company shall not be obligated, and shall have no liability for failure, to issue or deliver any Shares under the Plan unless such issuance or delivery would comply with Applicable Law, with such compliance determined by the Company in consultation with its legal counsel.

17. Reservation of Shares .

The Company, during the term of this Plan, will at all times reserve and keep available such number of Shares as shall be sufficient to satisfy the requirements of the Plan.

18. Effective Date .

This Plan shall become effective on the date which it has received approval by a vote of a majority of the votes cast at a duly held meeting of the Company’s shareholders (or by such other shareholder vote that the Committee determines to be sufficient for the issuance of Shares or stock options according to the Company’s governing documents and applicable state law), which shall occur no later more than 12 months after the date the Plan is adopted by the Company. Awards may be granted under the Plan, but shall not become exercisable, prior to obtaining such shareholder approval.

19. Controlling Law .

All disputes relating to or arising from the Plan shall be governed by the internal substantive laws (and not the laws of conflicts of laws) of the State of Colorado, to the extent not preempted by United States federal law. If any provision of this Plan is held by a court of competent jurisdiction to be invalid and unenforceable, the remaining provisions shall continue to be fully effective.

20. Laws And Regulations .

(a) U.S. Securities Laws . This Plan, the grant of Awards, and the exercise of Options and SARs under this Plan, and the obligation of the Company to sell or deliver any of its securities (including, without limitation, Options, Restricted Shares, Restricted Share Units, Unrestricted Shares, and Shares) under this Plan shall be subject to all Applicable Law. In the event that the

 

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Shares are not registered under the Securities Act of 1933, as amended (the “ Act ”), or any applicable state securities laws prior to the delivery of such Shares, the Company may require, as a condition to the issuance thereof, that the persons to whom Shares are to be issued represent and warrant in writing to the Company that such Shares are being acquired by him or her for investment for his or her own account and not with a view to, for resale in connection with, or with an intent of participating directly or indirectly in, any distribution of such Shares within the meaning of the Act, and a legend to that effect may be placed on the certificates representing the Shares.

(b)  Other Jurisdictions . To facilitate the making of any grant of an Award under this Plan, the Committee may provide for such special terms for Awards to Participants who are foreign nationals or who are employed by the Company or any Affiliate outside of the United States of America as the Committee may consider necessary or appropriate to accommodate differences in local law, tax policy or custom. The Company may adopt rules and procedures relating to the operation and administration of this Plan to accommodate the specific requirements of local laws and procedures of particular countries. Without limiting the foregoing, the Company is specifically authorized to adopt rules and procedures regarding the conversion of local currency, taxes, withholding procedures and handling of stock certificates which vary with the customs and requirements of particular countries. The Company may adopt sub-plans and establish escrow accounts and trusts as may be appropriate or applicable to particular locations and countries.

21. No Shareholder Rights .

Neither a Participant nor any transferee of a Participant shall have any rights as a shareholder of the Company with respect to any Shares underlying any Award until the date of issuance of a share certificate to a Participant or a transferee of a Participant for such Shares in accordance with the Company’s governing instruments and Applicable Law. Prior to the issuance of Shares pursuant to an Award, a Participant shall not have the right to vote or to receive dividends or any other rights as a shareholder with respect to the Shares underlying the Award, notwithstanding its exercise in the case of Options and SARs. No adjustment will be made for a dividend or other right that is determined based on a record date prior to the date the stock certificate is issued, except as otherwise specifically provided for in this Plan.

22. No Employment Rights .

The Plan shall not confer upon any Participant any right to continue an employment, service or consulting relationship with the Company, nor shall it affect in any way a Participant’s right or the Company’s right to terminate the Participant’s employment, service, or consulting relationship at any time, with or without Cause. By accepting any Award under this Plan a Participant confirms his or her at-will status (except as otherwise provided in a written employment agreement signed by an officer of the Company) and that such relationship only can be changed by a written agreement signed by an officer of the Company.

23. Termination, Rescission and Recapture of Awards .

(a) Each Award under the Plan is intended to align the Participant’s long-term interest with those of the Company. If the Participant engages in certain activities discussed below, either during employment or any other service relationship or after employment or such service relationship with the Company terminates for any reason, the Participant is acting contrary to the

 

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long-term interests of the Company. Accordingly, to the extent not prohibited by Applicable Law, the Company may terminate any outstanding, unexercised, unexpired, unpaid, or deferred Awards (“ Termination ”), rescind any exercise, payment or delivery pursuant to the Award (“ Rescission ”), or recapture any Common Stock (whether restricted or unrestricted) or proceeds from the Participant’s sale of Shares issued pursuant to the Award (“ Recapture ”), if the Participant does not comply with the conditions of subsections (b), (c), and (d) hereof (collectively, the “ Conditions ”).

(b) Each Participant acknowledges that by virtue of his or her employment or other service relationship with the Company, he or she will be granted otherwise prohibited access to confidential information and proprietary data including but not limited to such information described in those or other similar terms in any applicable patent, confidentiality, inventions, secrecy, or other agreement between the Participant and the Company, which are not known, and not readily accessible to the Company’s competitors. This information (the “ Confidential Information ”) includes, but is not limited to, current and prospective customers; the identity of key contacts at such customers; customers’ particularized preferences and needs; marketing strategies and plans; financial data; personnel data; compensation data; proprietary procedures and processes; and other unique and specialized practices, programs and plans of the Company and its customers and prospective customers. Each Participant recognizes that this Confidential Information constitutes a valuable property of the Company, developed over a significant period of time and at substantial expense. Accordingly, each Participant, by accepting any Award under this Plan, agrees that he or she shall not, at any time during or after his or her employment or other service relationship with the Company, divulge such Confidential Information or make use of it for his or her own purposes or the purposes of any person or entity other than the Company.

(c) Pursuant to any agreement between the Participant and the Company with regard to intellectual property (including but not limited to patents, trademarks, copyrights, trade secrets, inventions, developments, improvements, proprietary information, confidential business and personnel information), a Participant shall promptly disclose and assign to the Company or its designee all right, title, and interest in such intellectual property, and shall take all reasonable steps necessary to enable the Company to secure all right, title and interest in such intellectual property in the United States and in any foreign country.

(d) By virtue of his or her relationship with the Company, each Participant will be introduced to and involved in the solicitation and servicing of existing customers of the Company and new customers obtained by the Company and agrees that all efforts expended in soliciting and servicing such customers shall be for the permanent benefit of the Company. During each Participant’s employment or other service relationship with the Company he or she will not engage in any conduct which could in any way jeopardize or disturb any of the Company’s customer relationships. Each Participant agrees that, to the extent not prohibited by Applicable Law, for a period beginning on the date of grant of each Award and ending (i) 1 year after termination of Continuous Service, regardless of the reason for such termination, he or she shall not, directly or indirectly, without the prior written consent of the Chairman of the Company, market, offer, sell or otherwise furnish any products or services similar to, or otherwise competitive with, those offered by the Company to any customer of the Company; and (ii) 2 years after termination of Continuous Service, regardless of the reason for such termination, he or she shall not, directly or indirectly, solicit, offer employment to, hire or otherwise retain the services of any employee or other service provider of the Company.

 

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(e) Upon exercise, payment, or delivery of cash or Common Stock pursuant to an Award, the Participant shall certify on a form acceptable to the Company that he or she is in compliance with the terms and conditions of the Plan and, if a severance of Continuous Service has occurred for any reason, shall state the name and address of the Participant’s then-current employer or any entity for which the Participant performs business services and the Participant’s title, and shall identify any organization or business in which the Participant owns a greater-than-five-percent equity interest.

(f) If the Company determines, in its sole and absolute discretion, that (i) a Participant has violated any of the Conditions, or (ii) during his or her Continuous Service has rendered services to or otherwise directly or indirectly engaged in or assisted, any organization or business that, in the judgment of the Company in its sole and absolute discretion, is or is working to become competitive with the Company; or (iii) during his or her Continuous Service, or within one year after its termination for any reason, a Participant (a) has solicited any non-administrative employee of the Company to terminate employment with the Company; or (b) has engaged in activities which are materially prejudicial to or in conflict with the interests of the Company, including any breaches of fiduciary duty or the duty of loyalty, or taken any action or inaction that resulted in a restatement to the Company’s audited financial statements, then, except to the extent prohibited by Applicable Law, the Company may, in its sole and absolute discretion, impose a Termination, Rescission or Recapture with respect to any or all of the Participant’s relevant Awards, Shares, and the proceeds thereof.

(g) Within ten days after receiving notice from the Company of any such activity described in Section 23(f) above, the Participant shall deliver to the Company the Shares acquired pursuant to the Award, or, if Participant has sold the Shares, the gain realized, or payment received as a result of the rescinded exercise, payment, or delivery; provided, that if the Participant returns Shares that the Participant purchased pursuant to the exercise of an Option (or the gains realized from the sale of such Common Stock), the Company shall promptly refund the exercise price, without earnings, that the Participant paid for the Shares. Any payment by the Participant to the Company pursuant to this Section 23 shall be made either in cash or by returning to the Company the number of Shares that the Participant received in connection with the rescinded exercise, payment, or delivery. It shall not be a basis for Termination, Rescission or Recapture if after termination of a Participant’s Continuous Service, the Participant purchases, as an investment or otherwise, stock or other securities of such an organization or business, so long as (i) such stock or other securities are listed upon a recognized securities exchange or traded over-the-counter, and (ii) such investment does not represent more than a five percent equity interest in the organization or business.

(h) Notwithstanding the foregoing provisions of this Section, the Company has sole and absolute discretion not to require Termination, Rescission or Recapture, and its determination not to require Termination, Rescission or Recapture with respect to any particular act by a particular Participant or Award shall not in any way reduce or eliminate the Company’s authority to require Termination, Rescission or Recapture with respect to any other act or Participant or Award. Nothing in this Section shall be construed to impose obligations on the Participant to refrain from engaging in lawful competition with the Company after the termination of employment that does not violate subsections (b), (c), or (d) of this Section, other than any obligations that are part of any separate agreement between the Company and the Participant or that arise under Applicable Law.

 

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(i) All administrative and discretionary authority given to the Company under this Section shall be exercised by the most senior human resources executive of the Company or such other person or committee (including without limitation the Committee) as the Committee may designate from time to time.

(j) Notwithstanding any provision of this Section, if any provision of this Section is determined to be unenforceable or invalid under any Applicable Law, such provision will be applied to the maximum extent permitted by Applicable Law, and shall automatically be deemed amended in a manner consistent with its objectives to the extent necessary to conform to any limitations required under Applicable Law. Furthermore, if any provision of this Section is illegal under any Applicable Law, such provision shall be null and void to the extent necessary to comply with Applicable Law.

24. Pre-IPO Provisions .

Subject to any contrary terms set forth in any Award Agreement, for any period preceding the date of an initial public offering, this Section shall be applicable to any Shares subject to or issued pursuant to Awards. The provisions set forth below shall become null and void upon the occurrence of an initial public offering.

(a) Shareholders’ Agreement . As a condition for the delivery of any Shares pursuant to any Award, the Committee may require the Participant to execute and be bound by any agreement that generally exists between the Company and similarly-situated Shareholders.

(b) Repurchase Rights . Unless provided otherwise in the applicable Award Agreement, after a Participant experiences a termination of Continuous Service, the Company has the right to repurchase some or all of the Participant’s Shares (that were acquired as a result of exercising all or a portion of an Option or SAR) at any time after the lapse of six months and one day from the date such shares were issued. If the Company exercises its repurchase right, it shall pay the Participant the Fair Value of the Shares repurchased as of the date of repurchase. The Company shall pay the repurchase price to the Participant in any combination of cash, a promissory note payable over a time not to exceed five years the terms and conditions of which shall be determined in good faith by the Committee, or by canceling debts the Participant owes to the Company.

(c) Market Stand-Off . In connection with any underwritten public offering by the Company of its equity securities pursuant to an effective registration statement filed under the federal securities laws, including the Company’s initial public offering, Participants shall not directly or indirectly sell, make any short sale of, loan, hypothecate, pledge, offer, grant or sell any option or other contract for the purchase of, purchase any option or other contract for the sale of, or otherwise dispose or transfer, or agree to engage in any of the foregoing transactions with respect to, any Shares acquired under this Agreement without the prior written consent of the Company or its underwriters. Such restriction (the “ Market Stand-Off ”) shall be in effect for such period of time, not exceeding 180 days, following the date of the final prospectus for the offering as may be requested by the Company or such underwriters. The Market Stand-Off shall in any event terminate two years after the date of the Company’s initial public offering. In the event of the declaration of a stock dividend, a spin-off, a stock split, an adjustment in conversion ratio, a recapitalization or a similar transaction affecting the Company’s outstanding securities without receipt of consideration, any new, substituted or additional securities which are by reason of such transaction distributed with

 

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respect to any Shares subject to the Market Stand-Off, or into which such Shares thereby become convertible, shall immediately be subject to such Market Stand-Off. In order to enforce the Market Stand-Off, the Company may impose stop-transfer instructions with respect to the Shares acquired under this Agreement until the end of the applicable stand-off period. The Company and its underwriters shall be beneficiaries of the agreement set forth in this paragraph. This paragraph shall not apply to Shares registered in a public offering under the federal securities laws, and the Participant shall be subject to this paragraph only if the directors and officers of the Company are subject to similar arrangements.

 

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DigitalGlobe, Inc.

Employee Stock Option Plan

 

 

Appendix A: Definitions

 

 

As used in the Plan, the following definitions shall apply:

Affiliate ” means, with respect to any Person (as defined below), any other Person that directly or indirectly controls or is controlled by or under common control with such Person. For the purposes of this definition, “ control ,” when used with respect to any Person, means the possession, direct or indirect, of the power to direct or cause the direction of the management and policies of such Person or the power to elect directors, whether through the ownership of voting securities, by contract or otherwise; and the terms “ Affiliated ,” “ controlling ” and “ controlled ” have meanings correlative to the foregoing.

Applicable Law ” means the legal requirements relating to the administration of options and share-based plans under applicable U.S. federal and state laws, the Code, and any applicable stock exchange or automated quotation system rules or regulations (to the extent the Committee determines in its discretion that compliance with such rules or regulations is desirable) and the applicable laws of any other country or jurisdiction where Awards are granted or that apply to the Company’s or a Participant’s rights and obligations under this Plan or any Award Agreement, as such laws, rules, regulations and requirements shall be in place from time to time.

Award ” means any award made pursuant to the Plan, including awards made in the form of an Option, an SAR, a Restricted Share, a Restricted Share Unit, an Unrestricted Share, or any combination thereof, whether alternative or cumulative, authorized by and granted under this Plan.

Award Agreement ” means any written document setting forth the terms of an Award that has been authorized by the Committee. The Committee shall determine the form or forms of documents to be used, and may change them from time to time for any reason.

Board ” means the Board of Directors of the Company.

Cause ” for termination of a Participant’s Continuous Service will have the meaning set forth in any unexpired employment agreement between the Company and the Participant. 1 In the absence of such an agreement, “Cause” will exist if the Participant is terminated from employment or other service with the Company or an Affiliate for any of the following reasons: (i) the Participant’s willful failure to substantially perform his or her duties and responsibilities to the Company or deliberate violation of a material Company policy; (ii) the Participant’s commission of any material act or acts of fraud, embezzlement, dishonesty, or other willful misconduct; (iii) the Participant’s material unauthorized use or disclosure of any proprietary information or trade secrets of the Company or any other party to whom the Participant owes an obligation of nondisclosure as a result of his or her relationship with the Company; (iv) Participant’s willful and material breach of

 

1  

Confirm this limitation.


any of his or her obligations under any written agreement or covenant with the Company or any of its Affiliates; (v) the Participant’s conviction of, or plea of nolo contendere to a crime involving fraud, theft, or moral turpitude or any felony; or (vi) the Participant’s misconduct, significant failure to perform the Participant’s duties or engagement in any activity that constitutes a conflict of interest with the Company or its Affiliates.

The Committee shall in its discretion determine whether or not a Participant is being terminated for Cause. The Committee’s determination shall, unless arbitrary and capricious, be final and binding on the Participant, the Company, and all other affected persons. The foregoing definition does not in any way limit the Company’s ability to terminate a Participant’s employment or consulting relationship at any time, and the term “ Company ” will be interpreted herein to include any Affiliate or successor thereto, if appropriate.

Change in Control ” means any of the following:

(i) Acquisition of Controlling Interest . Any Person (other than Persons who are Employees at any time more than one year before a transaction) becomes the Beneficial Owner, directly or indirectly, of securities of the Company representing 50% or more of the combined voting power of the Company’s then outstanding securities. In applying the preceding sentence, (i) securities acquired directly from the Company or its Affiliates by or for the Person shall not be taken into account, and (ii) an agreement to vote securities shall be disregarded unless its ultimate purpose is to cause what would otherwise be Change in Control, as reasonably determined by the Board.

(ii) Merger . The Company consummates a merger, or consolidation of the Company with any other corporation unless: (a) the voting securities of the Company outstanding immediately before the merger or consolidation would continue to represent (either by remaining outstanding or by being converted into voting securities of the surviving entity) at least 50% of the combined voting power of the voting securities of the Company or such surviving entity outstanding immediately after such merger or consolidation; and (b) no Person (other than Persons who are Employees at any time more than one year before a transaction) becomes the Beneficial Owner, directly or indirectly, of securities of the Company representing 50% or more of the combined voting power of the Company’s then outstanding securities.

(iii) Sale of Assets . The stockholders of the Company approve an agreement for the sale or disposition by the Company of all, or substantially all, of the Company’s assets.

(iv) Liquidation or Dissolution . The stockholders of the Company approve a plan or proposal for liquidation or dissolution of the Company.

Notwithstanding the foregoing, a “Change in Control” shall not be deemed to have occurred by virtue of the consummation of any transaction or series of integrated transactions immediately following which the record holders of the common stock of the Company immediately prior to such transaction or series of transactions continue to have substantially the same proportionate ownership in an entity which owns all or substantially all of the assets of the Company immediately following such transaction or series of transactions.

 

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Code ” means the U.S. Internal Revenue Code of 1986, as amended.

Committee ” means one or more committees or subcommittees of the Board appointed by the Board to administer the Plan in accordance with Section 4 above. With respect to any decision involving an Award made at a time when the Company is publicly traded and that is intended to satisfy the requirements of Section 162(m) of the Code, the Committee shall consist of two or more Directors of the Company who are “outside directors” within the meaning of Section 162(m) of the Code. With respect to any decision relating to a Reporting Person made at a time when the Company is publicly traded, the Committee shall consist of two or more Directors who are disinterested within the meaning of Rule 16b-3.

Company ” means DigitalGlobe, Inc., a Delaware corporation; provided, however, that in the event the Company reincorporates to another jurisdiction, all references to the term “Company” shall refer to the Company in such new jurisdiction.

Consultant ” means any person, including an advisor, who is engaged by the Company or any Affiliate to render services and is compensated for such services.

Continuous Service ” means the absence of any interruption or termination of service as an Employee, Director, or Consultant. Continuous Service shall not be considered interrupted in the case of: (i) sick leave; (ii) military leave; (iii) any other leave of absence approved by the Committee, provided that such leave is for a period of not more than 90 days, unless reemployment upon the expiration of such leave is guaranteed by contract or statute, or unless provided otherwise pursuant to Company policy adopted from time to time; or (iv) in the case of transfers between locations of the Company or between the Company, its Affiliates or their respective successors. Changes in status between service as an Employee, Director, and a Consultant will constitute an interruption of Continuous Service if the Committee determines that the individual has not continued or will not continue to perform bona fide services for the Company or determines that the relationship will or may result in adverse accounting consequences.

Director ” means a member of the Board, or a member of the board of directors of an Affiliate.

Disabled ” means that a Participant is contemporaneously receiving full disability benefits under a long-term disability plan maintained by the Company (but, if a Participant is awarded disability benefits as the result of such a disability plan’s formal claims procedure process, prior to denial at the final level of administrative appeal, he or she shall be deemed to have contemporaneously received such benefits with respect to the period for which they were awarded). If a Participant is denied such benefits at the final level of appeal, or does not timely pursue his or her disability plan administrative remedies through the final level of appeal, he or she shall not be considered to be Disabled for purposes of the Plan.

Eligible Person ” means any Consultant, Director or Employee and includes non-Employees to whom an offer of employment has been or is being extended.

Employee ” means any person whom the Company or any Affiliate classifies as an employee (including an officer) for employment tax purposes, whether or not that classification is correct. The payment by the Company of a director’s fee to a Director shall not be sufficient to constitute “employment” of such Director by the Company.

 

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Exchange Act ” means the Securities Exchange Act of 1934, as amended.

Fair Value ” means, as of any date (the “ Determination Date ”) means: (i) the closing price of a Share on the New York Stock Exchange or the American Stock Exchange (collectively, the “ Exchange ”), on the Determination Date, or, if shares were not traded on the Determination Date, then on the nearest preceding trading day during which a sale occurred; or (ii) if such stock is not traded on the Exchange but is quoted on Nasdaq or a successor quotation system, (A) the last sales price (if the stock is then listed as a National Market Issue under The Nasdaq National Market System) or (B) the mean between the closing representative bid and asked prices (in all other cases) for the stock on the Determination Date as reported by Nasdaq or such successor quotation system; or (iii) if such stock is not traded on the Exchange or quoted on Nasdaq but is otherwise traded in the over-the-counter, the mean between the representative bid and asked prices on the Determination Date; or (iv) if subsections (i)-(iii) do not apply, the fair value established in good faith by the Board or the Committee.

Grant Date ” has the meaning set forth in Section 12 of the Plan.

Incentive Share Option or ISO ” means an Option intended to qualify as an incentive stock option within the meaning of Section 422 of the Code, as designated in the applicable Award Agreement.

Non-ISO ” means an Option not intended to qualify as an ISO, as designated in the applicable Award Agreement.

Option ” means any stock option granted pursuant to Section 6 of the Plan.

Participant ” means any holder of one or more Awards, or the Shares issuable or issued upon exercise of such Awards, under the Plan.

Person ” means any natural person, association, trust, business trust, cooperative, corporation, general partnership, joint venture, joint-stock company, limited partnership, limited liability company, real estate investment trust, regulatory body, governmental agency or instrumentality, unincorporated organization or organizational entity.

Plan ” means this DigitalGlobe, Inc. 2007 Employee Stock Option Plan.

Reporting Person ” means an officer, Director, or greater than ten percent shareholder of the Company within the meaning of Rule 16a-2 under the Exchange Act, who is required to file reports pursuant to Rule 16a-3 under the Exchange Act.

Restricted Shares ” mean Shares subject to restrictions imposed pursuant to Section 8 of the Plan.

Restricted Share Units ” mean Awards pursuant to Section 8 of the Plan.

 

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Rule 16b-3 ” means Rule 16b-3 promulgated under the Exchange Act, as amended from time to time, or any successor provision.

SAR” or “Share Appreciation Right” means Awards granted pursuant to Section 7 of the Plan.

Share ” means a share of common stock of the Company, as adjusted in accordance with Section 11 of the Plan.

Ten Percent Holder ” means a person who owns stock representing more than ten percent (10%) of the combined voting power of all classes of stock of the Company or any Affiliate.

Unrestricted Shares ” mean Shares awarded pursuant to Section 8 of the Plan.

 

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Exhibit 1

DIGITALGLOBE, INC.

2007 EMPLOYEE STOCK PLAN

 

 

Stock Option Award Agreement

 

 

Award No.             

You are hereby awarded the following stock option (the “ Option ”) to purchase Shares of DigitalGlobe, Inc. (the “ Company ”), subject to the terms and conditions set forth in this Stock Option Award Agreement (the “ Award Agreement ”) and in the DigitalGlobe, Inc. 2007 Employee Stock Option Plan (the “ Plan ”), which is attached hereto as Appendix 1. You should carefully review these documents, and consult with your personal financial advisor, before exercising this Option.

By executing this Award Agreement, you agree to be bound by all of the Plan’s terms and conditions as if they had been set out verbatim below. In addition, you recognize and agree that all determinations, interpretations, or other actions respecting the Plan and this Award Agreement will be made by the Company’s Board of Directors or any Committee appointed by the Board to administer the Plan, and shall (in the absence of material and manifest bad faith or fraud) be final, conclusive and binding on all parties, including you and your successors in interest. Terms that begin with initial capital letters have the special meanings set forth in the Plan or in this Award Agreement (unless the context indicates otherwise).

1. Specific Terms . This Option shall have, and be interpreted according to, the following terms, subject to the provisions of the Plan in all instances:

 

Your Name:   

 

  
Type of Stock Option:    ¨    Incentive Stock Option (ISO) 1   
   ¨    Non-Incentive Stock Option   
Number of Shares subject to Option:   

 

  
Option Exercise Price per Share:   

 

  
Grant Date:   

 

  

 

Vesting Schedule:

   (Establishes your rights to exercise this Option with respect to the Number of Shares stated above, subject to any shareholder approval requirement set forth in the Plan.)

 

1  

If you directly or indirectly own more than 10% of the voting power of all classes of stock of the Company or of any Subsidiary, then the term of your ISO cannot exceed 5 years and the exercise price must be at least 110% of the Fair Value (100% for any other employee who is receiving ISO awards). Only employees may receive ISOs.


 

   25% on the first anniversary of the Grant Date (subject to your Continuous Service through such date) and 1/36th of the remaining 75% thereafter on each of the first 36 monthly anniversaries of the Grant Date (subject to your Continuous Service through each such date).
Expiration Date:    ¨                years after Grant Date; or   
   ¨    10 years after Grant Date.   

2. Term of Option . The term of the Option will expire at 5:00 p.m. (M.D.T. or M.S.T., as applicable) on the Expiration Date.

3. Manner of Exercise . The Option shall be exercised in the manner set forth in the Plan, using the exercise form required by the Committee. The amount of Shares for which the Option may be exercised is cumulative; that is, if you fail to exercise the Option for all of the Shares vested under the Option during any period set forth above, then any Shares subject to the Option that are not exercised during such period may be exercised during any subsequent period, until the expiration or termination of the Option pursuant to Sections 2 and 5 of this Award Agreement and the terms of the Plan. Fractional Shares may not be purchased.

4. Special ISO Provisions . If designated as an ISO, this Option shall be treated as an ISO to the extent allowable under Section 422 of the Code, and shall otherwise be treated as a Non-ISO. If you sell or otherwise dispose of Shares acquired upon the exercise of an ISO within 1 year from the date such Shares were acquired or 2 years from the Grant Date, you agree to deliver a written report to the Company within 10 days following the sale or other disposition of such Shares detailing the net proceeds of such sale or disposition.

5. Termination of Continuous Service . If your Continuous Service with the Company is terminated for any reason, this Option shall terminate on the date on which you cease to have any right to exercise the Option pursuant to the terms and conditions set forth in Section 6 of the Plan.

6. Designation of Beneficiary . Notwithstanding anything to the contrary contained herein or in the Plan, following the execution of this Award Agreement, you may expressly designate a beneficiary (the “ Beneficiary ”) to your interest in the Option awarded hereby. You shall designate the Beneficiary by completing and executing a designation of beneficiary agreement in the form required by the Committee (the “ Designation of Beneficiary ”) and delivering an executed copy of the Designation of Beneficiary to the Company’s HR Manager or such other person designated by the Company in writing.

7. Restrictions on Transfer of Awards; Right of Repurchase . This Award Agreement may not be sold, pledged, or otherwise transferred without the prior written consent of the Committee. If the Committee permits any such transfer, any transferee shall succeed and be subject to all of the terms of this Award Agreement and the Plan. If you experience a termination of Continuous Service, the Company has the right to repurchase some or all of your Shares (that were acquired as a result of exercising all or a portion of your option) at any time after the lapse of six months and one day from the date such shares were issued. If the Company exercises its repurchase right, it shall pay you the Fair Value of the Shares repurchased as of the date of repurchase. The Company shall pay

 

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the repurchase price to you in any combination of cash, a promissory note payable over a time not to exceed five years, or by canceling debts you owe to the Company. The Company’s repurchase rights as set forth in this Section 7 shall lapse on the effective date of an initial public offering.

8. Conditions on Issuance of Shares; Transfer Restrictions . Notwithstanding any other provision of the Plan or of this Award Agreement: (i) the Committee may condition your receipt of Shares on your execution of a shareholder agreement imposing terms generally applicable to other similarly-situated employee-shareholders; and (ii) unless authorized by the Committee in writing, any Shares issued pursuant to this Award Agreement shall be non-transferable except in accordance with Section 7 above.

9. Taxes . By signing this Award Agreement, you acknowledge that you shall be solely responsible for the satisfaction of any taxes that may arise (including taxes arising under Sections 409A or 4999 of the Code), and that neither the Company nor the Committee shall have any obligation whatsoever to pay such taxes. In the event that any payment or benefit received or to be received by Participant pursuant to the Plan or otherwise (collectively, the “ Payments ”) would result in a “parachute payment” as described in section 280G of the Internal Revenue Code of 1986, as amended (or any successor provision), notwithstanding the other provisions of this Award Agreement, the Plan, or any other agreement or arrangement (but subject to any contrary provisions of any separate unexpired employment or other agreement between you and the Company), such Payments shall not, in the aggregate, exceed the maximum amount that may be paid to you without triggering golden parachute penalties under Section 280G and related provisions of the Internal Revenue Code, as determined in good faith by the Company’s independent auditors. If any benefits must be cut back to avoid triggering such penalties, they shall be cut back in the priority order designated by the Company. If an amount in excess of the limit set forth in this section is paid to you, you shall repay the excess amount to the Company on demand, with interest at the rate provided for in Internal Revenue Code Section 1274(b)(2)(B) (or any successor provision). The Company and you agree to cooperate with each other in connection with any administrative or judicial proceedings concerning the existence or amount of golden parachute penalties. The foregoing reduction, however, shall only apply if it increases the net amount you would realize from Payments, after payment of income and excise taxes on such Payments.

10. Notices . Any notice or communication required or permitted by any provision of this Award Agreement to be given to you generally shall be in writing and generally shall be delivered electronically, personally, or by certified mail, return receipt requested, addressed to you at the last address that the Company had for you on its records. Any notice or communication required or permitted by any provision of this Award Agreement to be given by you must be in writing and delivered personally or by certified mail, return receipt requested, addressed to the Company’s HR Manager at its corporate headquarters. Each party may, from time to time, by notice to the other party hereto, specify a new e-mail or address for delivery of notices relating to this Award Agreement. Any such notice shall be deemed to be given as of the date such notice is personally delivered or properly mailed.

11. Binding Effect . Except as otherwise provided in this Award Agreement or in the Plan, every covenant, term, and provision of this Award Agreement shall be binding upon and inure to the benefit of the parties hereto and their respective heirs, legatees, legal representatives, successors, transferees, and assigns.

 

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12. Modifications . This Award Agreement may be modified or amended at any time, in accordance with Section 13 of the Plan and provided that you must consent in writing to any modification that adversely and materially affects your rights or obligations under this Award Agreement (with such an affect being presumed to arise from a modification that would trigger a violation of Section 409A of the Code). Notwithstanding the foregoing, the Committee may, however, take the action permitted by Section 11 of the Plan without your written consent.

13. Headings . Section and other headings contained in this Award Agreement are for reference purposes only and are not intended to describe, interpret, define or limit the scope or intent of this Award Agreement or any provision hereof.

14. Severability . Every provision of this Award Agreement and of the Plan is intended to be severable. If any term hereof is illegal or invalid for any reason, such illegality or invalidity shall not affect the validity or legality of the remaining terms of this Award Agreement.

15. Counterparts . This Award Agreement may be executed by the parties hereto in separate counterparts, each of which when so executed and delivered shall be an original, but all such counterparts shall together constitute one and the same instrument.

16. Plan Governs . By signing this Award Agreement, you acknowledge that you have received a copy of the Plan and that your Award Agreement is subject to all the provisions contained in the Plan, the provisions of which are made a part of this Award Agreement and your Award is subject to all interpretations, amendments, rules and regulations which from time to time may be promulgated and adopted pursuant to the Plan. In the event of a conflict between the provisions of this Award Agreement and those of the Plan, the provisions of the Plan shall control.

17. Investment Purposes . By executing this Award Agreement, you represent and warrant that any Shares issued to you pursuant to your Options will be held for investment purposes only for your own account, and not with a view to, for resale in connection with, or with an intent in participating directly or indirectly in, any distribution of such Shares within the meaning of the Securities Act of 1933, as amended.

18. Not a Contract of Employment . By executing this Award Agreement you acknowledge and agree that (i) any person who is terminated before full vesting of an award, such as the one granted to you by this Award Agreement, could claim that he or she was terminated to preclude vesting; (ii) you promise never to make such a claim; (iii) nothing in this Award Agreement or the Plan confers on you any right to continue an employment, service or consulting relationship with the Company, nor shall it affect in any way your right or the Company’s right to terminate your employment, service, or consulting relationship at any time, with or without Cause; (iv) unless you have a written agreement signed by the Company’s President providing otherwise, you are an at-will employee who may be terminated at any time and for any or no reason; and (v) the Company would not have granted this Award to you but for these Acknowledgments and agreements.

19. Long-term Consideration for Award . By executing this Award Agreement you acknowledge the terms and conditions set forth in Section 23 of the Plan and that such terms are hereby incorporated by reference and made an integral part of this Award Agreement. An invalidation of all or part of Section 23 of the Plan, or your commencement of litigation to invalidate, modify, or alter the terms and conditions set forth in this Section 19 of this Award Agreement or Section 23 of

 

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the Plan, shall cause this Award to become null, void, and unenforceable. You further acknowledge and agree that the terms and conditions of this Section and Section 23 of the Plan shall survive both (i) the termination of your Continuous Service for any reason, and (ii) the termination of the Plan, for any reason. You acknowledge and agree that the grant of Options in this Award Agreement is just and adequate consideration for the survival of the restrictions set forth herein, and that the Company may pursue any or all of the following remedies if you either violate the terms of this Section or Section 23 of the Plan or succeed for any reason in invalidating any part of it (it being understood that the invalidity of any term hereof would result in a failure of consideration for the Award):

 

  (i) declaration that the Award is null and void and of no further force or effect;

 

  (ii) recapture of any cash paid or Shares issued to you, or any designee or beneficiary of you, pursuant to the Award;

 

  (iii) recapture of the proceeds, plus reasonable interest, with respect to any Shares that are both issued pursuant to this Award and sold or otherwise disposed of by you, or any designee or beneficiary of you.

The remedies provided above are not intended to be exclusive, and the Company may seek such other remedies as are provided by law, including equitable relief. You acknowledge and agree that your adherence to the foregoing requirements will not prevent you from engaging in your chosen occupation and earning a satisfactory livelihood following the termination of your employment with the Company

20. Governing Law . The laws of the State of Colorado shall govern the validity of this Award Agreement, the construction of its terms, and the interpretation of the rights and duties of the parties hereto.

 

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BY YOUR SIGNATURE BELOW, along with the signature of the Company’s representative, you and the Company agree that the Option is awarded under and governed by the terms and conditions of this Award Agreement and the Plan.

 

DIGITALGLOBE, INC.
By:  

 

  Name:
  Title:
PARTICIPANT
The undersigned Participant hereby accepts the terms of this Award Agreement and the Plan.
By:  

 

Name of Participant:  

 

 

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Exhibit 2

EARTHWATCH INCORPORATED 1999 EQUITY INCENTIVE PLAN


Exhibit 3

DIGITALGLOBE, INC.

2007 EMPLOYEE STOCK OPTION PLAN

 

 

Form of Exercise of Stock Option Award Agreement

 

 

 

   DigitalGlobe, Inc.
Attention:   

 

  

 

Dear Sir or Madam:

The undersigned elects to exercise his/her Incentive Stock Option to purchase              shares of Common Stock of DigitalGlobe, Inc. (the “ Company ”) under and pursuant to a Stock Option Agreement dated as of             .

Delivered herewith is a certified or bank cashier’s or teller’s check in the amount of $        .

The name or names to be on the stock certificate or certificates and the address and Social Security Number(s) of such person(s) is as follows:

 

Name:  

 

Address:  

 

Social Security Number  

 

 

    Very truly yours,

 

   

 

Date     Optionee

 

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Exhibit 4

DIGITALGLOBE, INC.

2007 EMPLOYEE STOCK OPTION PLAN

 

 

Designation of Beneficiary

 

 

In connection with the Awards designated below that I have received pursuant to the Plan, I hereby designate the person specified below as the beneficiary upon my death of my interest in Awards as defined in the Company’s 2007 Employee Stock Option Plan (the “ Plan ”). This designation shall remain in effect until revoked in writing by me.

 

  Name of Beneficiary:    

 

 
  Address:    

 

 
     

 

 
     

 

 
  Social Security No.:    

 

 

This beneficiary designation relates to any and all of my rights under the following Award or Awards:

 

  ¨ any Award that I have received or ever receive under the Plan.

 

  ¨ the                      Award that I received pursuant to an award agreement dated                  ,          between myself and the Company.

I understand that this designation operates to entitle the above-named beneficiary, in the event of my death, to any and all of my rights under the Award(s) designated above from the date this form is delivered to the Company until such date as this designation is revoked in writing by me, including by delivery to the Company of a written designation of beneficiary executed by me on a later date.

 

Date:  

 

By:  

 

  Name of Participant

Sworn to before me this

     day of             , 200    

 

Notary Public
County of  

 

State of  

 


Exhibit 2

(This form is needed only when designating a non-spouse as a beneficiary)

 

( State of                           

   )   

(                                         

   ) ss.   

( County of                         

   )   

SPOUSE’S CONSENT

TO

BENEFICIARY DESIGNATION

                     (Name of Spouse), being duly sworn, deposes and says:

As the spouse of                      (Name of Participant) — I have read the Designation of Beneficiary form attached to this affidavit and completed by my spouse. I understand that:

1. My spouse has named an entity or a person other than me to receive benefits under the DigitalGlobe, Inc. 2007 Employee Stock Option Plan. This benefit may consist of community property in which I have an interest.

2. The designation of a beneficiary other than me will cause some or all of any benefits available on my spouse’s death to be provided to the named beneficiary rather than to me.

3. If I do not voluntarily consent to my spouse’s beneficiary designation, the designation may be invalid and I may receive the Plan benefits that may be available on my spouse’s death.

I hereby voluntarily consent to and join in the beneficiary selections made by my spouse by means of the attached form. This affidavit of consent applies only to the attached form. As long as my spouse allows this form to remain in force, I hereby waive any and all claim to benefits that I may have under applicable law solely because of my status as the spouse of an employee. Prior to my spouse’s death, I retain the right to revoke this consent at any time by delivering a written revocation notice to the Company’s Human Resources Manager. Upon my spouse’s death, my consent shall become irrevocable.

 

 

Signature of Spouse

Sworn to before me this

     day of                  , 200    

 

Notary Public
County of  

 

State of  

 


On March 6, 2008, the Board of Directors of DigitalGlobe, Inc. amended Section 6(h)(i) of the 2007 Employee Stock Option Plan to provide as follows:

“(i) Termination other than Upon Disability or Death or for Cause . In the event of termination of a Participant’s Continuous Service (other than as a result of Participant’s death, disability, or termination for Cause), the Participant shall have the right to exercise an Option at any time within three months following such termination (or such earlier date on which the Option expires) to the extent the Participant was entitled to exercise such Option at the date of such termination.”

Exhibit 21.1

LIST OF SUBSIDIARIES OF DIGITALGLOBE, INC.

As of December 31, 2011

 

Legal Entity  

State or

Country of

Incorporation

 

%

Ownership

 

Name Doing

Business As

DG Consents Sub, Inc.

  Delaware   100%   DG Consents Sub, Inc.

DigitalGlobe International, Inc.

  Colorado   100%   DigitalGlobe International, Inc.

DigitalGlobe China Ventures LLC

  Colorado   100%   DigitalGlobe China Ventures LLC

Exhibit 23.1

CONSENT OF INDEPENDENT REGISTERED PUBLIC ACCOUNTING FIRM

We hereby consent to the incorporation by reference in the Registration Statements on Form S-3 (No. 333-169354) and Form S-8 (No. 333-159373) of DigitalGlobe, Inc. of our report dated February 29, 2012 relating to the financial statements and the effectiveness of internal control over financial reporting, which appears in this Form 10-K.

/s/    PricewaterhouseCoopers LLP

Denver, Colorado

February 29, 2012

Exhibit 31.1

CERTIFICATION OF CHIEF EXECUTIVE OFFICER

Section 302 Certification

I, Jeffrey R. Tarr, certify that:

 

  1) I have reviewed this Annual Report on Form 10-K for the year ended December 31, 2011 of DigitalGlobe, Inc.;

 

  2) Based on my knowledge, this report does not contain any untrue statement of a material fact or omit to state a material fact necessary to make the statements made, in light of the circumstances under which such statements were made, not misleading with respect to the period covered by this report;

 

  3) Based on my knowledge, the financial statements, and other financial information included in this report, fairly present in all material respects the financial condition, results of operations and cash flows of the registrant as of, and for, the periods presented in this report;

 

  4) The registrant’s other certifying officer(s) and I are responsible for establishing and maintaining disclosure controls and procedures (as defined in Exchange Act Rules 13a-15(e) and 15d-15(e)) and internal control over financial reporting (as defined in Exchange Act Rules 13a-15(f) and 15d-15(f)) for the registrant and have:

 

  a) Designed such disclosure controls and procedures, or caused such disclosure controls and procedures to be designed under our supervision, to ensure that material information relating to the registrant, including its consolidated subsidiaries, is made known to us by others within those entities, particularly during the period in which this report is being prepared;

 

  b) Designed such internal control over financial reporting, or caused such internal control over financial reporting to be designed under our supervision, to provide reasonable assurance regarding the reliability of financial reporting and the preparation of financial statements for external purposes in accordance with generally accepted accounting principles;

 

  c) Evaluated the effectiveness of the registrant’s disclosure controls and procedures and presented in this report our conclusions about the effectiveness of the disclosure controls and procedures, as of the end of the period covered by this report based on such evaluation; and

 

  d) Disclosed in this report any change in the registrant’s internal control over financial reporting that occurred during the registrant’s most recent fiscal quarter (the registrant’s fourth fiscal quarter in the case of an annual report) that has materially affected, or is reasonably likely to materially affect, the registrant’s internal control over financial reporting; and

 

  5) The registrant’s other certifying officer(s) and I have disclosed, based on our most recent evaluation of internal control over financial reporting, to the registrant’s auditors and the audit committee of the registrant’s board of directors (or persons performing the equivalent functions):

 

  a) All significant deficiencies and material weaknesses in the design or operation of internal control over financial reporting which are reasonably likely to adversely affect the registrant’s ability to record, process, summarize and report financial information; and

 

  b) Any fraud, whether or not material, that involves management or other employees who have a significant role in the registrant’s internal control over financial reporting.

Date: February 29, 2012

 

/s/    Jeffrey R. Tarr

Jeffrey R. Tarr

Chief Executive Officer & President

Exhibit 31.2

CERTIFICATION OF CHIEF FINANCIAL OFFICER

Section 302 Certification

I, Yancey L. Spruill, certify that:

 

  1) I have reviewed this Annual Report on Form 10-K for the year ended December 31, 2011 of DigitalGlobe, Inc.;

 

  2) Based on my knowledge, this report does not contain any untrue statement of a material fact or omit to state a material fact necessary to make the statements made, in light of the circumstances under which such statements were made, not misleading with respect to the period covered by this report;

 

  3) Based on my knowledge, the financial statements, and other financial information included in this report, fairly present in all material respects the financial condition, results of operations and cash flows of the registrant as of, and for, the periods presented in this report;

 

  4) The registrant’s other certifying officer(s) and I are responsible for establishing and maintaining disclosure controls and procedures (as defined in Exchange Act Rules 13a-15(e) and 15d-15(e)) and internal control over financial reporting (as defined in Exchange Act Rules 13a-15(f) and 15d-15(f)) for the registrant and have:

 

  a) Designed such disclosure controls and procedures, or caused such disclosure controls and procedures to be designed under our supervision, to ensure that material information relating to the registrant, including its consolidated subsidiaries, is made known to us by others within those entities, particularly during the period in which this report is being prepared;

 

  b) Designed such internal control over financial reporting, or caused such internal control over financial reporting to be designed under our supervision, to provide reasonable assurance regarding the reliability of financial reporting and the preparation of financial statements for external purposes in accordance with generally accepted accounting principles;

 

  c) Evaluated the effectiveness of the registrant’s disclosure controls and procedures and presented in this report our conclusions about the effectiveness of the disclosure controls and procedures, as of the end of the period covered by this report based on such evaluation; and

 

  d) Disclosed in this report any change in the registrant’s internal control over financial reporting that occurred during the registrant’s most recent fiscal quarter (the registrant’s fourth fiscal quarter in the case of an annual report) that has materially affected, or is reasonably likely to materially affect, the registrant’s internal control over financial reporting; and

 

  5) The registrant’s other certifying officer(s) and I have disclosed, based on our most recent evaluation of internal control over financial reporting, to the registrant’s auditors and the audit committee of the registrant’s board of directors (or persons performing the equivalent functions):

 

  a) All significant deficiencies and material weaknesses in the design or operation of internal control over financial reporting which are reasonably likely to adversely affect the registrant’s ability to record, process, summarize and report financial information; and

 

  b) Any fraud, whether or not material, that involves management or other employees who have a significant role in the registrant’s internal control over financial reporting.

Date: February 29, 2012

 

/s/    Yancey L. Spruill

Yancey L. Spruill

Executive Vice President, Chief Financial Officer and Treasurer

Exhibit 32.1

CERTIFICATION OF CHIEF EXECUTIVE OFFICER

Section 906 Certification

Pursuant to 18 U.S.C. Section 1350, the undersigned officer of DigitalGlobe, Inc. (the “Company”) hereby certifies that:

 

  1) the Annual Report on Form 10-K for the year ended December 31, 2011 which this statement accompanies fully complies with the requirements of Section 13(a) or 15(d) of the Securities Exchange Act of 1934, and

 

  2) the information contained in the Annual Report on Form 10-K for the year ended December 31, 2011 fairly presents, in all material respects, the financial condition and results of operations of DigitalGlobe, Inc.

Date: February 29, 2012

 

/s/    Jeffrey R. Tarr

Jeffrey R. Tarr

Chief Executive Officer and President

A signed original of this certification has been provided to DigitalGlobe, Inc. and will be retained by DigitalGlobe, Inc. and furnished to the Securities and Exchange Commission upon request.

Exhibit 32.2

CERTIFICATION OF CHIEF FINANCIAL OFFICER

Section 906 Certification

Pursuant to 18 U.S.C. Section 1350, the undersigned officer of DigitalGlobe, Inc. (the “Company”) hereby certifies that:

 

  1) the Annual Report on Form 10-K for the year ended December 31, 2011 which this statement accompanies fully complies with the requirements of Section 13(a) or 15(d) of the Securities Exchange Act of 1934, and

 

  2) the information contained in the Annual Report on Form 10-K for the year ended December 31, 2011 fairly presents, in all material respects, the financial condition and results of operations of DigitalGlobe, Inc.

Date: February 29, 2012

 

/s/ Yancey L. Spruill

Yancey L. Spruill

Executive Vice President , Chief Financial Officer and Treasurer

 

A signed original of this certification has been provided to DigitalGlobe, Inc. and will be retained by DigitalGlobe, Inc. and furnished to the Securities and Exchange Commission upon request.