Document:

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 Exhibit 10.5.5 

Amendment No. 7 
 To the 
 WorldView3 Satellite Purchase Agreement 

#60150 
 This
Amendment No.7 (“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 Digital Globe or BATC, as appropriate, and “Patties” means DigitalGlobe and BATC. 

WHEREAS, DigitalGlobe and BATC entered into the WorldView3 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 018: Documentation Updates 

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

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

  

	 	a.	Exhibit 2 to the Agreement, titled “DigitalGlobe WorldView 3 Satellite Specification - 10329655, Rev 9.0,” and dated 19 December 201I, is replaced in its
entirety by the updated version “WorldView-3 Satellite Specification – 10329655, Rev 11.0”, dated 18 Oct 2012, included as Attachment 1 to this Amendment; and 

 

	 	b.	Exhibit 3 to the Agreement, titled ·“WorldView 3 Payment Milestone Schedule-10329669, Rev 5.0” and dated 14 December 2011, is replaced in its
entirety by the updated version “WorldView 3 Payment Milestone Schedule- 10329669, Rev 6.0,” dated 1 Oct 2012, included as Attachment 2 to this Amendment; and 

 

	 	c.	“WorldView-3 CAVIS-ACI Specification - 10385893, Rev 3.0”, and dated 22 November 2011, is replaced in its entirety by the updated version
“WorldView-3 CAVIS-ACI Specification - 10385893 Rev 4.0”, and dated 22 May, 2012, included as Attachment 3 to the Amendment) 

  

	 	d.	“WorldView-3 Spacecraft Simulator Specification- 10258368, Rev 4.0”, and dated 12 December 2011, is replaced in its entirety by the document
“WorldView-3 .Spacecraft Simulator Specification – 10258368, Rev 5.0”, dated 1 October 2012, included as Attachment 4 to this Amendment. 

  

  

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

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 2. ECP 019: Satellite Control Processor (SCP) Holding Buffer Re-size. 

This change directs BATC to change the size of the holding buffer on the SCP from [**Redacted**]. Full details are listed in the
BATC FFP letter dated 14 September 2012 (COS.12.JRS.026). 
 Price: The Firm-Fixed Price for the holding buffer change is
$65,000. 
 3. ECP 020: Bus Accommodation for Additional AUX Heater Circuit. 

This change directs BATC to make hardware and software modifications to support accommodation of an additional heater circuit for the AUX
payload. Full details may be found in the BATC FFP letter dated 3 Aug 2012 (COS.12.JRS.021), and in the DigitalGlobe RFP letter dated 12 July 2012. 
 Price: The Firm-Fixed Price for the Flight Software changes is $135,000. 

SUMMARY 

The value for these ECPs is $200,000, outlined in the following table: 

 

							
	 Change #
	  	Change Description	  	$	 
	 018
	  	Documentation Updates	  	$	0.00	  
	 019
	  	[**Redacted**]	  	 	[**Redacted**]	  
	 020
	  	[**Redacted**]	  	 	[**Redacted**]	  
		  	TOTAL	  	$	200,000.00	  

 Contract Value Summary 

 

					
	 Previous Contract Value
	  	$	217,562,399.00	  
	 ECPs
	  	$	200,000.00	  
	 New Contract Value
	  	$	217,762,399.00	  

 Unless otherwise expressly provided herein, all other terms and conditions of the Agreement shall remain
in full force and effect. 
 This Amendment No. 7 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 & Technology Corp.	 		 	DigitalGlobe, Inc.
			
	 [**Redacted**]
	 		 	 [**Redacted**]

	Signature	 		 	Signature
			
	 [**Redacted**]
	 		 	 [**Redacted**]

  

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	Name	 		 	Name
			
	 [**Redacted**]
	 		 	 [**Redacted**]

			
	 [**Redacted**]
	 		 	 [**Redacted**]

  

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 Exhibit 2 to Contract 60150 

WorldView-3 Satellite 
 Specification 
  

											
		 		 		 		 	Document #	  	10329655
		 		 		 		 	 Revision #
	  	11.0
		 		 		 		 	Release Date	  	18 Oct 2012
		 		 		 		 	Prepared by	  	George Hunyadi
		 		 		 		 	Approved by	  	Keith Constantinides

 [**Redacted**] 
 RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION 
 This document contains information proprietary and confidential to
DigitalGlobeTM, 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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 Change Record 

 

							
	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

	1.0	  	20 Aug 2010	  	All	  	Initial Release
	2.0	  	1 Oct 2010	  	Various	  	Corrected minor grammatical errors.
		  		  	1.2	  	Reference instrument changes. (Details in the ICD and elsewhere in this specification).
		  		  	 2.1.1,
 3.3.5
	  	Updated Range Safety document reference
		  		  	2.3	  	Added [**Redacted**]
		  		  	 Table 3-1,
 3.1.3.1.3.4,
 3.1.3.1.3.6
	  	Updated [**Redacted**]
		  		  	3.1.3.1.4	  	Item (b) generalized for the [**Redacted**]
		  		  	3.2.1.1.2.3	  	Changed item (e) [**Redacted**]
		  		  	 3.2.1.5.2.1,
 Fig. 3-6
	  	Updated [**Redacted**]
		  		  	3.2.1.5.5.2	  	Item (c) [**Redacted**]
		  		  	3.2.1.6.1.1	  	Updated [**Redacted**]
		  		  	3.2.1.6.1.2	  	Updated [**Redacted**]
		  		  	3.2.1.7.4.2.1	  	Increased time allowed to [**Redacted**]
		  		  	3.2.1.7.5.2.6	  	Deleted [**Redacted**]
		  		  	3.2.1.7.6.1.11	  	[**Redacted**]
		  		  	3.2.1.7.6.2.7	  	Item (c) edited for accuracy; item (k) corrected to include the completion of the last sentence, which was missing.
		  		  	3.2.1.7.6.2.8	  	Item (a) edited for accuracy
		  		  	3.2.1.7.6.2.12	  	Edited rationale for accuracy

  

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	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

		  		  	3.2.1.7.8.3	  	Generalized item (a) to be consistent with 3.2.1.5.2 and 3.2.3.4.1.
		  		  	3.2.1.7.9.3.3	  	Generalized item (c) to be consistent with 3.2.1.5.2 and 3.2.3.4.1.
		  		  	3.2.1.7.10.3	  	Generalized item (a) to be consistent with 3.2.1.5.2 and 3.2.3.4.1.
		  		  	3.2.1.7.11.4.8	  	Added [**Redacted**]
		  		  	3.2.1.7.11.5.4	  	Updated item (c) and added rationale.
	3.0	  	17 Dec 2010	  	Figure 3-1	  	Updated to [**Redacted**]
	 3.0
 (cont.)
	  		  	 3.1.3.1.1.8,
 Figures 3-3,
 3-4, & 3-5
	  	Deleted [**Redacted**]
		  		  	3.1.3.1.7	  	New requirement to [**Redacted**]
		  		  	3.2.1.5.5.2	  	Updated [**Redacted**]
		  		  	3.2.1.6.1	  	Removed TBR’s from the [**Redacted**]
		  		  	Table 3-5	  	Removed TBR’s from [**Redacted**]
		  		  	Figure 3-3	  	Updated the [**Redacted**], and removed TBR. Note new figure number.
		  		  	Table 3-7	  	Updated [**Redacted**]
		  		  	Table 3-9	  	Corrected [**Redacted**]
		  		  	3.2.1.7.6.1.6	  	Changed title to [**Redacted**]
		  		  	3.2.1.7.8.8	  	Removed TBR and rationale for [**Redacted**]

 
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	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

	4.0	  	2 Feb 2011	  	Various	  	Corrected table and figure reference errors throughout
		  		  	Table 3-1	  	Updated [**Redacted**]
		  		  	3.2.1.5.5.2	  	Updated [**Redacted**]
		  		  	3.2.1.7.6.2.1	  	Added item (d) to reflect [**Redacted**]
		  		  	3.2.1.7.6.2.2	  	Updated the [**Redacted**]
		  		  	3.2.1.7.7.1.7	  	Removed TBD from item (h)
		  		  	3.2.1.7.7.2.7	  	Updated [**Redacted**]
	5.0	  	2 May 2011	  	2.2.3	  	Updated [**Redacted**]
		  		  	3.1.2.4.1	  	Updated [**Redacted**]
		  		  	3.2.1.1.2.5	  	Updated [**Redacted**]
		  		  	3.2.1.4.1	  	Updated item (c) for [**Redacted**]
		  		  	 3.2.1.7.1.4.1
 3.2.1.7.1.4.2
 0
	  	Updated [**Redacted**]
	5.0 (cont.)	  		  	3.2.1.7.5.4.4	  	Clarified requirement [**Redacted**]
		  		  	3.2.1.7.6.2.7	  	Clarified requirement [**Redacted**]
		  		  	3.2.1.7.7.2.7	  	Clarified requirement [**Redacted**]

 
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 EXCHANGE COMMISSION 
  

							
	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

		  		  	3.2.1.7.8.7	  	Updated item (a) to reflect [**Redacted**]
		  		  	3.2.2.2	  	Updated reference to [**Redacted**]
		  		  	3.2.4.2.1	  	Updated Launch Induced Environments to refer to the [**Redacted**]
		  		  	3.3.6	  	Deleted this paragraph, as the contents are now contained in the requirements for affected components (ref. 3.2.1.7.5.4.4, 3.2.1.7.6.2.7 and 3.2.1.7.7.2.7).
	6.0	  	27 Jul 2011	  	Table 3-1	  	Updated [**Redacted**]
		  		  	3.2.1.7.1.4.1	  	Removed item (d)
		  		  	0	  	Clarified item (b)
		  		  	 3.1.3.3,
 Table 3-2
	  	New [**Redacted**]
		  		  	 3.1.3.3.6,
 Table 3-3
	  	New [**Redacted**]

  

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	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

		  		  	 1.2,
 Figure 3-1,
 Table 3-4,

Table 3-6,

3.2.1.7.7.1,

3.2.1.7.7.1.1,

3.2.1.7.7.1.5,

3.2.1.7.7.1.6,

3.2.1.7.7.1.7,

3.2.1.7.5.2,

3.2.1.7.9.1
	  	Updated to accommodate [**Redacted**]
	7.0	  	13 Sept 2011	  	All	  	Replace
		  		  	1.2	  	Updated with respect to [**Redacted**]
		  		  	2.2.1	  	Added [**Redacted**]
		  		  	Figure 3-1	  	Updated [**Redacted**]
		  		  	Table 3-3	  	Deleted (other table numbers unchanged)
		  		  	3.1.3.3.6	  	[**Redacted**]

  

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	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

	 7.0
 (cont.)
	  		  	 3.2.1.5.1.5,
 3.2.1.5.2,
 3.2.1.5.2.1,

3.2.1.5.5,

3.2.1.7.2.4.1,

3.2.1.7.7.1.1
	  	Requirements updated to include [**Redacted**]
		  		  	3.2.1.7.3.1	  	Changed due to additional [**Redacted**]
	8.0	  	2 Nov 2011	  	2.2.3	  	Updated [**Redacted**]
		  		  	Figure 3-1	  	Updated to reflect the [**Redacted**]
		  		  	Table 3-1	  	Updated [**Redacted**]
		  		  	3.1.3.3, various	  	Updated terminology with respect to the [**Redacted**]
		  		  	3.1.3.3.1.3	  	Updated [**Redacted**]
		  		  	3.1.3.3.1.4	  	Deleted “will” statement which was incorrect. [**Redacted**]
		  		  	3.1.3.3.3.1	  	Updated item [**Redacted**]

  

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 EXCHANGE COMMISSION 
  

							
	 Revision
	 	 Date
	 	Sections	  	 Description of Change

		 		 	3.1.3.3.3.4	  	Replaced TBD’s with [**Redacted**]
		 		 	3.1.3.3.4	  	Added general reference to ICD
		 		 	3.1.3.3.4.2	  	Clarified specification with respect to fields of view and removed TBR, [**Redacted**]
		 		 	3.1.3.3.5.1	  	Deleted (c)(2); removed TBR from item (c)(3); updated (d).
		 		 	3.1.3.3.6	  	New requirements
		 		 	3.1.3.3.6	  	Corrected sub-section numbers in this section
		 		 	3.1.4.1	  	Changed item (a)(2) to Reserved; added (c).
		 		 	3.1.4.4.1	  	Added (b), (c), (d) and (e). Note TBR’s.
		 		 	3.2.1.5.1.5,
 Table 3-7
	  	Updated to include [**Redacted**]
		 		 	3.2.1.5.2.1	  	Updated to include effects of secondary sensors.
		 		 	3.2.1.7.2.4.1	  	Updated in account for secondary sensors

 
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	 Revision
	 	 Date
	 	Sections	  	 Description of Change

		 		 	3.2.1.7.11,
 3.2.1.7.11.3.1
	  	Updated to explicitly allow [**Redacted**]
		 		 	3.2.1.7.11.3.5,
3.2.1.7.11.3.6	  	Added items (i) and (b)(6), respectively. TBR.
		 		 	3.2.1.7.11.4.8	  	Added item (b)
		 		 	Table 3-13	  	Updated to clarify with respect to [**Redacted**]
	9.0	 	19 Dec 2011	 	3.1.3.1.4.2	  	Clarified (b) and (c)
		 		 	3.1.3.3.1.3	  	Updated to point to the ICD
		 		 	3.1.3.3.4.2	  	Clarified item (b)
	9.0
 (cont.)
	 		 	3.1.4.1	  	Updated; added item (d) [**Redacted**]
		 		 	3.1.4.2	  	Extensively updated: [**Redacted**]
		 		 	Table 3-3	  	Reinstated for use as a [**Redacted**]

 
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	 Revision
	 	 Date
	 	Sections	  	 Description of Change

		 		 	3.1.4.4.1	  	Removed items (d) and (e); changed item (c) which had been erroneously placed in this section
		 		 	3.2.1.5.2.3	  	Clarified with respect to [**Redacted**]
		 		 	3.2.1.7.2.3	  	Clarified with respect to [**Redacted**]
		 		 	3.2.1.7.2.4.1	  	Reordered and updated items; added (f) and (g). New TBR’s.
		 		 	3.2.1.7.3.1	  	Updated to account for updated [**Redacted**]
	10.0	 	14 June 2012	 	2.1.1,
 2.2.2
	  	Updated reference documents
		 		 	3.1.2.1.3	  	Updated reference
		 		 	3.1.2.3	  	Updated/clarified rationale
		 		 	3.1.3.3.3.1	  	Updated rationale and clarified section heading
		 		 	3.1.3.3.5.1	  	Updated due to [**Redacted**]
		 		 	3.1.4.1	  	Updated for consistency with other [**Redacted**]
		 		 	Table 3-4,
Table 3-5	  	Updated to include [**Redacted**]
		 		 	3.2.1.4.1	  	Updated item (c)
		 		 	3.2.1.5.2	  	Updated to reflect secondary sensor performance constraints, and clarify design environments
		 		 	Table 3-7	  	Updated [**Redacted**]
		 		 	3.2.1.5.5.1	  	Updated to include [**Redacted**]

 
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	 Revision
	 	 Date
	 	Sections	  	 Description of Change

		 		 	3.2.1.5.5.2	  	Updated to refer to [**Redacted**]
		 		 	3.2.1.7.1.3.2	  	Updated to account for secondary sensors
		 		 	3.2.1.7.2.4.1	  	Removed TBR’s from (e) and (g)
		 		 	3.2.1.7.7.2.16	  	Updated (a) to account for latest system layout constraints
		 		 	3.2.1.7.11.3.5	  	Removed TBR from item (i)
		 		 	3.2.1.7.11.3.6	  	Removed TBR from item (b)(6)
	11.0	 	17 Oct 2012	 	Various	  	Minor edits to make ICD naming convention consistent throughout
		 		 	2.2.1	  	DAF ICD titles were made [**Redacted**] pending updates to those documents
	11.0
 (cont.)
	 		 	2.2.3	  	Removed TBD from last item
		 		 	3.1.4.2	  	Updated item (a)
		 		 	3.1.3.3.2	  	Added Aux Survival/Decontamination heater control
		 		 	Table 3-2	  	Added line item for Aux survival/decontamination heater power

  
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	 Revision
	 	 Date
	 	Sections	  	 Description of Change

		 		 	3.2.1.7.2.4.1	  	Updated item (c) and removed TBR’s
		 		 	3.2.1.7.7.1.1,
 3.2.1.7.7.2.1,

3.2.1.7.7.2.2,

3.2.1.7.11.5.4
	  	Corrected cross-reference typos

  

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	 Revision
	 	 Date
	 	Sections	  	 Description of Change

		 		 	3.2.1.7.10.6	  	New requirements
		 		 	3.2.1.7.11.3.2,
 3.2.1.7.11.3.5,

3.2.1.7.11.3.6,

3.2.1.7.11.4.2,

3.2.1.7.11.4.4,

3.2.1.7.11.4.5
	  	Updated [**Redacted**]

  
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 Table of Contents 

 

					
	 1. SCOPE
	  	 	1	  
		
	 1.1 Purpose
	  	 	1	  
	 1.2 System Overview
	  	 	1	  
	 1.3 Document Overview
	  	 	1	  
		
	 2. APPLICABLE DOCUMENTS
	  	 	2	  
		
	 2.1 Government Documents
	  	 	2	  
	 2.1.1 Specifications
	  	 	2	  
	 2.1.2 Standards
	  	 	2	  
	 2.2 Non-Government Documents
	  	 	3	  
	 2.2.1 DigitalGlobe Documents
	  	 	3	  
	 2.2.2 Space Segment Integrator Documents
	  	 	3	  
	 2.2.3 Other Documents
	  	 	3	  
	 2.3 Reference Documents
	  	 	3	  
		
	 3. REQUIREMENTS
	  	 	3	  
		
	 3.1 Satellite Definition
	  	 	3	  
	 3.1.1 Satellite Diagrams
	  	 	3	  
	 3.1.1.1 Component Tree
	  	 	3	  
	 3.1.1.2 Coordinate System
	  	 	3	  
	 3.1.2 Satellite Interfaces
	  	 	4	  
	 3.1.2.1 Non-interference with Outside Systems
	  	 	4	  
	 3.1.2.1.1 [**Redacted**]
	  	 	4	  
	 3.1.2.1.2 [**Redacted**]
	  	 	4	  
	 3.1.2.1.3 [**Redacted**]
	  	 	4	  
	 3.1.2.2 Satellite-Global Positioning System Interfaces
	  	 	4	  
	 3.1.2.2.1 Compatibility
	  	 	4	  
	 3.1.2.3 Satellite-Ground Interfaces
	  	 	4	  
	 3.1.2.3.1 Compatibility
	  	 	4	  
	 3.1.2.3.2 Remote Ground Terminal Locations
	  	 	4	  
	 3.1.2.3.3 Command Uplink
	  	 	4	  
	 3.1.2.3.4 Narrowband Telemetry Downlink
	  	 	4	  
	 3.1.2.3.5 Wideband Data Downlink
	  	 	5	  
	 3.1.2.4 Satellite-Launch Vehicle Interfaces
	  	 	5	  
	 3.1.2.4.1 Compatibility
	  	 	5	  
	 3.1.2.4.2 Nitrogen Purge
	  	 	5	  
	 3.1.2.4.3 Umbilical
	  	 	5	  
	 3.1.3 Customer Furnished Equipment
	  	 	6	  
	 3.1.3.1 Instrument
	  	 	6	  
	 3.1.3.1.1 Physical, Structural and Mechanical Requirements
	  	 	6	  
	 3.1.3.1.2 Thermal Interfaces
	  	 	6	  
	 3.1.3.1.3 Power Interfaces
	  	 	7	  
	 3.1.3.1.4 Command and Telemetry Interfaces
	  	 	7	  
	 3.1.3.1.5 Image Data Interfaces
	  	 	8	  

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

  
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	 3.1.3.1.6 [**Redacted**]
	  	 	8	  
	 3.1.3.1.7 [**Redacted**]
	  	 	9	  
	 3.1.3.2 MGB
	  	 	9	  
	 3.1.3.3 [**Redacted**]
	  	 	9	  
	 3.1.3.3.1 [**Redacted**]
	  	 	9	  
	 3.1.3.3.2 [**Redacted**]
	  	 	9	  
	 3.1.3.3.3 [**Redacted**]
	  	 	9	  
	 3.1.3.3.4 [**Redacted**]
	  	 	10	  
	 3.1.3.3.5 [**Redacted**]
	  	 	11	  
	 3.1.3.3.6 [**Redacted**]
	  	 	11	  
	 3.1.4 [**Redacted**]
	  	 	11	  
	 3.1.4.1 [**Redacted**]
	  	 	11	  
	 3.1.4.2 [**Redacted**]
	  	 	11	  
	 3.1.4.3 [**Redacted**]
	  	 	11	  
	 3.1.4.3.1 [**Redacted**]
	  	 	11	  
	 3.1.4.3.2 [**Redacted**]
	  	 	11	  
	 3.1.4.4 [**Redacted**]
	  	 	11	  
	 3.1.4.4.1 [**Redacted**]
	  	 	11	  
	 3.1.4.4.2 [**Redacted**]
	  	 	12	  
	 3.1.4.4.3 [**Redacted**]
	  	 	12	  
	 3.1.4.4.4 [**Redacted**]
	  	 	12	  
	 3.1.4.5 [**Redacted**]
	  	 	12	  
	 3.2 Satellite Characteristics
	  	 	12	  
	 3.2.1 Performance
	  	 	12	  
	 3.2.1.1 General Mission Requirements
	  	 	12	  
	 3.2.1.1.1 Mission Life
	  	 	12	  
	 3.2.1.1.2 Orbits
	  	 	12	  
	 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
	  	 	13	  
	 3.2.1.2.3 Intermediate and Transitional Modes
	  	 	14	  
	 3.2.1.3 Pre-Launch Operations
	  	 	14	  
	 3.2.1.3.1 Ground Storage
	  	 	14	  
	 3.2.1.3.2 Launch Delay
	  	 	14	  
	 3.2.1.4 Early Orbit Operations
	  	 	14	  
	 3.2.1.4.1 Autonomous Operations After Separation
	  	 	14	  
	 3.2.1.4.2 First 48 hours
	  	 	14	  
	 3.2.1.4.3 Commissioning
	  	 	14	  
	 3.2.1.5 Mission Operations
	  	 	14	  
	 3.2.1.5.1 Viewing Angles
	  	 	14	  
	 3.2.1.5.2 Imaging and Downlink Operations
	  	 	15	  
	 3.2.1.5.3 Stereo Imaging
	  	 	16	  
	 3.2.1.5.4 Off-Nadir Imaging
	  	 	17	  

  
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	 3.2.1.5.5 Special Imaging
	  	 	16	  
	 3.2.1.5.6 [**Redacted**]
	  	 	16	  
	 3.2.1.6 Instrument Requirements
	  	 	16	  
	 3.2.1.6.1 Integrated Bus/Instrument Performance Effects
	  	 	16	  
	 3.2.1.6.2 [**Redacted**]
	  	 	17	  
	 3.2.1.6.3 [**Redacted**]
	  	 	17	  
	 3.2.1.6.4 [**Redacted**]
	  	 	17	  
	 3.2.1.7 Bus Subsystem Requirements
	  	 	18	  
	 3.2.1.7.1 [**Redacted**]
	  	 	18	  
	 3.2.1.7.2 ADCS
	  	 	19	  
	 3.2.1.7.3 Propulsion
	  	 	22	  
	 3.2.1.7.4 Flight Software
	  	 	22	  
	 3.2.1.7.5 C&DH
	  	 	24	  
	 3.2.1.7.6 Narrowband Communications
	  	 	26	  
	 3.2.1.7.7 [**Redacted**]
	  	 	29	  
	 3.2.1.7.8 EPDS
	  	 	32	  
	 3.2.1.7.9 Structures and Mechanisms
	  	 	33	  
	 3.2.1.7.10 Thermal Control
	  	 	34	  
	 3.2.1.7.11 [**Redacted**]
	  	 	35	  
	 3.2.2 Physical Characteristics
	  	 	39	  
	 3.2.2.1 Size Constraints
	  	 	39	  
	 3.2.2.2 Mass Constraints
	  	 	39	  
	 3.2.2.3 Shipping Constraints
	  	 	39	  
	 3.2.3 Reliability
	  	 	39	  
	 3.2.3.1 [**Redacted**]
	  	 	39	  
	 3.2.3.2 [**Redacted**]
	  	 	39	  
	 3.2.3.3 [**Redacted**]
	  	 	39	  
	 3.2.3.4 Cycle-Limited Items
	  	 	39	  
	 3.2.3.4.1 [**Redacted**]
	  	 	40	  
	 3.2.3.4.2 [**Redacted**]
	  	 	40	  
	 3.2.4 Availability and Maintainability
	  	 	40	  
	 3.2.4.1 Fault Recovery Timeline
	  	 	40	  
	 3.2.4.2 Environmental Conditions
	  	 	40	  
	 3.2.4.2.1 Launch Induced Environments
	  	 	40	  
	 3.2.4.2.2 On-Orbit Environments
	  	 	40	  
	 3.2.4.2.3 Pre-Launch Environments
	  	 	40	  
	 3.3 Satellite Design and Construction
	  	 	40	  
	 3.3.1 General
	  	 	40	  
	 3.3.2 SEUs
	  	 	40	  
	 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**]
	  	 	41	  

  
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	 3.3.4.3 [**Redacted**]
	  	 	41	  
	 3.3.4.4 [**Redacted**]
	  	 	41	  
	 3.3.5 Safety
	  	 	41	  
	 3.3.6 Reserved
	  	 	41	  
	 4. VERIFICATION
	  	 	41	  
	 5. QUALITY ASSURANCE
	  	 	41	  

  
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 List of Tables 

 

					
	 Table 3-1 [**Redacted**]
	  	 	7	  
	 Table 3-2 [**Redacted**]
	  	 	10	  
	 Table 3-3 [**Redacted**]
	  	 	10	  
	 Table 3-4 [**Redacted**]
	  	 	13	  
	 Table 3-5 [**Redacted**]
	  	 	13	  
	 Table 3-6 [**Redacted**]
	  	 	14	  
	 Table 3-7 [**Redacted**]
	  	 	15	  
	 Table 3-8 [**Redacted**]
	  	 	21	  
	 Table 3-9 [**Redacted**]
	  	 	21	  
	 Table 3-10 [**Redacted**]
	  	 	26	  
	 Table 3-11 [**Redacted**]
	  	 	31	  
	 Table 3-12 [**Redacted**]
	  	 	38	  
	 Table 3-13 [**Redacted**]
	  	 	40	  

 List of Figures 
  

					
	 Figure 3-1[**Redacted**]
	  	 	3	  
	 Figure 3-2 [**Redacted**]
	  	 	4	  
	 Figure 3-3 [**Redacted**]
	  	 	15	  
	 Figure 3-4 [**Redacted**]
	  	 	29	  
	 Figure 3-5 [**Redacted**]
	  	 	31	  
	 Figure 3-6 [**Redacted**]
	  	 	38	  

  
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 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 (Instrument), as well as [**Redacted**] This will be the same Bus design as used for
predecessor WorldView Satellites. The Instrument and [**Redacted**] 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. BATC will provide and integrate [**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 [**Redacted**] with a descending equator crossing
[**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. [**Redacted**] 

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 WV3 Instrument to Spacecraft ICD 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 Specifications 

[**Redacted**] 
 2.1.2
Standards 
 [**Redacted**] 
  

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 2.2 Non-Government Documents 
 2.2.1 DigitalGlobe Documents 
 [**Redacted**] 

2.2.2 Space Segment Integrator Documents 
 [**Redacted**] 
 2.2.3 Other Documents 

[**Redacted**] 
 2.3
Reference Documents 
 [**Redacted**] 
 3. REQUIREMENTS 
 Remarks contained as [**Redacted**] 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 as CFE 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 as [**Redacted**]. 

Figure 3-1[**Redacted**] 

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**] 
 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
[**Redacted**]. 
  
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 Figure 3-2 [**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**] 

[**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 [**Redacted**].  
 [**Redacted**] 
 3.1.2.3.1 Compatibility 

The Satellite [**Redacted**] 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 
  
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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**]. 
 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**] 
 [**Redacted**] 
 3.1.2.4.2 Nitrogen Purge 

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**]

 [**Redacted**] 
  

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 3.1.3 Customer Furnished Equipment 
 3.1.3.1 Instrument 
 The Instrument will be provided to the SSI as [**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 WV3 Instrument to Spacecraft ICD. 
 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**]. 
 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 WV3 Instrument to Spacecraft ICD: 

[**Redacted**] 
  

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 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 WV3 Instrument to
Spacecraft ICDs. 
 3.1.3.1.3.1 Instrument Power Feeds 
 The Spacecraft Bus shall provide power to all Instrument units as follows: 

[**Redacted**] 

[**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 Load Shedding 

[**Redacted**] 

3.1.3.1.3.4 Average Operating Power 

During normal operations, the Spacecraft Bus shall be able to perform [**Redacted**]. 

Table 3-1 [**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**]. 

[**Redacted**] 
 [**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**] 
 [**Redacted**] 
 3.1.3.1.4.1 Instrument Commanding 

Using the specified data interfaces, the Spacecraft Bus shall forward commands to the Instrument, either real-time or stored, as documented in the WV3
Instrument to Spacecraft ICD. 
  
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 3.1.3.1.4.2 Image Start and Stop Commands 

 

	 	a)	The commands for main Instrument image [**Redacted**] shall be issued from the Spacecraft Bus [**Redacted**]. 

 

	 	b)	The Bus shall allow main Instrument command timing consistent with [**Redacted**], so as to allow collection of the same contiguous area with all sensors or any
combination thereof. 

  

	 	c)	Commands for the main Instrument image [**Redacted**] on an image by image basis with respect to the Bus scanning maneuver, [**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 WV3 Instrument to Spacecraft ICD.
The following rules shall be applied to Instrument telemetry: 
 [**Redacted**] 

[**Redacted**] 
 3.1.3.1.4.5
[**Redacted**] 
 The Spacecraft Bus shall provide a [**Redacted**] as follows: 

[**Redacted**] 

[**Redacted**] 
 3.1.3.1.5
Image Data Interfaces 
 The Spacecraft Bus shall provide image data interfaces [**Redacted**]. 

[**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**] 

[**Redacted**] 
 3.1.3.1.6
[**Redacted**] 
 [**Redacted**] 
  

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 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 as [**Redacted**]. The Spacecraft Bus shall interface to the [**Redacted**] as specified in the [**Redacted**]. 

3.1.3.2 MGB 
 The MGB will be provided to
the SSI as [**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**] 
  

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 3.1.3.3.3.1     [**Redacted**] 

[**Redacted**] 
 3.1.3.3.3.2
    [**Redacted**] 
     [**Redacted**] 

3.1.3.3.3.3     [**Redacted**] 
     [**Redacted**] 
 3.1.3.3.3.4
    [**Redacted**] 
     [**Redacted**] 

Table 3-2 [**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**] 
  
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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**] 
 Table 3-3 [**Redacted**] 
 3.1.4.3     [**Redacted**]

 [**Redacted**] 

3.1.4.3.1 [**Redacted**] 

[**Redacted**] 
 3.1.4.3.2
[**Redacted**] 
     [**Redacted**] 
 3.1.4.4     [**Redacted**] 
 [**Redacted**] 

3.1.4.4.1 [**Redacted**] 

[**Redacted**] 
  

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 3.1.4.4.2 [**Redacted**] 
     [**Redacted**] 
 3.1.4.4.3 [**Redacted**] 

    [**Redacted**] 
  

	3.1.4.4.4	[**Redacted**] 

[**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 WV3 Instrument to Spacecraft 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**]. 

[**Redacted**] 
 3.2.1.1.2.2
Reserved 
 3.2.1.1.2.3 Mission Orbit 
 The Mission Orbit shall be defined as: 
     [**Redacted**] 

[**Redacted**] 
  

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 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**] 
 [**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**]

 [**Redacted**] 
 Table 3-4 [**Redacted**] 
 3.2.1.2.2 Special / Contingency Modes 

The Satellite shall, at a minimum, provide the modes defined in [**Redacted**]. 
 a) [**Redacted**] 
 [**Redacted**] 

Table 3-5 [**Redacted**] 
  

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 Table 3-6 [**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**] 
 [**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: 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.4.2 First 48 hours 

Following the Autonomous Operations after Separation, the Satellite shall pose no constraints on operation such that: 

[**Redacted**] 

[**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**] 

 
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 3.2.1.5.1.1 Nominal Field of Regard 
 The Nominal Field of Regard shall be defined as a [**Redacted**] 
 [**Redacted**]

 3.2.1.5.1.2 Maximum Field of Regard 
 The Maximum Field of Regard shall be defined as a [**Redacted**] 
 [**Redacted**]

 3.2.1.5.1.3 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

 
 3.2.1.5.1.4 [**Redacted**] 

[**Redacted**] 
 [**Redacted**]

 3.2.1.5.1.5 Instrument, [**Redacted**] 
 The Satellite shall allow operation of the Instrument, [**Redacted**] 

[**Redacted**] 

Table 3-7 [**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**] 

[**Redacted**] 
 3.2.1.5.2.1
[**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 
 Figure 3-3 [**Redacted**] 

3.2.1.5.2.2 Wideband and Narrowband Downlinks 
 It shall be possible to perform both Wideband and Narrowband downlinks as follows: 

[**Redacted**] 

[**Redacted**] 
 3.2.1.5.2.3
Instrument Mass Properties for [**Redacted**] 
 For purposes of verifying the Satellite’s ability to perform the
[**Redacted**]. 
  
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and Confidential 
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 3.2.1.5.2.4 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.5.3 Stereo Imaging 
  

	a)	The Satellite shall be capable of collecting the stereo imagery [**Redacted**] 

 [**Redacted**] 
 3.2.1.5.4 Off-Nadir Imaging 

The Satellite shall be capable of supporting off-nadir image collections as follows: 

[**Redacted**] 

[**Redacted**] 
 3.2.1.5.5
Special Imaging 
 3.2.1.5.5.1 Minimum Capabilities 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.5.5.2 Main Instrument [**Redacted**] 
 For the Main Instrument (not Secondary Sensors): 
 [**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: 
 a) [**Redacted**] 
 3.2.1.6.1.1 [**Redacted**] 
 [**Redacted**] 

[**Redacted**] 
 3.2.1.6.1.2
[**Redacted**] 
 [**Redacted**] 
  

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 [**Redacted**] 
 3.2.1.6.2 [**Redacted**] 
 [**Redacted**] 

3.2.1.6.2.1 [**Redacted**] 

[**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**] 
 3.2.1.6.3.5.2 [**Redacted**] 
 [**Redacted**] 

3.2.1.6.3.6 [**Redacted**] 
 [**Redacted**] 
 3.2.1.6.4 [**Redacted**] 

[**Redacted**] 
  

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 3.2.1.6.4.1 [**Redacted**] 
 [**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**] 
 [**Redacted**] 

3.2.1.7.1.2 [**Redacted**] 
  

	a)	[**Redacted**] 

 [**Redacted**]

 3.2.1.7.1.3 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.1.3.1 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.1.3.2 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.1.3.3 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.1.3.4 [**Redacted**] 
 [**Redacted**] 
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 3.2.1.7.1.3.5 [**Redacted**] 

[**Redacted**] 
 [**Redacted**]

 3.2.1.7.1.3.6 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.1.3.7 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.1.3.8 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.1.4 [**Redacted**] 

3.2.1.7.1.4.1 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.1.4.2 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.1.4.3 [**Redacted**] 
 [**Redacted**] 
 3.2.1.7.1.4.4 [**Redacted**] 

[**Redacted**] 

[**Redacted**] 
 3.2.1.7.2
ADCS 
 3.2.1.7.2.1 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

 
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 3.2.1.7.2.2 [**Redacted**] 
 3.2.1.7.2.2.1 [**Redacted**] 
 [**Redacted**]

 [**Redacted**] 

3.2.1.7.2.2.2 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.2.2.3 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.2.2.4 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.2.2.5 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.2.3 [**Redacted**] 

[**Redacted**] 
 [**Redacted**]

 3.2.1.7.2.4 [**Redacted**] 
 3.2.1.7.2.4.1 [**Redacted**] 
 [**Redacted**]

 [**Redacted**] 

3.2.1.7.2.4.2 [**Redacted**] 
 [**Redacted**] 
 3.2.1.7.2.5 Reserved 

3.2.1.7.2.6 [**Redacted**] 

[**Redacted**] 
 [**Redacted**]

 3.2.1.7.2.7 [**Redacted**] 
 [**Redacted**] 
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 3.2.1.7.2.8 [**Redacted**] 

[**Redacted**] 

[**Redacted**] 
 3.2.1.7.2.9
[**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 
 3.2.1.7.2.9.1 [**Redacted**] 

[**Redacted**] 

[**Redacted**] 

Table 3-8 [**Redacted**] 

3.2.1.7.2.9.2 [**Redacted**] 
 [**Redacted**] 
 3.2.1.7.2.9.3 [**Redacted**] 

[**Redacted**] 
 Table
3-9 [**Redacted**] 
 [**Redacted**] 
 3.2.1.7.2.9.4 [**Redacted**] 
  

	a)	[**Redacted**] 

 [**Redacted**]

 3.2.1.7.2.9.5 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.2.10 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.2.11 Solar Arrays 

[**Redacted**] 
 [**Redacted**]

 3.2.1.7.2.12 [**Redacted**] 
 [**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**]. 
 [**Redacted**] 
 3.2.1.7.3.2 Propellant Budget 
 The SSI shall develop and maintain a
[**Redacted**] 
 [**Redacted**] 
 [**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**] 

[**Redacted**] 
 3.2.1.7.3.4
[**Redacted**] 
 [**Redacted**] 
 3.2.1.7.3.5 [**Redacted**] 
 [**Redacted**] 

[**Redacted**] 
 3.2.1.7.4 Flight
Software 
 3.2.1.7.4.1 [**Redacted**] 
 [**Redacted**] 
 [**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**] across multiple contacts, [**Redacted**]. 

[**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. 
  

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 3.2.1.7.4.3.2 [**Redacted**] 

[**Redacted**] 
 [**Redacted**]

 3.2.1.7.4.4 [**Redacted**] 
 [**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**] 
 [**Redacted**]

 3.2.1.7.4.6 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.4.7 [**Redacted**] 

[**Redacted**] 
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 3.2.1.7.4.7.1 [**Redacted**] 
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3.2.1.7.4.8 [**Redacted**] 

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 3.2.1.7.4.9 [**Redacted**] 
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[**Redacted**] 
 3.2.1.7.4.10
[**Redacted**] 
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 Use or disclosure of data is
subject to the restriction on the title page of this document. 

  
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 EXCHANGE COMMISSION 
  

 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 the [**Redacted**] 

3.2.1.7.5.1.3 [**Redacted**] 
 [**Redacted**] 
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3.2.1.7.5.1.4 [**Redacted**] 
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3.2.1.7.5.1.6 [**Redacted**] 
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3.2.1.7.5.1.7 [**Redacted**] 
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3.2.1.7.5.1.8 [**Redacted**] 
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 3.2.1.7.5.1.9 [**Redacted**] 

[**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 [**Redacted**] 

The C&DH [**Redacted**]shall collect and format housekeeping telemetry for the [**Redacted**] sufficient to provide the following
capabilities on the ground: 
  
 DigitalGlobe
Proprietary and Confidential 
 Use or disclosure of data is subject to the restriction on the title page of this document.

  
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3.2.1.7.5.2.3 [**Redacted**] 
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 3.2.1.7.5.2.5 [**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 [**Redacted**] of telemetry at an average [**Redacted**] 

[**Redacted**] 

3.2.1.7.5.2.8 [**Redacted**] 
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 3.2.1.7.5.2.9 [**Redacted**] 

[**Redacted**] 
 3.2.1.7.5.3
[**Redacted**] 
 [**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 to the
[**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 3-10 [**Redacted**] 

3.2.1.7.5.4.2 Format 
 The
C&DH subsystem shall format the [**Redacted**] 
 [**Redacted**] 

3.2.1.7.5.4.3 Redefinable Content 

It shall be possible to independently re-define the content of the [**Redacted**] 
 [**Redacted**] 
 3.2.1.7.5.4.4 [**Redacted**] 

[**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**] 

[**Redacted**] 

3.2.1.7.5.4.6 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.5.4.7 [**Redacted**] 
 [**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**] 
 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**] 

[**Redacted**] 
 3.2.1.7.6.1.2
Bit Error Rate 
 The Command Uplink shall provide a bit error rate not to exceed [**Redacted**]. 

 
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 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**] 
 [**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**]

 [**Redacted**] 

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**] 

[**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**] 
 [**Redacted**] 
 3.2.1.7.6.2.2 [**Redacted**]
Telemetry Bit Rate 
 The Telemetry Downlink shall be at a
[**Redacted**]. 
 [**Redacted**] 
  

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

  
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 FOIA CONFIDENTIAL TREATMENT REQUESTED 

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 EXCHANGE COMMISSION 
  

 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**] 
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 [**Redacted**] 
 3.2.1.7.6.2.8 [**Redacted**] 

[**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**] 

  

	b)	A minimum elevation angle up to [**Redacted**] shall be permitted. 

  

	c)	It shall be permissible to require ground commands in order to [**Redacted**] 

 [**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**] 
 [**Redacted**] 
  
 DigitalGlobe Proprietary and Confidential 
 Use or disclosure of data is
subject to the restriction on the title page of this document. 

  
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 3.2.1.7.6.2.13 Antenna Polarization 

The Telemetry Downlink antenna shall use [**Redacted**] 
 [**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**] 

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3.2.1.7.7.1 [**Redacted**] 

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3.2.1.7.7.1.4 [**Redacted**] 
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Figure 3-4 [**Redacted**] 

3.2.1.7.7.1.5 [**Redacted**] 
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3.2.1.7.7.1.6 [**Redacted**] 
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 3.2.1.7.7.2.1 [**Redacted**] 

[**Redacted**] 
 Table 3-11 [**Redacted**] 
  
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 3.2.1.7.7.2.7 [**Redacted**]

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Reserved 
 3.2.1.7.7.2.9 [**Redacted**] 
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Figure 3-5 [**Redacted**] 

3.2.1.7.7.2.10 [**Redacted**] 
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3.2.1.7.7.2.21 [**Redacted**] 
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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**] 
 [**Redacted**] 

3.2.1.7.8.2 Realistic Worst Case Conditions 
 EPDS performance shall be evaluated under realistic worst-case conditions [**Redacted**] 
  

DigitalGlobe Proprietary and Confidential 
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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 at the nominal orbit specified in [**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**] 
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 3.2.1.7.8.6 [**Redacted**] 

[**Redacted**] 
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 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 [**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**] 

[**Redacted**] 
  

DigitalGlobe Proprietary and Confidential 
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 3.2.1.7.9.3.4 [**Redacted**] 

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[**Redacted**] 
 [**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 cannot
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**] 
 [**Redacted**] 
 3.2.1.7.10.4 [**Redacted**] 
 [**Redacted**] 

[**Redacted**] 
 3.2.1.7.10.4.1
Number of Circuits 
 [**Redacted**] 
 3.2.1.7.10.4.2 [**Redacted**] 
 [**Redacted**]

 3.2.1.7.10.4.3 [**Redacted**] 
 [**Redacted**] 
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3.2.1.7.10.4.4 [**Redacted**] 
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 3.2.1.7.10.4.5 [**Redacted**] 

[**Redacted**] 
  

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 3.2.1.7.10.4.6 [**Redacted**] 

Reserved 
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3.2.1.7.10.5 [**Redacted**] 

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WITH THE SECURITIES AND
 EXCHANGE COMMISSION 
  

 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**] 
 [**Redacted**] 

3.2.1.7.11.5.2 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

[**Redacted**] 

3.2.1.7.11.5.3 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

3.2.1.7.11.5.4 [**Redacted**] 
 [**Redacted**] 
 [**Redacted**] 

Table 3-12 [**Redacted**] 
 Figure 3-6 [**Redacted**] 
  
 DigitalGlobe Proprietary and Confidential 
 Use or disclosure of data is
subject to the restriction on the title page of this document. 

  
 38 

 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 
  

 3.2.1.7.11.5.5 [**Redacted**] 

[**Redacted**] 
 3.2.1.7.11.5.6
[**Redacted**] 
 [**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**] 
 [**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**] 
 3.2.3 Reliability 
 3.2.3.1 [**Redacted**] 
 [**Redacted**] 

[**Redacted**] 
 3.2.3.2
[**Redacted**] 
 [**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 two times 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**] 
  

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

  
 39 

 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 
  

 3.2.3.4.1 [**Redacted**] 
 [**Redacted**] 
  
 Table 3-13 [**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 24 hours of ground operator intervention, with the exception of [**Redacted**] 
 [**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**] 
 [**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**] 
  

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

  
 40 

 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 
  

 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 Reserved 

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

  
 41 

 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 
  

 WorldView 3 Payment Milestone Schedule 

Exhibit 3 to WV3 Satellite Agreement # 60150 
  

																	
	 Item
#
	  	Invoice Date	 	  	Line
Item	 	  	 Description
	  	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**]	  	[90000000]
		  				  	 	a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	[**Redacted**]
		  				  	 	b	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
		  				  	 	c	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
		  				  	 	d	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
	9	  	 	[**Redacted**]	  	  				  	Milestone 9 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  				  	 	9a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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		  				  	 	9d	  	  	[**Redacted**]	  	[**Redacted**]	  		  	

 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 
  

															
	10	  	[**Redacted**]	  				  	Milestone 10 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	10a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	[**Redacted**]
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		  		  	 	10d	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
	11	  	[**Redacted**]	  				  	Milestone 11 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	11a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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		  		  	 	11e	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
	12	  	[**Redacted**]	  				  	Milestone 12 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	12a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
		  		  	 	12b	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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	13	  	[**Redacted**]	  				  	Milestone 13 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	13a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	[**Redacted**]
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		  		  	 	13f	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
	14	  	[**Redacted**]	  				  	Milestone 14 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	14a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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		  		  	 	14e	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
	15	  	[**Redacted**]	  				  	Milestone 15 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	15a	  	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	
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		  		  	 	15f	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
	16	  	[**Redacted**]	  				  	Milestone 16 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	16a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
		  		  	 	16b	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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		  		  	 	16e	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
	17	  	[**Redacted**]	  				  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	17a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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		  		  	 	17d	  	  	[**Redacted**]	  	[**Redacted**]	  		  	

 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 
  

															
	18	  	[**Redacted**]	  				  	Milestone 18 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	18a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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		  		  	 	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**]	  		  	
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		  		  	 	21a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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		  		  	 	21e	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
	22	  	[**Redacted**]	  				  	Milestone 22 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	 	22b	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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		  		  	 	23a	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
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	25	  	[**Redacted**]	  				  	Milestone 25 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
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		  		  	 	25e	  	  	[**Redacted**]	  	[**Redacted**]	  		  	

 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 
  

															
	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**]	  		  	
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		  		  	 	27d	  	  	[**Redacted**]	  	[**Redacted**]	  		  	
	28	  	[**Redacted**]	  				  	Milestone 28 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
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	29	  	[**Redacted**]	  				  	Milestone 29 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
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		  		  	 	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**]	  		  	
		  		  	 	30e	  	  	[**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**]	  		  	

 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 
  

															
	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**]	  		  	

 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 
  

															
	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	  	$217,762,399	  	$217,762,399	  	$217,762,399
		  		  				  		  	  
	  	  
	  	  

 10385893 
 WV-3 CAVIS-ACI Specification 
  
 

 
 WorldView-3 CAVIS-ACI 
 Atmospheric Correction 
 Instrument Specification 

 

			
	Document #	  	10385893
	Revision #	  	4.0
	Release Date	  	22 May 2012
	Prepared by	  	 Amy Newbury, Paul
 Scott, Frank
Gerlach

	Approved by	  	Keith Constantinides

 RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION 

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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. 

 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 Change Record 

 

							
	 Revision
	  	 Date
	  	Sections	  	 Description of Change

	 1.0
	  	[**Redacted**]	  		  	
				
	 3.0
	  	[**Redacted**]	  		  	

  
  

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

  
 i 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

							
	 Revision
	  	 Date
	  	Sections	  	 Description of Change

	 4.0
	  	[**Redacted**]	  		  	

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

  
 ii 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 Table of Contents 

 

					
	 1.     Scope
	  	 	1	  
	     1.1     Purpose
	  	 	1	  
	     1.2     System Overview
	  	 	1	  
	 2.     Applicable Documents
	  	 	1	  
	 3.     Requirements
	  	 	2	  
	     3.1     [**Redacted**]
	  	 	2	  
	         3.1.1
        [**Redacted**]
	  	 	2	  
	     3.2     [**Redacted**]
	  	 	2	  
	         3.2.1
        [**Redacted**]
	  	 	2	  
	         3.2.2
        [**Redacted**]
	  	 	2	  
	         3.2.3
        Reserved
	  	 	2	  
	         3.2.4
        Reserved
	  	 	2	  
	         3.2.5
        [**Redacted**]
	  	 	2	  
	         3.2.6
        Reserved
	  	 	2	  
	         3.2.7
        [**Redacted**]
	  	 	2	  
	     3.3     [**Redacted**]
	  	 	2	  
	         3.3.1
        [**Redacted**]
	  	 	3	  
	         3.3.2
        [**Redacted**]
	  	 	3	  
	         3.3.3
        [**Redacted**]
	  	 	3	  
	         3.3.4
        [**Redacted**]
	  	 	3	  
	         3.3.5
        [**Redacted**]
	  	 	3	  
	         3.3.6
        [**Redacted**]
	  	 	3	  
	         3.3.7
        [**Redacted**]
	  	 	3	  
	         3.3.8
        [**Redacted**]
	  	 	3	  
	         3.3.9
        [**Redacted**]
	  	 	3	  
	         3.3.10
        [**Redacted**]
	  	 	3	  
	         3.3.11
        [**Redacted**]
	  	 	3	  
	         3.3.12
        [**Redacted**]
	  	 	4	  
	         3.3.13
        [**Redacted**]
	  	 	5	  
	         3.3.14
        [**Redacted**]
	  	 	6	  
	         3.3.15
        [**Redacted**]
	  	 	6	  
	         3.3.16
        [**Redacted**]
	  	 	6	  
	         3.3.17
        [**Redacted**]
	  	 	6	  
	         3.3.18
        [**Redacted**]
	  	 	6	  
	         3.3.19
        [**Redacted**]
	  	 	6	  
	         3.3.20
        [**Redacted**]
	  	 	6	  
	         3.3.21
        [**Redacted**]
	  	 	6	  
	         3.3.22
        [**Redacted**]
	  	 	7	  
	         3.3.23
        [**Redacted**]
	  	 	7	  
	         3.3.24
        [**Redacted**]
	  	 	7	  

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

  
 iii

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

					
	
        3.3.25        [**Redacted**]
	  	 	7	  
	
        3.3.26        [**Redacted**]
	  	 	7	  
	
        3.3.27        [**Redacted**]
	  	 	7	  
	
        3.3.28        [**Redacted**]
	  	 	7	  
	
        3.3.29        [**Redacted**]
	  	 	7	  
	
        3.3.30        [**Redacted**]
	  	 	7	  
	
        3.3.31        [**Redacted**]
	  	 	7	  
	
        3.3.32        [**Redacted**]
	  	 	7	  
	
        3.3.33        [**Redacted**]
	  	 	8	  
	
        3.3.34        [**Redacted**]
	  	 	8	  
	
        3.3.35        [**Redacted**]
	  	 	9	  
	     3.4    [**Redacted**]
	  	 	9	  
	
        3.4.1        [**Redacted**]
	  	 	9	  
	
        3.4.2        [**Redacted**]
	  	 	9	  
	
        3.4.3        [**Redacted**]
	  	 	9	  
	
        3.4.4        [**Redacted**]
	  	 	9	  
	     3.5    [**Redacted**]
	  	 	10	  
	
        3.5.1        [**Redacted**]
	  	 	10	  
	
        3.5.2        [**Redacted**]
	  	 	10	  
	     3.6    [**Redacted**]
	  	 	10	  
	
        3.6.1        [**Redacted**]
	  	 	10	  
	
        3.6.2        [**Redacted**]
	  	 	10	  
	
        3.6.3        [**Redacted**]
	  	 	10	  
	     3.7    [**Redacted**]
	  	 	11	  
	
        3.7.1        [**Redacted**]
	  	 	11	  
	
        3.7.2        [**Redacted**]
	  	 	11	  
	     3.8    [**Redacted**]
	  	 	11	  
	
        3.8.1        [**Redacted**]
	  	 	11	  
	
        3.8.2        [**Redacted**]
	  	 	11	  
	
        3.8.3        [**Redacted**]
	  	 	11	  
	
        3.8.4        [**Redacted**]
	  	 	11	  
	
        3.8.5        [**Redacted**]
	  	 	11	  
	     3.9    [**Redacted**]
	  	 	11	  
	
        3.9.1        [**Redacted**]
	  	 	11	  
	
        3.9.2        [**Redacted**]
	  	 	12	  
	     3.10    [**Redacted**]
	  	 	12	  
	     3.11    [**Redacted**]
	  	 	14	  
	
        3.11.1        [**Redacted**]
	  	 	14	  
	
        3.11.2        [**Redacted**]
	  	 	14	  
	
        3.11.3        [**Redacted**]
	  	 	14	  
	
        3.11.4        [**Redacted**]
	  	 	14	  
	
        3.11.5        [**Redacted**]
	  	 	14	  

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

  
 iv 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 1. Scope 
 1.1 Purpose 
 [**Redacted**] 

1.2 System Overview 

[**Redacted**] 
 2. Applicable
Documents 
 [**Redacted**] 
  

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

  
 1 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 3. Requirements 
 3.1 [**Redacted**] 
 [**Redacted**] 

3.1.1 [**Redacted**] 
 [**Redacted**]

 3.2 [**Redacted**] 

3.2.1 [**Redacted**] 

 [**Redacted**] 
 Table 3.2.1-1 [**Redacted**] 
 3.2.2 [**Redacted**] 

[**Redacted**] 
 3.2.3 Reserved

 3.2.4 Reserved 
 3.2.5
[**Redacted**] 
 [**Redacted**] 
 3.2.6 Reserved 
 3.2.7 [**Redacted**] 

[**Redacted**] 
 3.3 [**Redacted**]

 [**Redacted**] 
  

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

  
 2 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 3.3.1 [**Redacted**] 
 [**Redacted**] 
 3.3.2 [**Redacted**] 

[**Redacted**] 
 3.3.3 [**Redacted**]

 [**Redacted**] 
 3.3.4
[**Redacted**] 
 [**Redacted**] 
 3.3.5 [**Redacted**] 
 [**Redacted**] 

3.3.6 [**Redacted**] 
 [**Redacted**]

 3.3.7 [**Redacted**] 

[**Redacted**] 
 3.3.8 [**Redacted**]

 [**Redacted**] 
 Table 3.3.8-1 [**Redacted**] 
 [**Redacted**]

 3.3.9 [**Redacted**] 

[**Redacted**] 
 3.3.10 [**Redacted**]

 [**Redacted**] 

3.3.11 [**Redacted**] 
 [**Redacted**]

  
 DigitalGlobe Proprietary and Confidential

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

  
 3 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 Table 3.3.11-1:[**Redacted**] 

3.3.12 [**Redacted**] 
 [**Redacted**]

  
 DigitalGlobe Proprietary and Confidential

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

  
 4 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 Table 3.3.12-1 [**Redacted**] 

3.3.13 [**Redacted**] 
 [**Redacted**]

  
 DigitalGlobe Proprietary and Confidential

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

  
 5 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 Table 3.3.13-1 [**Redacted**] 

3.3.14 [**Redacted**] 
 3.3.14.1
[**Redacted**] 
 [**Redacted**] 
 3.3.14.2 [**Redacted**] 
 [**Redacted**] 

3.3.15 [**Redacted**] 
 [**Redacted**]

 3.3.16 [**Redacted**] 
 [**Redacted**] 
 Table 3.3.16-1 [**Redacted**]

 3.3.17 [**Redacted**] 

[**Redacted**] 
 3.3.18 [**Redacted**]

 [**Redacted**] 

3.3.19 [**Redacted**] 
 [**Redacted**]

 3.3.20 [**Redacted**] 

[**Redacted**] 
 3.3.21 [**Redacted**]

 [**Redacted**] 
 Table 3.3.21-1 [**Redacted**] 
 [**Redacted**] 

 
 DigitalGlobe Proprietary and Confidential 

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

  
 6 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 3.3.22 [**Redacted**] 
 [**Redacted**] 
 3.3.23 [**Redacted**] 

[**Redacted**] 
 3.3.24 [**Redacted**]

 [**Redacted**] 

3.3.25 [**Redacted**] 
 [**Redacted**]

 3.3.26 [**Redacted**] 
 [**Redacted**] 
 Table 3.3.26-1 [**Redacted**]

 3.3.27 [**Redacted**] 

[**Redacted**] 
 3.3.28 [**Redacted**]

 [**Redacted**] 

3.3.29 [**Redacted**] 
 [**Redacted**]

 3.3.30 [**Redacted**] 

[**Redacted**] 
 3.3.31 [**Redacted**]

 [**Redacted**] 

3.3.32 [**Redacted**] 
 [**Redacted**]

  
 DigitalGlobe Proprietary and Confidential

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

  
 7 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 Table 3.3.32-1: [**Redacted**] 

[**Redacted**] 
 3.3.33
[**Redacted**] 
 [**Redacted**] 
 3.3.34 [**Redacted**] 
 3.3.34.1 [**Redacted**] 

[**Redacted**] 
 3.3.34.2
[**Redacted**] 
 [**Redacted**] 
 3.3.34.3 [**Redacted**] 
 [**Redacted**] 

3.3.34.4 [**Redacted**] 

[**Redacted**] 
 3.3.34.5
[**Redacted**] 
 [**Redacted**] 
 3.3.34.6 [**Redacted**] 
 [**Redacted**] 

3.3.34.7 [**Redacted**] 

[**Redacted**] 
 3.3.34.8
[**Redacted**] 
 [**Redacted**] 
 3.3.34.9 [**Redacted**] 
 [**Redacted**] 

3.3.34.10 [**Redacted**] 

[**Redacted**] 
  

DigitalGlobe Proprietary and Confidential 
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 8 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 3.3.34.11 [**Redacted**] 
 [**Redacted**] 
 3.3.34.12 [**Redacted**] 

[**Redacted**] 
 3.3.34.13
[**Redacted**] 
 [**Redacted**] 
 3.3.34.14 Reserved 
 3.3.35 [**Redacted**] 

3.3.35.1 [**Redacted**] 

[**Redacted**] 
 3.3.35.2
[**Redacted**] 
 [**Redacted**] 
 3.3.35.3 [**Redacted**] 
 [**Redacted**] 

3.4 [**Redacted**] 
 3.4.1
[**Redacted**] 
 3.4.1.1 [**Redacted**] 
 [**Redacted**] 
 3.4.1.2 Reserved 

3.4.1.3 Reserved 
 3.4.1.4
[**Redacted**] 
 [**Redacted**] 
  

DigitalGlobe Proprietary and Confidential 
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 9 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 3.4.2 [**Redacted**] 
 [**Redacted**] 
 3.4.2.1 [**Redacted**] 

[**Redacted**] 
 3.4.2.2
[**Redacted**] 
 [**Redacted**] 
 3.4.2.3 [**Redacted**] 
 [**Redacted**] 

3.4.3 [**Redacted**] 

a) [**Redacted**] 

3.4.4 [**Redacted**] 
 [**Redacted**]

 3.5 [**Redacted**] 

3.5.1 [**Redacted**] 
 [**Redacted**]

 3.5.2 [**Redacted**] 

[**Redacted**] 
 3.6
[**Redacted**] 
 [**Redacted**] 
 3.6.1 [**Redacted**] 
 [**Redacted**] 

3.6.2 [**Redacted**] 
 [**Redacted**]

 3.6.3 [**Redacted**] 

[**Redacted**] 
  

DigitalGlobe Proprietary and Confidential 
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 10 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 3.7 [**Redacted**] 
 [**Redacted**] 
 3.7.1 [**Redacted**] 

[**Redacted**] 
 3.7.2
[**Redacted**] 
 [**Redacted**] 
 3.8 [**Redacted**] 
 [**Redacted**] 

3.8.1 [**Redacted**] 
 [**Redacted**]

 3.8.2 [**Redacted**] 

[**Redacted**] 
 3.8.3 [**Redacted**]

 3.8.3.1 [**Redacted**] 

[**Redacted**] 
 3.8.3.2 Reserved

 a) 
 3.8.4
[**Redacted**] 
 [**Redacted**] 
 3.8.5 [**Redacted**] 
 [**Redacted**] 

Table 3.8.5-1 [**Redacted**] 
 3.9 [**Redacted**] 
 3.9.1 [**Redacted**] 

[**Redacted**] 
  

DigitalGlobe Proprietary and Confidential 
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 11 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 3.9.2 [**Redacted**] 
 [**Redacted**] 
 3.10 [**Redacted**] 

[**Redacted**] 
  

DigitalGlobe Proprietary and Confidential 
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 12 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 [Table 3.9.2-1 [**Redacted**] 

[**Redacted**] 
  

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 13 

			
	

	  	 WV-3 CAVIS-ACI Specification
 Rev 4.0

  

 3.11 [**Redacted**] 
 [**Redacted**] 
 3.11.1 [**Redacted**] 

[**Redacted**] 

3.11.2 [**Redacted**] 
 [**Redacted**]

 3.11.3 [**Redacted**] 

[**Redacted**] 
 3.11.4 [**Redacted**]

 [**Redacted**] 

3.11.5 [**Redacted**] 
 [**Redacted**]

  
 DigitalGlobe Proprietary and Confidential

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 14 

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THE SECURITIES AND EXCHANGE COMMISSION 
 WorldView-3 

Spacecraft Simulator Specification 
 Specification 
  

							
		  		  	Document #:	  	10258368
		  		  	 Revision:
	  	5.0
		  		  	 Release Date:
	  	October 1, 2012
		  		  	 Prepared By:
	  	Doug Laczkowski
		  		  	 Approved By:
	  	Brian Uzzle

 [**Redacted**] 
 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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EXCHANGE COMMISSION 
  

							
	 Revision History

	 Issue
	  	 Date
	  	 Sections Affected
	  	 Description

	 Initial
	  	Dec 20, 2010	  	[**Redacted**]	  	
	 Rev 1
	  	Sep 9, 2011	  	[**Redacted**]	  	
	 Rev 2
	  	Sep 23, 2011	  	[**Redacted**]	  	
	 Rev 3
	  	Oct 24, 2011	  	[**Redacted**]	  	
	 Rev 4
	  	Dec 9, 2011	  	[**Redacted**]	  	
	 Rev 5
	  	Sep 13, 2012	  	[**Redacted**]	  	
	 Rev 6
	  	TBD	  	[**Redacted**]	  	

  
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EXCHANGE COMMISSION 
  

 1. SCOPE 
 1.1 WorldView Spacecraft Simulator (WVSS) General Overview 
 The WorldView system will collect
and process imagery of the Earth to support the commercial development and distribution of image products. The flight segment of the WorldView system consists of a spacecraft and an imaging instrument. The spacecraft and the instrument are under the
management of DigitalGlobe. The WorldView ground segment consists of remote ground stations and a single mission control facility that provides commanding capability, and data archival and distribution facilities. 

[**Redacted**] 
 1.2 WVSS Purpose

 [**Redacted**] 
  

	 	•	 	 [**Redacted**] 

[**Redacted**] 
  

	 	•	 	 [**Redacted**] 

[**Redacted**] 
  

	 	•	 	 [**Redacted**] 

[**Redacted**] 
  

	 	•	 	 [**Redacted**] 

[**Redacted**] 
  

	 	•	 	 [**Redacted**] 

[**Redacted**] 
 1.3 Document
Overview 
 This document specifies functional, performance and interface requirements for the integrated Spacecraft Simulator, including
simulator external model interfaces. Separate Interface Control Documents (ICDs) detail the specifics of the Spacecraft Simulator-External Model interfaces. Satisfaction of the Satellite simulator-level requirements contained in this specification
assume the External Model simulators provided as CFE meets its requirements, which are documented separately. 
 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. 
  

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	 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.

 

	
	 2.1 [**Redacted**]

 

	
	 2.2 [**Redacted**]

 

	
	 2.2.1 [**Redacted**]

 

	
	[**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. 

 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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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 
  

																	
	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**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. 

 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 
  

																	
	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**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. 

 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 
  

																	
	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**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. 

 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 
  

																	
	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**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. 

 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 
  

																	
	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]	  	[**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. 

 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 
  

					
	 Table 1. [**Redacted**]

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	  	[**Redacted**]	  	[**Redacted**]
		  	[**Redacted**]	  	[**Redacted**]
		  	[**Redacted**]	  	[**Redacted**]

  
 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 
  

					
	 [**Redacted**]
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		 	[**Redacted**]	 	[**Redacted**]

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

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REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND 

EXCHANGE COMMISSION 
  

					
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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.

 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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 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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 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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 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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 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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 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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 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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 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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 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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 Amendment No. 8 
 To the 
 WorldView3 Satellite Purchase Agreement #60150 

This Amendment No. 8 (“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 &
Technology 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 WorldView3 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 021: Documentation Updates 

 This
change updates 1 specification 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 1-2 to the Agreement. 
  

	 	a.	Exhibit 1 to the Agreement, titled “Statement of Work for the WorldView 3 Satellite-10329656, Rev 5.0,” and dated 14 December 2011, is replaced in its
entirety by the updated version “Statement of Work for the WorldView 3 Satellite- 10329656, Rev 6.0,” dated 6 December 2012, included as Attachment 1 to this Amendment; and 

 

	 	b.	Exhibit 3 to the Agreement, titled “WorldView 3 Payment Milestone Schedule-10329669, Rev 6.0” and dated 1 October 2012, is replaced in its entirety by
the updated version “WorldView 3 Payment Milestone Schedule- 10329669, Rev 7.0,” dated 29 Nov 2012, included as Attachment 2 to this Amendment. 

  

	2.	ECP 022: [**Redacted**]. 

[**Redacted**]. 
  

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 [**Redacted**]. 
 SUMMARY 
 The value for these ECPs is $60,000, outlined in the following table: 

 

							
	 Change#
	  	Change Description	  	$	 	  
	 021
	  	Documentation Updates	  	$	0.00	  
	 022
	  	[**Redacted**]	  	$	[**Redacted**]	  
		  	TOTAL	  	$	60,000.00	  

 Contract Value Summary 
  

					
	 Previous Contract Value
	  	$	217,762,399.00	  
	 ECPs
	  	$	60,000.00	  
	 New Contract Value
	  	$	217,822,399.00	  

 Unless otherwise expressly provided herein, all other terms and conditions of the Agreement shall remain in full force
and effect. 
 This Amendment No. 8 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**]
	 		  	 [**Redacted**]

	Signature	 		  	Signature
			
	 [**Redacted**] 
	 		  	 [**Redacted**] 

	Name	 		  	Name
			
	 [**Redacted**] 
	 		  	 [**Redacted**]

			
	 [**Redacted**] 
	 		  	 [**Redacted**]

  
  
  
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Exhibit 1 to Agreement 60150 
 Statement of Work 
 for the WorldView 3 

Satellite 
  

			
	Document Number	  	10329656
	Release Date:	  	Dec 6, 2012
	Issue/Revision:	  	Release 6.0
	Prepared by:	  	Brian Uzzle
	Approved by	  	Steve Linn

  

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 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. 
  
 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 

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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,	  	Changed launch vehicle baseline from Delta-2 to Atlas V.
		  		  	4.5.3.2.F,	  	Changed number of TIMs from 8 to 20.
		  		  	[**Redacted**],	  	Changed SLRR from [**Redacted**] to [**Redacted**].
		  		  	11.4, 12.1, 12.2,12.3, Attachment 2	  	
		  		  	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**]

  

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	 Issue
	  	 Date
	  	 Section(s)
	  	 Description of Change

		  		  	Attachment 1	  	Added [**Redacted**] and CGSE-16. Changed [**Redacted**]
		  		  	n/a	  	Added Table of Contents
	Rev 4	  	24 Oct 2011	  	[**Redacted**]	  	
	Rev 5	  	14 Dec 2011	  	[**Redacted**]	  	
	Rev 6	  	6 Dec 2012	  	[**Redacted**]	  	

  

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 Table of Contents 

 

							
	 1.0
	 	INTRODUCTION	  	 	1	  
	     1.1
	 	    DEFINITIONS	  	 	1	  
	     1.2
	 	    PROGRAM OVERVIEW	  	 	2	  
	 2.0
	 	DOCUMENTS	  	 	3	  
	     2.1
	 	    APPLICABLE DOCUMENTS	  	 	3	  
	     2.2
	 	    REFERENCE DOCUMENTS	  	 	5	  
	 3.0
	 	CONTRACT DELIVERABLES	  	 	6	  
	     3.1
	 	    DELIVERABLE ITEMS	  	 	6	  
	     3.2
	 	    DELIVERABLE DATA	  	 	7	  
	     3.3
	 	    DELIVERABLE SERVICES	  	 	7	  
	 4.0
	 	PROGRAM MANAGEMENT	  	 	8	  
	     4.1
	 	    PROGRAM PHILOSOPHY	  	 	8	  
	     4.2
	 	    BATC ORGANIZATION (CDIL PM-1)	  	 	8	  
	     4.3
	 	    DIGITALGLOBE MANAGEMENT	  	 	8	  
	     4.4
	 	    SPACE SEGMENT MASTER PROGRAM SCHEDULE (MPS) (CDIL PM-2)	  	 	9	  
	         4.4.1
	 	      General	  	 	9	  
	         4.4.2
	 	      Required Software	  	 	9	  
	         4.4.3
	 	      MPS Construction	  	 	10	  
	         4.4.4
	 	      Reports	  	 	10	  
	     4.5
	 	    MEETINGS & REVIEWS	  	 	10	  
	         4.5.1
	 	      Weekly Status Meeting	  	 	10	  
	         4.5.2
	 	      Monthly Program Status Review	  	 	11	  
	         4.5.3
	 	      Program Reviews	  	 	11	  
	         4.5.4
	 	      Component/Subsystem Design Review Listing (CDIL PM-3)	  	 	13	  
	         4.5.5
	 	      Component/Subsystem Test Readiness / Data Review Listing [(CDIL PM-4)]	  	 	14	  
	         4.5.6
	 	      DigitalGlobe Meetings	  	 	14	  
	     4.6
	 	    DOCUMENTATION MANAGEMENT	  	 	14	  
	         4.6.1
	 	      Access to Program Technical Data	  	 	14	  
	         4.6.2
	 	      Objective	  	 	14	  
	         4.6.3
	 	      Documentation Listing (CDIL PM-5)	  	 	15	  
	         4.6.4
	 	      Documentation Delivery	  	 	15	  
	     4.7
	 	    ACTION ITEM TRACKING (CDIL PM-6)	  	 	15	  
	     4.8
	 	    FINANCIAL MANAGEMENT	  	 	16	  
	         4.8.1
	 	      Historical Record of Payments (CDIL PM-7)	  	 	16	  
	         4.8.2
	 	      Payments Forecast (CDIL PM-7)	  	 	16	  
	     4.9
	 	    CONTRACT CHANGE CONTROL	  	 	16	  
	 5.0
	 	DESIGN	  	 	17	  
	     5.1
	 	    GENERAL	  	 	17	  
	     5.2
	 	    WORKING GROUPS AND TRADE STUDIES	  	 	17	  
	         5.2.1
	 	      Working Groups	  	 	17	  

  

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	         5.2.2
	 	      Trade Studies	  	 	17	  
	     5.3
	 	    SATELLITE DESIGN DATA	  	 	17	  
	         5.3.1
	 	      Satellite to Instrument Interface Control Document(s) (CDIL D-1)	  	 	17	  
	         5.3.2
	 	      Satellite to Ground Terminal Narrowband Link ICD (CDIL D-2)	  	 	17	  
	         5.3.3
	 	      Satellite to Ground Terminal Wideband Link ICD (CDIL D-3)	  	 	17	  
	         5.3.4
	 	      Satellite Environmental Design and Test Specification (EDTS) (CDIL D-4)	  	 	18	  
	         5.3.5
	 	      Contamination Control Plan(s) (CDIL D-5)	  	 	18	  
	         5.3.6
	 	      Satellite Level Requirements Verification/Compliance Matrix (CDIL D-6)	  	 	18	  
	         5.3.7
	 	      Box Level Requirements Verification/Compliance Matrix (CDIL D-7)	  	 	18	  
	         5.3.8
	 	      Drawings (CDIL D-8)	  	 	19	  
	         5.3.9
	 	      Performance Compliance and Risk Management	  	 	19	  
	         5.3.10
	 	        Subsystem Description Documents (CDIL D-11)	  	 	19	  
	         5.3.11
	 	        Analysis and reports	  	 	20	  
	         5.3.12
	 	        Other Interface Control Documents	  	 	21	  
	         5.3.13
	 	        Critical Items list (CDIL D-18)	  	 	21	  
	         5.3.14
	 	        Component Heritage Summary (CDIL D-19)	  	 	21	  
	         5.3.15
	 	        Engineering Reports (CDIL D-20)	  	 	21	  
	         5.3.16
	 	        Flight Software Source Code (CDIL D-21)	  	 	22	  
	         5.3.17
	 	        Composite Grounding Design (CDIL D-22)	  	 	22	  
	         5.3.18
	 	        Structural, Power, Thermal, and Reliability Analytical Models (CDIL D-23)	  	 	22	  
	         5.3.19
	 	        Coordinate Transformation Document (CDIL D-24)	  	 	22	  
	         5.3.20
	 	        Flight Software Users Manual (CDIL D-25)	  	 	23	  
	         5.3.21
	 	        Component Acceptance Data Package (CDIL D-26)	  	 	23	  
	         5.3.22
	 	        [**Redacted**]	  	 	23	  
	         5.3.23
	 	        Instrument/Sensor Boresight Stability Data (CDIL D-28)	  	 	23	  
	         5.3.24
	 	        Position and Attitude Accuracy (CDIL D-29)	  	 	23	  
	         5.3.25
	 	        Satellite to MGB Interface Control Document(s) (CDIL D-32)	  	 	23	  
	         5.3.26
	 	        DigitalGlobe to BATC Electrical GSE Interface Control Document (CDIL D-33)	  	 	23	  
	 6.0
	 	PRODUCT ASSURANCE	  	 	24	  
	     6.1
	 	    PRODUCT ASSURANCE PLAN	  	 	24	  
	     6.2
	 	    BATC PARTS CONTROL BOARD (PCB)	  	 	24	  
	         6.2.1
	 	Subcontractor Parts Control Board (PCB)	  	 	24	  
	         6.2.2
	 	PCB Process	  	 	24	  
	     6.3 PARTS AND MATERIALS
	  	 	25	  
	         6.3.1
	 	Electrical, Electronic, and Electro-mechanical Parts (EEE) Parts Listing (CDIL QA-1)	  	 	25	  
	         6.3.2
	 	Material and Processes Reports (CDIL QA-2)	  	 	25	  
	     6.4 AS-BUILT CONFIGURATION AND
CONFORMANCE
	  	 	25	  
	         6.4.1
	 	As-Built Configured Article List (CDIL QA-3)	  	 	25	  
	         6.4.2
	 	Certificate of Conformance (CDIL QA-4)	  	 	25	  
	     6.5 PRODUCT ASSURANCE REVIEWS (CDIL
QA-5)
	  	 	26	  
	     6.6 DOCUMENTATION
	  	 	26	  

  

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	     6.7
	 	KNOWN NON-COMPLIANT HARDWARE	  	 	26	  
	     6.8
	 	MILITARY STANDARD 461	  	 	26	  
	 7.0
	 	PROCUREMENT	  	 	27	  
	     7.1
	 	    GENERAL	  	 	27	  
	     7.2
	 	    MAKE/BUY PLANS (CDIL PT-1)	  	 	27	  
	     7.3
	 	    [**REDACTED**]	  	 	27	  
	     7.4
	 	    REVIEWS	  	 	27	  
	     7.5
	 	    PROGRAM SUBCONTRACT STATUS REPORT (PSSR) (CDIL PT-2)	  	 	27	  
	     7.6
	 	    DOCUMENTATION	  	 	27	  
	     7.7
	 	    SUBCONTRACT FLOW-DOWNS	  	 	28	  
	         7.7.1
	 	      Assignment Clause	  	 	28	  
	         7.7.2
	 	      Access	  	 	28	  
	 8.0
	 	PRODUCTION ACTIVITIES	  	 	29	  
	     8.1
	 	    GENERAL	  	 	29	  
	     8.2
	 	    PRODUCTION PROCESS	  	 	29	  
	     8.3
	 	    ACCESS	  	 	29	  
	     8.4
	 	    PRODUCTION DOCUMENTATION	  	 	29	  
	 9.0
	 	INTEGRATION AND TEST ACTIVITIES	  	 	30	  
	     9.1
	 	    GENERAL	  	 	30	  
	     9.2
	 	    BOX/SUBSYSTEM LEVEL TESTING	  	 	30	  
	         9.2.1
	 	      General	  	 	30	  
	         9.2.2
	 	      [**Redacted**]	  	 	30	  
	     9.3
	 	    WV BUS AND SATELLITE INTEGRATION AND TEST PLANS
(CDIL PT-3)	  	 	30	  
	     9.4
	 	    POST-SHIPMENT INSTRUMENT TESTING	  	 	30	  
	     9.5
	 	    SUPPORTING DOCUMENTS	  	 	31	  
	     9.6
	 	    SYSTEM TEST REPORTS (CDIL PT-5)	  	 	31	  
	         9.6.1
	 	      Content	  	 	31	  
	         9.6.2
	 	      Timeliness	  	 	31	  
	     9.7
	 	    UNINTERRUPTIBLE POWER SUPPLY (UPS)	  	 	31	  
	     9.8
	 	    DIGITALGLOBE INTEGRATION AND TEST ENGINEERING
ACCESS	  	 	31	  
	         9.8.1
	 	      On-Site and Visiting Engineers	  	 	31	  
	         9.8.2
	 	      Access to Live Satellite Telemetry	  	 	32	  
	         9.8.3
	 	      Test Observation By Other DG Engineers	  	 	32	  
	         9.8.4
	 	      Access to Command and Telemetry Log Files (CDIL PT-6)	  	 	32	  
	     9.9
	 	    TEST REVIEWS	  	 	32	  
	     9.10
	 	    OPTIONAL TESTING	  	 	32	  
	 10.0
	 	CUSTOMER FURNISHED EQUIPMENT AND SERVICES	  	 	33	  
	     10.1
	 	    GENERAL	  	 	33	  
	     10.2
	 	    FLIGHT EQUIPMENT	  	 	33	  
	         10.2.1
	 	      [**Redacted**]	  	 	33	  
	         10.2.2
	 	      [**Redacted**]	  	 	33	  
	         10.2.3
	 	      [**Redacted**]	  	 	33	  

  

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	         10.2.4
	 	      [**Redacted**]	  	 	33	  
	         10.2.5
	 	      [**Redacted**]	  	 	33	  
	         10.2.6
	 	      [**Redacted**]	  	 	33	  
	     10.3
	 	    SIMULATORS (CSIM-1)	  	 	33	  
	     10.4
	 	    LAUNCH VEHICLE INTERFACES	  	 	34	  
	         10.4.1
	 	      Launch Vehicle Interface	  	 	34	  
	         10.4.2
	 	      Launch Vehicle Separation Connectors (CLSE-3)	  	 	34	  
	     10.5
	 	    GROUND SUPPORT EQUIPMENT	  	 	34	  
	         10.5.1
	 	      Wideband Link RGT Equipment	  	 	34	  
	         10.5.2
	 	      Narrowband Link RGT Equipment (CGSE-5)	  	 	34	  
	         10.5.3
	 	      Special Test Equipment	  	 	34	  
	         10.5.4
	 	      Mission Control Center (CGSE-11)	  	 	34	  
	         10.5.5
	 	      [**Redacted**]	  	 	35	  
	         10.5.6
	 	      [**Redacted**]	  	 	35	  
	         10.5.7
	 	      [**Redacted**]	  	 	35	  
	         10.5.8
	 	      MGB Test Equipment (CGSE-15)	  	 	35	  
	         10.5.9
	 	      [**Redacted**]	  	 	35	  
	     10.6
	 	    LAUNCH VEHICLE DATA (CLD-1 AND CLD-2)	  	 	35	  
	     10.7
	 	    INSTRUMENT DATA	  	 	35	  
	         10.7.1
	 	      Instrument Structural Analysis Data (CID-1)	  	 	35	  
	         10.7.2
	 	      Instrument Thermal Analysis Data (CID-2)	  	 	35	  
	 11.0
	 	STORAGE AND DELIVERY	  	 	36	  
	     11.1
	 	    GENERAL	  	 	36	  
	     11.2
	 	    SATELLITE PRE-SHIPMENT STORAGE	  	 	36	  
	     11.3
	 	    PRE-SHIPMENT RE-TEST	  	 	36	  
	     11.4
	 	    SATELLITE SHIPPING AND DELIVERY	  	 	36	  
	     11.5
	 	    SATELLITE LAUNCH SITE STORAGE	  	 	37	  
	 12.0
	 	LAUNCH SUPPORT SERVICES	  	 	38	  
	     12.1
	 	    GENERAL	  	 	38	  
	     12.2
	 	    REQUIREMENT DEFINITION	  	 	38	  
	     12.3
	 	    TECHNICAL INTERCHANGE MEETINGS	  	 	38	  
	     12.4
	 	    FEM AND CLA-TO-DESIGN LOAD COMPARISONS (CDIL LM-2)	  	 	38	  
	     12.5
	 	    EXPORT REGULATIONS	  	 	39	  
	     12.6
	 	    ADAPTER FIT-CHECK	  	 	39	  
	     12.7
	 	    LAUNCH SITE INFRASTRUCTURE	  	 	39	  
	     12.8
	 	    LAUNCH SITE OPERATIONS	  	 	39	  
	     12.9
	 	    FUELING	  	 	40	  
	 13.0
	 	MISSION PREPARATION AND ON-ORBIT COMMISSIONING	  	 	41	  
	     13.1
	 	    TRAINING (CDIL LM-3)	  	 	41	  
	         13.1.1
	 	      Training Materials	  	 	41	  
	         13.1.2
	 	      Training Sessions	  	 	41	  
	     13.2
	 	    COMMAND AND TELEMETRY HANDBOOK (CDIL LM-4)	  	 	41	  

  

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	     13.3
	 	    BUS SUBSYSTEM CALIBRATION TOOLS (CDIL LM-5)	  	 	41	  
	     13.4
	 	    DIGITALGLOBE PROCEDURE DEVELOPMENT SUPPORT	  	 	41	  
	     13.5
	 	    COMMISSIONING PLAN (CDIL LM-6)	  	 	41	  
	     13.6
	 	    ANOMALY PREPARATIONS	  	 	42	  
	     13.7
	 	    SATELLITE COMMISSIONING	  	 	42	  
	         13.7.1
	 	      Launch and Early Operations (LEOP) Phase	  	 	42	  
	         13.7.2
	 	      Verification and Calibration (V&C) Phase	  	 	42	  
	     13.8
	 	    SATELLITE SIMULATOR	  	 	43	  
	         13.8.1
	 	      Satellite Simulator (CDIL LM-8)	  	 	43	  
	         13.8.2
	 	      Documentation (CDIL LM-9)	  	 	43	  
	         13.8.3
	 	      Source Code (CDIL LM-10)	  	 	44	  
	         13.8.4
	 	      Delivery Schedule	  	 	44	  
	         13.8.5
	 	      Technical Interchange Meetings and Design Reviews	  	 	44	  
	     13.9
	 	    MANEUVER PLANNERS	  	 	44	  
	         13.9.1
	 	      [**Redacted**]	  	 	44	  
	         13.9.2
	 	      [**Redacted**]	  	 	44	  
	         13.9.3
	 	      [**Redacted**]	  	 	44	  
	     13.10
	 	    SOFTWARE TEST BENCH	  	 	44	  
	     13.11
	 	    GROUND STATIONS	  	 	45	  
	     13.12
	 	    TELEMETRY PACKET CREATION AND MAPPING TOOLS (CDIL
LM-15)	  	 	45	  
	     13.13
	 	    TELEMETRY MONITOR AND RESPONSE (CDIL LM-16)	  	 	45	  
	 14.0
	 	COMMUNICATIONS FLEXIBILITY AND TT&C DEFINITION	  	 	45	  
	 15.0
	 	FACILITIES	  	 	45	  
	 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**] 
 [**Redacted**] 
 [**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. 
  

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 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
[**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 
 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**]
	[**Redacted**]	  	[**Redacted**]
	WV-3 CDM Plan Addendum	  	
		  	[**Redacted**]

 Associated Contractor Produced Documents 

 

			
	Astrotech Vandenberg Facility Accommodations Manual	  	[**Redacted**]

  
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	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**]

  
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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 2: [**Redacted**] 

Simulator Delivery 3: [**Redacted**] 
 Simulator Delivery 4: [**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** ]. 

  

	 	s.	[**Redacted** ]. 

  

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 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 

  

	 	e.	[**Redacted**] 

  

	 	f.	[**Redacted**] 

 BATC shall appoint a
different individual to be a single point of contact for each of the following: 
  

	 	g.	Various Bus Subsystem Lead Engineers 

  

	 	h.	Launch Vehicle Integration Engineer 

  

	 	i.	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. 

 
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 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. 
 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. 

 
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 4.4.3 MPS Construction 
 4.4.3.1 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 

 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. 
 4.4.3.2 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. 
  

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 4.5.2 Monthly Program Status Review 
 BATC Program Manager shall support a monthly Program Status Review with DigitalGlobe. 
 4.5.3
Program Reviews 
 4.5.3.1 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**] 

  

	 	i.	[**Redacted**] 

  

	 	j.	[**Redacted**] 

  

	 	k.	[**Redacted**] 

  

	 	l.	[**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 

  

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	 	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 

  

	 	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: 

        a. [**Redacted**].  

 
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	 	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**] 
 [**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: 
 [**Redacted**] 

 
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 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 

  

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	 	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. 

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. 

 
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 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. 

 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 

5.2.1.1 [**Redacted**] 
 [**Redacted**] 
 5.2.2 Trade Studies 

[**Redacted**] 
 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, [**Redacted**]. 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. 
  
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 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**] 

  

	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 

  

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 [**Redacted**] 

 

	i.	Operational constraints 

[**Redacted**] 
  

	j.	Fault Protection 

[**Redacted**] 
  

	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) 

  

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 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
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.) 

 
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 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. 

  

	 	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. 

 
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 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). 
  
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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

 6.4.1 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. 
 6.4.2 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. 
  
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 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. 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 [**Redacted**]

 [**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.

  
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 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**] 
 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. 
  
 DigitalGlobe Proprietary and Confidential 
 Use or disclosure of data is
subject to the restriction on the title page of this document. 

  
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 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**] 
  
 DigitalGlobe Proprietary and Confidential 
 Use or disclosure of data is
subject to the restriction on the title page of this document. 

  
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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.f. 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 (MCC) 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. 
  
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 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**] 
 [**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. 
  
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 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. 

 
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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. 
 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. 
  

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 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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 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: 

 
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	 	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: 
  

	 	•	 	 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. 
  
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 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**] 

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**] 
  
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 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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 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	  	

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

  
 Attch 1 - 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 
  

											
	 Data
Item
	  	 Title
	  	 SOW
Ref
	  	 Initial

Submittal
	  	 Updates
	  	 Comments

	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	  	
	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	  	

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

  
 Attch 1 - 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 
  

											
	 Data
Item
	  	 Title
	  	 SOW
Ref
	  	 Initial

Submittal
	  	 Updates
	  	 Comments

	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	  	

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

  
 Attch 1 - 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 
  

											
	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**]	  		  	

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

  
 Attch 1 - 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 
  

											
	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**]	  		  	
		  	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	  	

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

  
 Attch 1 - 5

 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 
  

											
	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	  	13.9.3	  	[**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	  	
	CAVIS-ACI	  		  		  		  		  	
	[**Redacted**]	  	[**Redacted**]	  	4.5.3.1	  	[**Redacted**]	  		  	
	[**Redacted**]	  	[**Redacted**]	  	4.5.3.1	  	[**Redacted**]	  		  	
	[**Redacted**]	  	 [**Redacted**]
	  	4.5.3.1	  	[**Redacted**]	  		  	

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

  
 Attch 1 - 6

 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 
  

											
	[**Redacted**]	  	[**Redacted**]	  	4.5.3.1	  	[**Redacted**]	  		  	
	 [**Redacted**]
	  	[**Redacted**]	  	4.5.3.1	  	[**Redacted**]	  		  	
	 [**Redacted**]
	  	[**Redacted**]	  	4.5.3.11.i	  	[**Redacted**]	  	[**Redacted**]	  	
	 [**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. 
  
 DigitalGlobe Proprietary and Confidential 

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

  
 Attch 1 - 7

 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 
  

 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**]	  	
	[SIMULATORS]	  		  		  		  	
	CSIM-1	  	[**Redacted**]	  	10.3	  	[**Redacted**]	  	 Remains the property of

DG

	[LAUNCH SUPPORT EQUIPMENT]	  		  		  	
	CLSE-1	  	[**Redacted**]	  	10.4.1	  	[**Redacted**]	  	
	CLSE-2	  	[**Redacted**]	  	10.4.1	  	[**Redacted**]	  	
	CLSE-3	  	[**Redacted**]	  	10.4.2	  	[**Redacted**]	  	
	[**Redacted**]	  		  		  		  	

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

  
 Attch 2 - 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 
  

									
	 Item
	  	 Title
	  	 SOW

Ref
	  	 Date
	  	 Comment

	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

  

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

  
 Attch 2 - 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 
  

									
	 Item
	  	 Title
	  	 SOW

Ref
	  	 Date
	  	 Comment

	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

  

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

  
 Attch 2 - 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 
  

									
	 Item
	  	 Title
	  	 SOW

Ref
	  	 Date
	  	 Comment

	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. 

 
 DigitalGlobe Proprietary and Confidential 

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

  
 Attch 2 - 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 
  

 WorldView 3 Payment Milestone Schedule 

Exhibit 3 to WV3 Satellite Agreement # 60150 
  

													
	 Item
#
	  	 Invoice Date
	  	Line
Item	  	 Description
	  	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**]	  	
		  		  	a	  	[**Redacted**]	  	[**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**]	  		  	

 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 
  

													
	10	  	[**Redacted**]	  		  	Milestone 10 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	10a	  	[**Redacted**]	  	[**Redacted**]	  		  	[**Redacted**]
		  		  	10b	  	[**Redacted**]	  	[**Redacted**]	  		  	
		  		  	10c	  	[**Redacted**]	  	[**Redacted**]	  		  	
		  		  	10d	  	[**Redacted**]	  	[**Redacted**]	  		  	
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 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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 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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	29	  	[**Redacted**]	  		  	Milestone 29 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
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 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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	38	  	[**Redacted**]	  		  	Milestone 38 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
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	40	  	[**Redacted**]	  		  	Milestone 40 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
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		  		  	40e	  	[**Redacted**]	  	[**Redacted**]	  		  	

 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 
  

													
	41	  	[**Redacted**]	  		  	Milestone 41 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
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	42	  	[**Redacted**]	  		  	Milestone 42 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
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	44	  	[**Redacted**]	  		  	Milestone 44 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
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	45	  	[**Redacted**]	  		  	Milestone 45 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	45a	  	[**Redacted**]	  	[**Redacted**]	  		  	
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	46	  	[**Redacted**]	  		  	Milestone 46 Total Value	  	[**Redacted**]	  	[**Redacted**]	  	[**Redacted**]
		  		  	46a	  	[**Redacted**]	  	[**Redacted**]	  		  	
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		  		  	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	  	$217,822,399	  	$217,822,399	  	$217,822,399EX-10.6.2

 Exhibit 10.6.2 
 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 
 Modification #13 
 ([**Redacted**] Bid
#10-351c;11-433;11-529;11-545;11-521) 
 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 1601Dry 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: 
  

	•	Bid 10-351c [**Redacted**] 

  

	•	Bid #11-545 [**Redacted**] 

  

	•	Bid #11-433- [**Redacted**] 

  

	•	Bid #11-237 – [**Redacted**] 

  

	•	Bid #11-521- [**Redacted**] 

  

	•	Acceptance of Technical Instrument Specification Revision #6 dated 10/31/2011 

 

	•	Acceptance of the Statement of Work Rev #5 

  

							
	 Original Contract Value
	  	[**Redacted**]	  	$	140,688,933	  
	 This Modification
	  	[**Redacted**]	  	$	26,818,000	  
	 Adjusted TOTAL Contract Value
	  		  	$	167,506,933	  

 Subject to establishment of a mutually agreed upon milestone payment schedule. 

This modification will be incorporated in the master program schedule. The ending period of performance for the overall WV3 Program remains unchanged.
Current WV3 Program delivery is [**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 s hall be a binding agreement. 

 

							
	ITT Space Systems, LLC	 		  	DigitalGlobe, Inc.	  	
				
	 /s/ [**Redacted**]
 Signature
	 		  	 /s/ Yancey L. Spruill
 Signature
	  	
	 [**Redacted**]

[**Redacted**]
	 		  	 Name: Yancey L. Spruill
 Title: Chief Financial Officer

	Date: 13 December 2011	 		  	Date: 13 December 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 
  

 Modification #14 (Proposal #12-22) 

[Redacted] 

To 
 Firm Fixed
Price Agreement No. 60151 
 This Modification updates the Statement of Work dated August 18,2010; Attachment entitled :
[**Redacted**], under contract 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 1601Dry
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 Statement of Work as follows: 

Adding of Addendum #2 identified as ITT proposal #12-022 dated February 29, 2012 including all assumptions and exceptions as stated in the amount of
$220,000.00. This effort will be incorporated in the current WV3 program scheduled delivery date of [**Redacted**] per the Contract Instrument Purchase Agreement dated August 24, 2010. 

 

							
	 Original Contract Value
	  	[**Redacted**]	  	$	167,506,933	  
	 This Modification
	  	[**Redacted**]	  	$	220,000	  
	 Adjusted TOTAL Contract Value
	  		  	$	167,726,933	  

 The following milestone payment schedule for this effort is accepted as follows: 

[**Redacted**] 
 All
other terms and conditions of the Agreement not noted as changed herein remain in full force and effect. 

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EXCHANGE COMMISSION 
  

 Modification #14 – [**Redacted**] Proposal #12-022 

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. 
  

	 Date: 
	                     

  

							
	ITT Space Systems, LLC	 		  	DigitalGlobe, Inc.	  	
				
	 /s/ [**Redacted**]
 Signature
	 		  	 /s/ *Neal T. Anderson
 Signature
	  	
	 [**Redacted**]

[**Redacted**]
	 		  	 Name: Neal T. Anderson

Title: *VP, Technology Development
	  	
	Date: 9 May 2012	 		  	Date: 9 May 2012	  	

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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 
  

 Modification #16 

(Technical Specifications- Revision #7) 
 To 
 Firm Fixed Price Agreement No.60161 

This Modification to the Firm Fixed Price Agreement No. 60151 (the “Agreement”) is entered into by and between DigitalGlobe
(“Customer”), with a place of business at 1601Dry Creek Drive, Suite 260, Longmont, Colorado 80503; and ITT Space Systems, LLC (“Contractor’’), with a place of business at 1447 St. Paul Street, P.O. Box 60488, Rochester, New
York 14606-0488/ 
 WHEREAS, the Customer and Contractor entered into the Agreement effective September 7th, as amended. 

WHEREAS, the Customer and Contractor agree to amend the Agreement. 
 NOW THEREFORE, in consideration of the mutual covenants contained herein and other good and valuable consideration, Customer and Contractor agree as follows: 

 

	 	1.	To remove WorldView-3 Instrument Specification, Revision 6, Document #10329742 in its entirety and replace it with the WorldView-3 Specification, Revision 7, Document
#10329742, attached hereto. 

 All other terms and conditions of the Agreement shall remain in full force and effect. 

IN WITNESS WHEREOF, the Parties have executed this Amendment in duplicate to be effective as of the Effective Date. 

 

							
	ITT Space Systems, LLC	 		  	DigitalGlobe, Inc.	  	
				
	 /s/ [**Redacted**]
 Signature
	 		  	 /s/ Neal T. Anderson
 Signature
	  	
	 [**Redacted**]

[**Redacted**]
	 		  	 Name: Neal T. Anderson

Title: VP, Technology Development
	  	
	Date: 10 September 2012	 		  	Date: 7 September 2012	  	

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WorldView-3 Instrument 
 Specification 
  

			
	Document #	 	10329742
	Revision #	 	7.0
	Release Date	 	19 July 2012
	Prepared by	 	Paul Scott
	Approved by	 	Keith Constantinides
	[**Redacted**]

 RESTRICTION ON USE, PUBLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION 

This document contains information proprietary and confidential to DigitalGlobeTM, 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. 

 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 
  

 Change Record 

 

							
	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

	1.0	  	8/24/2010	  	All	  	Initial Release
	2.0	  	9/23/2010	  	 2.2.2
  

 
 3.1.4

3.3.1
	  	 Eliminated reference to Nextview on Contamination Control Implementation Plan for WV-3 and replaced TBD with document number. Added WV-3
SSS 1553 Command List to Contractor Documents list.
 Change [**Redacted**]
 Changed [**Redacted**]

				
		  		  	 3.3.11.1
 3.3.11.3
 3.3.11.4

3.3.11.5

3.3.12.2
	  	 Decreased [**Redacted**]

Increased [**Redacted**]
 Changed number
[**Redacted**]
 Dropped [**Redacted**]
 Increased [**Redacted**]

				
		  		  	3.3.12.3	  	[**Redacted**]
				
		  		  	3.4.1.2	  	[**Redacted**]
				
		  		  	 3.4.2.3
 3.4.3.1
	  	 Added TBR [**Redacted**]

Maximum [**Redacted**]

				
		  		  	3.4.4.3	  	Added TBR [**Redacted**]
				
		  		  	3.5.2	  	States and state [**Redacted**]
				
		  		  	3.6.3	  	 Replaced previous paragraph with reference [**Redacted**]
 Added TBR [**Redacted**]

		  		  	3.7.1.4	  
				
		  		  	3.9.7	  	[**Redacted**]
				
		  		  	3.9.11.4.1	  	Eliminated [**Redacted**]
				
		  		  	4.7	  	Removed the A from 3.4.2.1, 3.4.2.2, and 3.4.2.3. Added T to 3.4.2.2, 3.4.2.3, 3.9.11.1.3.1 and 3.9.11.1.3.2. Removed T from
3.5.4.1.

  

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

  
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REQUEST FOR CONFIDENTIAL TREATMENT FILED SEPARATELY WITH THE SECURITIES AND 

EXCHANGE COMMISSION 
  

							
	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

	3.0	  	1/14/2011	  	2.2.3	  	[**Redacted**]
				
		  		  	3.1.1	  	Changed block diagram to include [**Redacted**]
				
		  		  	 3.1.4
  

3.2.2.2
  

3.2.2.3
  

3.2.2.4

3.3.7

3.3.11.5
	  	 Change [**Redacted**]
  

Added [**Redacted**]
  
 Revised [**Redacted**]
  

Added word “Any” to beginning of d)

Revised [**Redacted**]
 Revised
[**Redacted**]

				
		  		  	 3.4.2.3
 3.4.4.1
 3.4.4.3

 
 3.5.2

 
 3.6.3

 
 3.7.1.4
	  	 Removed [**Redacted**]

Replaced [**Redacted**]
 Removed TBR,
[**Redacted**]
  
 Removed TBR [**Redacted**]

 
 Removed TBR [**Redacted**]

 
 Remove TBR and [**Redacted**]

				
		  		  	 3.9.10
 3.9.11.1.8
 3.9.11.2

3.9.11.4.1

3.9.11.17.3

4.6.5.8.1
	  	 Reworded [**Redacted**]

Included [**Redacted**]
 Revised
[**Redacted**]
 Deleted [**Redacted**]
 Corrected [**Redacted**]
 Added entry to [**Redacted**]

				
		  		  	 4.6.5.10
  

4.6.5.10.1
	  	 Made this section a title only and put content into new 4.6.5.10.1

 
 Added this section to include content from previous 4.6.5.10 and [**Redacted**].
Corrected [**Redacted**].

				
		  		  	 4.6.5.10.2
 4.7
	  	 New paragraph entitled [**Redacted**]
 Changed entry in [**Redacted**]

  

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

  
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EXCHANGE COMMISSION 
  

							
	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

	4.0	  	5/4/2011	  	 2.1.1
 2.2.1
	  	 Changed [**Redacted**]

Added [**Redacted**]

				
		  		  	 2.3
 3.2.2.2
 3.3.9 and its subparagraphs

3.4.3.1

3.5.5
	  	 Clarified that this document is obsolete.
 Inserted word [**Redacted**]
 New content replacing Reserved

Minor [**Redacted**]
 Deleted reference to
removed section [**Redacted**]

				
		  		  	 3.9.4.3
 3.9.11.2
	  	 Deleted section
 Added new
entry to [**Redacted**]

				
		  		  	3.9.11.3.1	  	Added words [**Redacted**]
				
		  		  	 3.9.11.4.4
 3.9.11.4.5
 3.9.11.10

3.9.11.11

3.9.11.15.1

3.9.11.15.4
  

3.9.11.15.5

3.9.11.15.6

3.9.11.17

3.9.11.17.1

3.9.11.17.2

3.9.11.17.3

4.6.5.7.3

4.6.5.9
	  	 Replaced section with reference to ICD
 Replaced section with reference to ICD
 Changed title to remove [**Redacted**]

Deleted content, changed title to Reserved

Changed [**Redacted**]
 Added sentence
requiring DG approval for non-standard parts. Removed sentence regarding mission non-critical parts
 Clarified “plastic parts” to mean
plastic encapsulated electronic parts.
 Extensively revised.
 Extensively revised.
 Removed first sentence. Added [**Redacted**] to second
sentence
 Removed first sentence.

Removed first sentence.
 Added 2 sentences at
end.
 Modified wording of first paragraph to [**Redacted**]

				
		  		  	4.6.5.10.1	  	Added clarification to performance parameters [**Redacted**]
				
		  		  	 4.6.5.10.2
 4.6.5.12
	  	 Retitled and revised [**Redacted**]
 Changed title and text [**Redacted**]

				
		  		  	4.7	  	Updated verification matrix due to other changes. [**Redacted**]

  

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

  
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EXCHANGE COMMISSION 
  

							
	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

	5.0	  	10/10/2011	  	3.3.9.7	  	Increased value to [**Redacted**]
				
		  		  	3.3.9.8	  	Increased [**Redacted**]
				
		  		  	3.3.9.10	  	Refined voltage range [**Redacted**]. Changed section title.
				
		  		  	 3.3.12.10
 3.4.1.1
	  	 Corrected and clarified wording of specification
 Clarification added to [**Redacted**]

				
		  		  	3.4.1.2	  	Updated [**Redacted**]
				
		  		  	3.4.1.3	  	New section for [**Redacted**]
				
		  		  	 3.9.11.1.5
 3.9.11.1.7
 3.9.11.2
	  	 Changed [**Redacted**]

Changed [**Redacted**]
 Removed
[**Redacted**]

				
		  		  	3.9.11.3.1	  	Added [**Redacted**]
				
		  		  	3.9.11.1.11.2	  	Changed [**Redacted**]
				
		  		  	 3.9.11.10
 4.6.5.7.2
 4.6.5.10.2
	  	 Added further clarifications [**Redacted**]. Retitled.
 Specified workmanship testing [**Redacted**].
 Extensive re-write to account for the
[**Redacted**]

		  		  	4.7	  	Added entry for new paragraph 3.4.1.3 [**Redacted**]

  

DigitalGlobe Proprietary and Confidential 
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EXCHANGE COMMISSION 
  

							
	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

	6.0	  	10/31/2011	  	Global	  	Labeled requirements that refer only to the main instrument only as Main and those [**Redacted**]
				
		  		  	3.1.1	  	Added new information about [**Redacted**]
				
		  		  	 3.2.1.4
  

3.2.1.12

3.2.1.13

3.2.1.14

3.2.2.2

3.2.2.3

3.3

3.4.1.2

3.4.3

3.4.3.1

3.5.1

3.5.2

3.5.3

3.5.4.1

3.5.4.2

3.6.1

3.9.1.1

3.9.1.2

3.9.7

3.9.11.2

3.9.11.3.1

3.9.11.5
 3.10 and
all subparagraphs
 4.6.5.8.1
 4.6.5.8.4
 4.6.5.10.3
	  	 Added requirement to cover [**Redacted**]
 Changed table to include [**Redacted**]
 Added TBD purge fitting for
[**Redacted**]
 New paragraph for [**Redacted**]
 New paragraph for [**Redacted**]
 Minor updates to account for
[**Redacted**]
 Minor updates to account for [**Redacted**]
 Text added to clarify scope of section with regard to Main and [**Redacted**]
 Modified to
account for [**Redacted**]
 Modified to accunt for [**Redacted**]
 Modified to account for [**Redacted**]
 Modified to account for
[**Redacted**]
 Modified to account for [**Redacted**]
 Modified to account for [**Redacted**]
 Modified to account for
[**Redacted**]
 Modified to account for [**Redacted**]
 Modified to account for [**Redacted**]
 Modified to account for
[**Redacted**]
 Modified to account for [**Redacted**]
 Modified to account for [**Redacted**]
 Modified to account for
[**Redacted**]
 Modified to account for [**Redacted**]
 Modified to account for [**Redacted**]
 New requirements added for
[**Redacted**]
  
 Modified to account for
[**Redacted**]
 Modified to account for [**Redacted**]
 New [**Redacted**]

				
		  		  	4.7	  	Supplemented to account for [**Redacted**].

  

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EXCHANGE COMMISSION 
  

							
	 Revision
	  	 Date
	  	 Sections
	  	 Description of Change

	7.0	  	7/19/2012	  	 Throughout
  

2.2.1
 2.2.1,
3.3.9.1, 3.3.9.3, 3.3.9.4, and 3.3.9.6
 3.2.1.12
 3.2.1.13
	  	 Fixed formatting errors introduced by Word version change.
 Added Reference for [**Redacted**]
 Changed title of [**Redacted**]

 
 Removed TBD and [**Redacted**]

 
 Corrected nominal [**Redacted**]

				
		  		  	 3.2.2.2
 3.3.8
 3.3.9.4.1
	  	 Removed (TBR) in item d.

Removed paragraph [**Redacted**]
 Changed
[**Redacted**]

				
		  		  	 3.3.9.4.2
  

3.3.11.5
  

3.3.12.2
  

3.3.12.3

3.4.1.3

3.5.2
	  	 Changed [**Redacted**]
  

Deleted [**Redacted**]
  
 Extensively revised to [**Redacted**]
  
 Clarified applicability [**Redacted**]
 Add exception (c) [**Redacted**]

Changed terminology in Tables [**Redacted**]

				
		  		  	 3.5.4.1
  

3.5.5
  

3.8.4

3.10.3

3.9.11.2
  

 
 3.9.11.3.1

3.10.1

3.10.9.6
	  	 Modified paragraph to refer to new [**Redacted**]

 
 Separated Operating Cycle requirements for Main and 

[**Redacted**]
 Added
[**Redacted**]
 Corrected typo. Changed [**Redacted**]
 Clarified definition of Max Operational Range of 
 [**Redacted**]. Removed TBRs for
max operational and
 survival temperatures [**Redacted**]
 Changed to allow for new [**Redacted**]
 Changed table reference from 3.3.11-2 to
3.10.10-1.
 Relaxed tolerance on [**Redacted**]

				
		  		  	3.10.12	  	Added [**Redacted**]
				
		  		  	 4.6.5.7.2
 4.7
	  	 Added “no greater than” to sweep rate.
 Added lines for new items omitted from Rev. 6.0 and fixed formatting issues.

  

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 Table of Contents 

 

					
	 1. Scope
	  	 	1	  
		
	 1.1 Purpose
	  	 	1	  
		
	 1.2 System Overview
	  	 	1	  
		
	 1.3 Document Overview
	  	 	1	  
		
	 2. Applicable Documents
	  	 	1	  
		
	 2.1 Government Documents
	  	 	2	  
		
	 2.1.1 Specifications
	  	 	2	  
		
	 2.1.2 Standards
	  	 	2	  
		
	 2.1.3 Handbooks
	  	 	2	  
		
	 2.2 Non-Government Documents
	  	 	2	  
		
	 2.2.1 DigitalGlobe Documents
	  	 	3	  
		
	 2.2.2 Contractor Documents
	  	 	3	  
		
	 2.2.3 Satellite Integrating Contractor Documents
	  	 	3	  
		
	 2.2.4 Other Documents
	  	 	3	  
		
	 2.3 Reference Documents
	  	 	3	  
		
	 3. Requirements
	  	 	4	  
		
	 3.1 Definitions
	  	 	4	  
		
	 3.1.1 Instrument System Definition
	  	 	4	  
		
	 3.1.2 Instrument Data Definitions
	  	 	4	  
		
	 3.1.3 Instrument Detector and Pixel Definitions
	  	 	4	  
		
	 3.1.4 Nominal Mission Orbit
	  	 	5	  
		
	 3.2 Mechanical
	  	 	5	  
		
	 3.2.1 Physical, Structural and Mechanical Requirements
	  	 	5	  
		
	 3.2.2 Thermal
	  	 	7	  
		
	 3.3 Main Optical
	  	 	8	  
		
	 3.3.1 Field of View
	  	 	8	  
		
	 3.3.2 Coverage
	  	 	8	  
		
	 3.3.3 Distortion Knowledge
	  	 	8	  
		
	 3.3.4 Distortion [**Redacted**]
	  	 	8	  

  

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	 3.3.5 [**Redacted**]
	  	 	8	  
		
	 3.3.6 Geometric Precision – Line of Sight Stability
	  	 	8	  
		
	 3.3.7 On-Orbit [**Redacted**]
	  	 	9	  
		
	 3.3.8 [**Redacted**]
	  	 	9	  
		
	 3.3.9 [**Redacted**]
	  	 	9	  
		
	 3.3.10 [**Redacted**]
	  	 	10	  
		
	 3.3.11 Image Properties
	  	 	11	  
		
	 3.3.12 Radiometry
	  	 	12	  
		
	 3.4 Electrical
	  	 	14	  
		
	 3.4.1 Input Power
	  	 	14	  
		
	 3.4.2 Main Data Compression
	  	 	15	  
		
	 3.4.3 Interface to Mission Data Recorder
	  	 	15	  
		
	 3.4.4 Telemetry
	  	 	16	  
		
	 3.5 Operations
	  	 	16	  
		
	 3.5.1 Image Collection Angles
	  	 	16	  
		
	 3.5.2 States and State Transitions
	  	 	16	  
		
	 3.5.3 Simultaneous Operations
	  	 	17	  
		
	 3.5.4 Overlapping Main + AUX (different start and stop times).Operational Duty Cycle
	  	 	17	  
		
	 3.5.5 Operating Cycles
	  	 	18	  
		
	 3.6 Command and Telemetry
	  	 	18	  
		
	 3.6.1 Command and Telemetry Interface
	  	 	18	  
		
	 3.6.2 Reserved.
	  	 	18	  
		
	 3.6.3 Command Latency
	  	 	18	  
		
	 3.7 Protection
	  	 	19	  
		
	 3.7.1 Power Fault Protection
	  	 	19	  
		
	 3.8 Test and Integration
	  	 	19	  
		
	 3.8.1 Orbit Compatibility
	  	 	19	  
		
	 3.8.2 Stand-Alone Testing
	  	 	19	  
		
	 3.8.3 Instrument Integration and Checkout
	  	 	20	  
		
	 3.8.4 Satellite/Instrument Initialization and Checkout Capabilities
	  	 	20	  

  

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	 3.8.5 Checkout Operations
	  	 	20	  
		
	 3.9 Design and Construction
	  	 	20	  
		
	 3.9.1 Quality Factors
	  	 	20	  
		
	 3.9.2 Availability
	  	 	22	  
		
	 3.9.3 Optical Construction
	  	 	22	  
		
	 3.9.4 Useful Life
	  	 	22	  
		
	 3.9.5 Reserved
	  	 	22	  
		
	 3.9.6 Reserved
	  	 	22	  
		
	 3.9.7 Cleanliness and Contamination Control
	  	 	22	  
		
	 3.9.8 Safety
	  	 	23	  
		
	 3.9.9 Design of Mechanisms
	  	 	23	  
		
	 3.9.10 Computer Resources
	  	 	23	  
		
	 3.9.11 Environmental Design
	  	 	23	  
		
	 3.10 [**Redacted**] Performance Requirements
	  	 	33	  
		
	 3.10.1 [**Redacted**]
	  	 	33	  
		
	 3.10.2 [**Redacted**]
	  	 	33	  
		
	 3.10.3 [**Redacted**]
	  	 	33	  
		
	 3.10.4 Total Field of View
	  	 	33	  
		
	 3.10.5 Distortion Stability
	  	 	33	  
		
	 3.10.6 Geometric Precision – Line of Sight Stability
	  	 	33	  
		
	 3.10.7 On-Orbit Focus Adjustment
	  	 	33	  
		
	 3.10.8 Stray Light Rejection and Internal Light Scattering
	  	 	33	  
		
	 3.10.9 Sensor Spectral Properties
	  	 	33	  
		
	 3.10.10 Line Rates
	  	 	34	  
		
	 3.10.11 Band Selections
	  	 	35	  
		
	 3.10.12 Knowledge of Capture Time
	  	 	35	  
		
	 3.10.13 AUX Modulation Transfer Function
	  	 	35	  
		
	 3.10.14 Signal to Noise Ratio
	  	 	35	  
		
	 3.10.15 Detector Full Well Capacity
	  	 	35	  
		
	 3.10.16 Exposure Optimization
	  	 	35	  

  

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

  
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	 3.10.17 Bit Depth
	  	 	36	  
		
	 3.10.18 No AUX Image Data Compression
	  	 	36	  
		
	 3.10.19 Absolute Radiometric Accuracy
	  	 	36	  
		
	 3.10.20 Noise Equivalent Spectral Radiance
	  	 	36	  
		
	 3.10.21 Quantum Step Equivalent Spectral Radiance
	  	 	36	  
		
	 3.10.22 Operable Pixel
	  	 	36	  
		
	 3.10.23 Inoperable and Out of Specification Pixels
	  	 	37	  
		
	 3.10.24 Banding and Streaking
	  	 	37	  
		
	 3.10.25 Coherent Noise
	  	 	37	  
		
	 3.10.26 Reserved
	  	 	37	  
		
	 3.10.27 Pixel-to-Pixel Crosstalk
	  	 	37	  
		
	 3.10.28 Bright Target Recovery
	  	 	37	  
		
	 3.10.29 Polarization
	  	 	37	  
		
	 3.10.30 Pixel to Pixel Calibration and Stability
	  	 	37	  
		
	 3.10.31 Radiometric Stability
	  	 	37	  
		
	 3.10.32 Image Data Content
	  	 	38	  
		
	 4. Verification
	  	 	38	  
		
	 4.1 Verification Methods
	  	 	38	  
		
	 4.1.1 Test (T)
	  	 	38	  
		
	 4.1.2 Inspection (I)
	  	 	38	  
		
	 4.1.3 Analysis (A)
	  	 	38	  
		
	 4.1.4 Similarity (S)
	  	 	39	  
		
	 4.2 Instrument Level Verification
	  	 	39	  
		
	 4.3 Satellite Level of Verification
	  	 	39	  
		
	 4.4 Unit Level of Verification
	  	 	39	  
		
	 4.5 Reserved
	  	 	39	  
		
	 4.6 Test Program
	  	 	39	  
		
	 4.6.1 Test Connections
	  	 	39	  
		
	 4.6.2 Baseline Performance Tests
	  	 	39	  
		
	 4.6.3 Abbreviated Functional Test
	  	 	40	  

  

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	 4.6.4 Reserved
	  	 	40	  
		
	 4.6.5 Environmental Test
	  	 	40	  
		
	 4.6.6 Main Charge Transfer Efficiency (CTE) Screening
	  	 	42	  
		
	 4.7 Verification Matrix
	  	 	44	  

  

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 List of Tables 

 

					
	 Table 3.2.1-1 [**Redacted**]
	  	 	6	  
		
	 Table 3.2.1-2 [**Redacted**]
	  	 	6	  
		
	 Table 3.3.10-1 [**Redacted**]
	  	 	10	  
		
	 Table 3.3.10-2 [**Redacted**]
	  	 	11	  
		
	 Table 3.3.11-1 [**Redacted**]
	  	 	11	  
		
	 Table 3.3.11-2 [**Redacted**]
	  	 	12	  
		
	 Table 3.3.12-1 [**Redacted**]
	  	 	12	  
		
	 Table 3.3.12-2a [**Redacted**]
	  	 	12	  
		
	 Table 3.3.12-3 [**Redacted**]
	  	 	13	  
		
	 Table 3.3.12-4 [**Redacted**]
	  	 	13	  
		
	 Table 3.4.1-1 [**Redacted**]
	  	 	14	  
		
	 Table 3.4.1-2 [**Redacted**]
	  	 	14	  
		
	 Table 3.4.1-3 [**Redacted**]
	  	 	14	  
		
	 Table 3.4.1-4 [**Redacted**]
	  	 	15	  
		
	 Table 3.4.2-1 [**Redacted**]
	  	 	15	  
		
	 Table 3.5.1-1 [**Redacted**]
	  	 	16	  
		
	 Table 3.5.2-1 [**Redacted**]
	  	 	17	  
		
	 Table 3.5.2-2 [**Redacted**]
	  	 	17	  
		
	 Table 3.5.2-3 [**Redacted**]
	  	 	17	  
		
	 Table 3.5.2-4 [**Redacted**]
	  	 	17	  
		
	 Table 3.5.4-1 [**Redacted**]
	  	 	17	  
		
	 Table 3.5.5-1 [**Redacted**]
	  	 	18	  
		
	 Table 3.9.11-1 [**Redacted**]
	  	 	23	  
		
	 Table 3.9.11-2 [**Redacted**]
	  	 	23	  
		
	 Table 3.9.11-3 [**Redacted**]
	  	 	24	  
		
	 Table 3.9.11-4 [**Redacted**]
	  	 	24	  
		
	 Table 3.9.11-5 [**Redacted**]
	  	 	24	  
		
	 Table 3.9.11-6 [**Redacted**]
	  	 	25	  
		
	 Table 3.9.11-7 [**Redacted**]
	  	 	25	  

  

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	 Table 3.9.11-8 [**Redacted**]
	  	 	26	  
		
	 Table 3.9.11-9 [**Redacted**]
	  	 	26	  
		
	 Table 3.9.11-10 [**Redacted**]
	  	 	26	  
		
	 Table 3.9.11-11 [**Redacted**]
	  	 	28	  
		
	 Table 3.9.11-12 [**Redacted**]
	  	 	28	  
		
	 Table 3.9.11-13 [**Redacted**]
	  	 	29	  
		
	 Table 3.10.9-1 [**Redacted**]
	  	 	34	  
		
	 Table 3.10.9-2 [**Redacted**]
	  	 	34	  
		
	 Table 3.10.10-1 [**Redacted**]
	  	 	34	  
		
	 Table 3.10.14-1 [**Redacted**]
	  	 	35	  
		
	 Table 3.10.16-1 [**Redacted**]
	  	 	35	  
		
	 Table 3.10.20-1 [**Redacted**]
	  	 	36	  
		
	 Table 4.6.5-1 [**Redacted**]
	  	 	41	  
		
	 Table 4.6.5-2 [**Redacted**]
	  	 	42	  
		
	 Table 4.6.6-1 [**Redacted**]
	  	 	43	  

 List of Figures 
  

					
	 Figure 3.1.1-1 [**Redacted**]
	  	 	4	  
		
	 Figure 3.3.12-1 [**Redacted**]
	  	 	13	  
		
	 Figure 3.5.5-1 [**Redacted**]
	  	 	18	  
		
	 Figure 3.9.11-1 [**Redacted**]
	  	 	24	  
		
	 Figure 3.9.11-2 [**Redacted**]
	  	 	24	  
		
	 Figure 3.9.11-3 [**Redacted**]
	  	 	25	  
		
	 Figure 3.9.11-4 [**Redacted**]
	  	 	26	  
		
	 Figure 3.9.11-5 [**Redacted**]
	  	 	26	  
		
	 Figure 3.9.11-6 [**Redacted**]
	  	 	26	  
		
	 Figure 3.9.11-7 [**Redacted**]
	  	 	28	  
		
	 Figure 3.9.11-8 [**Redacted**]
	  	 	28	  
		
	 Figure 4.6.5-1 [**Redacted**]
	  	 	41	  

  

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 1. Scope 
 1.1 Purpose 
 This specification contains the performance requirements for the development
and certification of a WorldView-3 (WV-3) multi-spectral space flight instrument. The Instrument provides digital imagery data for ground processing, to form imagery and information products, and to support government, agricultural, environmental,
and business markets. 
 1.2 System Overview 
 The satellite contains a multispectral imaging Instrument, a Spacecraft Bus, and the subsystems necessary to support all observatory and instrument functions. The Instrument uses a [**Redacted**].

 1.3 Document Overview 
 This
document contains all performance requirements for the Instrument. This document describes instrument-spacecraft interfaces. A separate Instrument Interface Control Drawing (ICD) details the specifics of the interfaces. This specification may
contain requirements that have not been fully defined. These open requirements are indicated by a “TBR” 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 Instrument Specification. This specification defines the technical requirements called out in
the Agreement and Statement of Work (SOW). The Agreement 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 Agreement, the
Statement of Work, this document, and Applicable documents shall govern in this order. 
 At contract signing, the Contamination Control Plan
and Interface Control Documents from heritage DigitalGlobe WorldView satellite programs using the WV110 Instrument shall be considered the baseline release for WV-3, specifically those documents listed under Applicable Documents paragraphs 2.2.2
Contractor Documents and 2.2.3 Satellite Integrating Contractor Documents. It is anticipated that the WV-3 versions of these documents will require few modifications from the WV110 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 WV110 version, which shall no longer be considered an Applicable Document.

  

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 Although the Satellite Integrating Contractor physically maintains the 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 the Satellite Integrating Contractor, the Instrument Contractor, and DigitalGlobe.

 2.1 Government Documents 

2.1.1 Specifications 
  

			
	[**Redacted**]	  	Range Safety User Requirements Manual (Volumes 1 through 7), 1 July 2004
		
	[**Redacted**]	  	Semiconductor Device, General Specification For
		
	[**Redacted**]	  	Stress Corrosion Cracking Control

 2.1.2 Standards 
  

			
	[**Redacted**]	  	Digital Time Division Command/Response Multiplex Data Bus
		
	[**Redacted**]	  	Electrical Grounding Practices for Aerospace Hardware
		
	[**Redacted**]	  	Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment
		
	[**Redacted**]	  	Test Methods Standard Microcircuits
		
	[**Redacted**]	  	Instructions for EEE Parts Selection, Screening, Qualification and Derating
		
	[**Redacted**]	  	Dissimilar Metals
		
	[**Redacted**]	  	Test Method Standard, Destructive Physical Analysis for EEE Parts

 2.1.3 Handbooks 
  

			
	[**Redacted**]	  	Reliability Prediction for Electronic Equipment
		
	[**Redacted**]	  	Electronic Parts, Materials and Processes for Space and Launch Vehicles

 2.2 Non-Government Documents 
  

			
	[**Redacted**]	  	Product Cleanliness Levels and Contamination Control Program
		
	[**Redacted**]	  	Protection of Electrical and Electronic Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices)

  
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 2.2.1 DigitalGlobe Documents 

 

			
	[**Redacted**]	  	WV-3 Space Segment Shutter Control Assembly Specification and ICD
		
	[**Redacted**]	  	WV-3 Secondary Sensor Subsystem Double Design Imaging Sequence

 2.2.2 Contractor Documents 
  

			
	[**Redacted**]	  	ITT NextView Contamination Control and Implementation Plan For WV60 Sensor Subsystem and WV110 Payload
		
	[**Redacted**]	  	ITT Contamination Control and Implementation Plan For WV-3 Payload
		
	[**Redacted**]	  	[**Redacted**]

 2.2.3 Satellite Integrating Contractor Documents 

 

			
	[**Redacted**]	  	Interface Control Document (ICD), [**Redacted**]
		
	[**Redacted**]	  	Interface Control Document (ICD), [**Redacted**]
		
	[**Redacted**]	  	Interface Control Document (ICD), [**Redacted**]
		
	[**Redacted**]	  	Interface Control Document (ICD), [**Redacted**]

 2.2.4 Other Documents 
  

			
	[**Redacted**]	  	Methods of Test, Total Mass and Controlled Volatile Condensable Materials from Outgassing in a Vacuum Environment
		
	[**Redacted**]	  	Cleanrooms and Associated Controlled Environments Part 1: Classification of Airborne Particulates

 2.3 Reference Documents 
  

			
	[**Redacted**]	  	Airborne Particulate Cleanliness Classes in Cleanrooms and Clean Zones (obsolete)

  
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 3. Requirements 
 3.1 Definitions 
 3.1.1 Instrument System Definition 

The Instrument is designed to image reflected solar energy from the Earth’s surface in multiple spectral bands. After collecting the reflected solar
energy, the Instrument converts the photons to digital data using two sets of focal planes and electronics: the Main [**Redacted**]. The Main SSS sends compressed data and the [**Redacted**]. As indicated, some Instrument components
are provided by the Satellite Integrating Contractor as CFE to the Instrument Contractor. 
 All requirements specified herein apply to the
entire Instrument, including both Main and [**Redacted**]. 
 [**Redacted**] 

Figure 3.1.1-1 [**Redacted**] 
 3.1.2 Instrument Data Definitions 
 The following general definitions apply to both Main and
[**Redacted**] 
 3.1.2.1 Image Data 
 Image data is the digital representation of the analog voltage signals generated by photons striking the focal plane. 
 3.1.2.2 Calibration Data 
 Calibration data is the data required to calibrate image
data. This includes sensor characteristics such [**Redacted**] 
 3.1.2.3 Ancillary Data 

Ancillary data includes other parameters such as [**Redacted**] 
 3.1.3 Instrument Detector and Pixel Definitions 
 The following general definitions apply to
both Main and [**Redacted**] 
 3.1.3.1 Detector 
 The smallest independent sensing region on a detector chip that produces photo-charge proportional to the radiant energy (exposure) it receives. 
  
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 3.1.3.2 Detector Column 
 A detector column is a column of detectors used with [**Redacted**] 
 3.1.3.3
Pixel 
 A picture element formed by a detector column used in [**Redacted**]. 

3.1.4 Nominal Mission Orbit 
 For
analyses that require a specific orbit (e.g. [**Redacted**]), the following orbital parameters shall be used: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

  

	 	e)	[**Redacted**] 

 See Section 3.8.1
Orbit Compatibility for the broader range of general orbit compatibility requirements. 
 3.2 Mechanical 

3.2.1 Physical, Structural and Mechanical Requirements 
 The Instrument shall meet the requirements of the [**Redacted**] 
 3.2.1.1 Satellite
Coordinate System 
 The mechanical coordinate system used for the Instrument shall be a [**Redacted**] 

3.2.1.2 EOA Mounted Spacecraft Bus Equipment 
 The EOA shall include mounting features to support the following Spacecraft Bus [**Redacted**] 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

 3.2.1.3 Spacecraft
Bus Mounted Instrument Equipment 
 The Spacecraft Bus will accommodate [**Redacted**] between the Instrument units and
[**Redacted**] 
 3.2.1.4 Instrument Envelope 
 The Instrument shall meet the requirements of the WV-3 Instrument to Spacecraft ICD. 
 All
[**Redacted**] 
  
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 3.2.1.5 Spacecraft Bus to Instrument Interconnections 

The Instrument design shall allow for all necessary [**Redacted**] 
 3.2.1.6 Instrument Mass 
 The Instrument component masses [**Redacted**]

 Table 3.2.1-1 [**Redacted**] 
 3.2.1.7 Center-of-Gravity 
 The Instrument shall meet the requirements of the WV-3
Instrument to Spacecraft ICD. 
 3.2.1.8 Moments-of-Inertia 
 The Instrument shall meet the requirements of the WV-3 Instrument to Spacecraft ICD. 
 3.2.1.9
EOA-Mounted Bus Equipment And CFE Mass 
 The Instrument shall support EOA-mounted bus equipment [**Redacted**] and customer-furnished
equipment [**Redacted**] 
 Table 3.2.1-2 [**Redacted**] 

[**Redacted**] 

3.2.1.10 Instrument Mechanical Interface Motion 
 It shall be possible to calculate the Instrument line of sight motion due to relative motion at the Spacecraft Bus to Instrument mechanical interface, using the Instrument [**Redacted**]

 [**Redacted**] 

3.2.1.11 Instrument Sensitivity to Bus Vibration [**Redacted**] 
 It shall be possible to calculate the Instrument line of sight motion due micro-vibration [**Redacted**] input at the Spacecraft Bus to Instrument mechanical interface, using the Instrument Finite
Element Model (FEM) and line of sight equations delivered to the Satellite Integrating Contractor as defined in the Statement of Work. [**Redacted**] 
 [**Redacted**] 
 3.2.1.12 Purge Fitting 

The Instrument shall accommodate a [**Redacted**] during all stages of instrument and satellite integration, test, shipment, launch site
processing, and while on the launch pad as close to launch as possible, per the WV-3 Instrument to Spacecraft ICD. 
  

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 3.2.1.13 [**Redacted**] 
 The [**Redacted**] 
 3.2.1.14 [**Redacted**] 

The relative alignment between the [**Redacted**] and as well as required to meet all other specifications. 

3.2.2 Thermal 
 3.2.2.1 Thermal
Interfaces 
 The Instrument shall meet the requirements of the WV-3 Instrument to Spacecraft ICD. 

3.2.2.2 EOA Thermal Control 
 All
hardware required for thermal control of the EOA (including [**Redacted**] 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

  

	 	e)	[**Redacted**] 

  

	 	f)	[**Redacted**] 

  

	 	g)	[**Redacted**] 

  

	 	h)	[**Redacted**] 

  

	 	i)	[**Redacted**] 

 [**Redacted**]

 3.2.2.3 EOA Thermal Control to Spacecraft Bus Interfaces 
 The [**Redacted**] interfaces shall be as follows and as further specified in the WV-3 Instrument to Spacecraft ICD: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

  

	 	e)	[**Redacted**] 

  

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 3.2.2.4 Thermal Telemetry 
 Thermal telemetry shall be implemented within the Instrument and processed via the Spacecraft Bus as follows and as further specified in the WV-3 Instrument to Spacecraft ICD: 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

 3.3 Main Optical

 All requirements within this Section apply only to the Main capability. Due to the design implementation, some features provided to meet
these requirements may also provide some benefit to the [**Redacted**] 
 3.3.1 Field of View 

The Instrument shall have [**Redacted**] 
 3.3.2 Coverage 
 The Instrument [**Redacted**] 

3.3.3 Distortion Knowledge 

Distortion is defined as the variation in LOS of any pixel in any array with respect to the center pixel in the pan array, not including uniform
scale changes in the [**Redacted**] 
 3.3.4 Distortion [**Redacted**] 
 The operational distortion [**Redacted**] 
 3.3.5 [**Redacted**] 

The Instrument shall limit [**Redacted**] 
 3.3.6 Geometric Precision – Line of Sight Stability 
 The following requirements are
for the stability of the [**Redacted**]. All requirements are relative to panchromatic pixels. 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

  

	 	e)	[**Redacted**] 

  

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 3.3.7 On-Orbit [**Redacted**] 
 The Instrument shall [**Redacted**] shall be controlled by ground command. 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

  

	 	e)	[**Redacted**] 

  

	 	f)	[**Redacted**] 

  

	 	g)	[**Redacted**] 

 3.3.8 [**Redacted**]

 [**Redacted**] 

[**Redacted**] 
 3.3.9 [**Redacted**]

 The instrument shall include [**Redacted**] 
 3.3.9.1 Functions 
 The [**Redacted**] 

3.3.9.1.1 [**Redacted**] 

[**Redacted**] 
 3.3.9.1.2
[**Redacted**] 
 3.3.9.1.2.1 [**Redacted**] 
 [**Redacted**] 
 3.3.9.1.2.2 [**Redacted**] 

[**Redacted**] 
 3.3.9.2 Redundancy

 The shutter mechanism shall be [**Redacted**] 
 3.3.9.3 Fail Safe 
 In addition [**Redacted**] 

 
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 3.3.9.4 Actuation Time 
 3.3.9.4.1 [**Redacted**] 
 [**Redacted**] 

3.3.9.4.2 [**Redacted**] 

[**Redacted**] 
 3.3.9.5 Operating
Cycles 
 The shutter mechanism shall be designed to meet the requirements [**Redacted**] 

3.3.9.6 Telemetry 
 The shutter
mechanism shall provide a primary and a [**Redacted**] 
 3.3.9.7 [**Redacted**] 

[**Redacted**] 
 3.3.9.8 [**Redacted**]

 [**Redacted**] 

[**Redacted**] 
 3.3.9.9 [**Redacted**]

 [**Redacted**] 

3.3.9.10 [**Redacted**] 

[**Redacted**] 
 3.3.10 [**Redacted**]

 3.3.10.1 [**Redacted**] 

[**Redacted**] 
 Table
3.3.10-1 [**Redacted**] 
 3.3.10.2 [**Redacted**] 
 [**Redacted**] 
  
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 3.3.10.3 [**Redacted**] 
 [**Redacted**] 
 3.3.10.4 [**Redacted**] 

[**Redacted**] 
 3.3.10.5
[**Redacted**] 
 [**Redacted**] 
 Table 3.3.10-2 [**Redacted**] 
 [**Redacted**]

 3.3.10.6 [**Redacted**] 

[**Redacted**] 
 3.3.10.7
[**Redacted**] 
 [**Redacted**] 
 3.3.11 Image Properties 
 3.3.11.1 [**Redacted**] 

[**Redacted**] 
 Table
3.3.11-1 [**Redacted**] 
 3.3.11.2 [**Redacted**] 
 [**Redacted**] 
 3.3.11.3 [**Redacted**] 

[**Redacted**] 
 3.3.11.4
[**Redacted**] 
 The Instrument shall allow for the following imaging [**Redacted**] 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

 [**Redacted**]

  

	 	a)	[**Redacted**] Table 3.3.11-2 [**Redacted**] 

  
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	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

 3.3.11.5 Image
Collection Modes 
 The Instrument shall provide the Image Collection Modes shown in Table 3.3.11-2 [**Redacted**] 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

 Table
3.3.11-2 [**Redacted**] 
 [**Redacted**] 
 3.3.11.6 Knowledge of Capture Time 
 [**Redacted**] 

3.3.11.7 Scan Order 
 [**Redacted**]

 3.3.11.8 Time Delay Integration (TDI) 
 Time Delay Integration (TDI) [**Redacted**] 
 3.3.12 Radiometry 

3.3.12.1 [**Redacted**] 

[**Redacted**] 
 Table
3.3.12-1 [**Redacted**] 
 3.3.12.2 [**Redacted**] 
 [**Redacted**] Table 3.3.11-2 [**Redacted**] 

Table 3.3.12-2a [**Redacted**] 

 
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 For consistency with the SSS testing, we have added Table 3.3.12-2b [**Redacted**]. This second
table represents the required NESR values from Table 3.3.12-2a at the compression rates listed in Table 3.3.12-2b. 
 Table
3.3.12-2b [**Redacted**] 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

 3.3.12.3
[**Redacted**] 
 The Instrument shall have mean Quantization Step Equivalent Spectral Radiance values less than or equal to the values
listed in Table 3.3.12-3for [**Redacted**]. For other line rates and TDI selections, QSESR will scale [**Redacted**]. 
 Table 3.3.12-3 [**Redacted**] 
 3.3.12.4 [**Redacted**] 

[**Redacted**] 
 Table
3.3.12-4 [**Redacted**] 
 [**Redacted**] 
 Figure 3.3.12-1 [**Redacted**] 
 [**Redacted**] 

[**Redacted**] 

3.3.12.5 [**Redacted**] 

[**Redacted**] 
 3.3.12.6
[**Redacted**] 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

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 3.3.12.7 Radiometric Stability 
 Calibrated response stability of the [**Redacted**] 
 3.3.12.8 Pixel-to-Pixel
Crosstalk 
 The image data shall be such that the electrical crosstalk-induced [**Redacted**] 

3.3.12.9 Bright Target Recovery 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

 3.3.12.10
Polarization 
 [**Redacted**] 
 3.4 Electrical 
 3.4.1 Input Power 

3.4.1.1 Voltage at Instrument Interface 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

 3.4.1.2 Power
Consumption 
 The SSS shall not exceed the power consumption values listed in [**Redacted**] 

Table 3.4.1-1 [**Redacted**] 
 The power used to maintain the temperature of the EOA shall not exceed the values in Table 3.4.1-2, exclusive of thermal control unique to the AUX capability. 

Table 3.4.1-2 [**Redacted**] 
 [**Redacted**] 
 Table 3.4.1-3 [**Redacted**]

 [**Redacted**] 
  

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 Table 3.4.1-4 [**Redacted**] 

3.4.1.3 Operational Voltages for Thermal Design 
 For sizing thermal control heaters and calculating time-averaged heater power and duty cycles, the following operational voltage ranges shall be used: 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

 [**Redacted**]

 3.4.2 Main Data Compression 
 The following data compression requirements apply only to Main data. 
 3.4.2.1 Data Compression

 The Instrument shall support lossy and lossless compression for the image data as follows and as further specified in the subparagraphs
below: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**]Table 3.3.11-2 [**Redacted**] 

 3.4.2.2 Lossless Compression 
 [**Redacted**] 

3.4.2.3 Lossy Compression 

[**Redacted**] 
 Table
3.4.2-1 [**Redacted**] 
 [**Redacted**] 
 3.4.3 Interface to Mission Data Recorder 
 Image data shall be output to the Mission Data
Recorder (MDR) on [**Redacted**]. All interfaces shall be as further specified in the WV-3 Instrument to Spacecraft ICD. 
 3.4.3.1
Interface Bit Rate 
 The Main average [**Redacted**] 

 
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 3.4.3.2 Transmit Clock 
 The Instrument shall generate a transmit clock [**Redacted**] 
 3.4.4 Telemetry

 The Instrument shall provide telemetry for the purposes of operational verification, test, troubleshooting and failure analysis.
[**Redacted**] 
 3.4.4.1 Command Verification 
 The SSS and [**Redacted**], as further specified in the WV-3 Instrument to Spacecraft ICD. 

3.4.4.2 Configuration 
 The Instrument
shall provide a response to commands sufficient to: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

 3.4.4.3 Electrical
Power 
 The Instrument shall provide telemetry on voltages and currents used by the Instrument as defined below. Voltage telemetry
shall be [**Redacted**] and current shall be [**Redacted**] 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

 3.5 Operations

 3.5.1 Image Collection Angles 
 The Instrument shall image over a range of viewing angles, [**Redacted**] 
 Table 3.5.1-1 [**Redacted**] 
 3.5.2 States and State Transitions

 The Instrument Main capability shall have the states and functions identified [**Redacted**]. When transitioning from standby to
disabled state, the system shall be considered disabled when the system is ready to be re-enabled to standby state. 
  

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 Table 3.5.2-1 [**Redacted**] 

Table 3.5.2-2 [**Redacted**] 
 [**Redacted**] 
 Table 3.5.2-3 [**Redacted**]

 Table 3.5.2-4 [**Redacted**] 
 3.5.3 Simultaneous Operations 
 The Instrument shall be capable of simultaneously performing
any or all of the functions as shown in Table 3.5.2-1 [**Redacted**] and Table 3.5.2-3 [**Redacted**] “Imaging” columns. Main and AUX states shall be independent, such that imagery can be collected, aggregated and compressed
(Main only), and transferred in any combination: 
  

	 	•	 	 Main only 

  

	 	•	 	 AUX only 

  

	 	•	 	 Simultaneous Main + AUX (within tolerances of independent / asynchronous clocks) 

3.5.4 Overlapping Main + AUX (different start and stop times).Operational Duty Cycle 
 3.5.4.1 Design Imaging Sequence (DIS) 
 The Instrument shall be capable of performing the
Design Imaging Sequence (DIS) specified in Table 3.5.5-1 under the following conditions: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

  

	 	e)	[**Redacted**] 

Table 3.5.4-1 [**Redacted**] 

[**Redacted**] 
 3.5.4.2 Special
Imaging 
 The Instrument shall be capable of performing a continuous [**Redacted**] image under the following conditions: 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

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	 	c)	[**Redacted**] 

 [**Redacted**]

 3.5.4.3 Day in the Life (DITL) Scenario for Thermal Analysis 
 The Instrument shall meet all requirements when operated in the Day In The Life (DITL) Scenario [**Redacted**] 
 Margins against the DITL shall be reported the following ways, at both BOL and EOL: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

 [**Redacted**]

 3.5.4.4 Minimum Image Duration 
 The Instrument shall be capable of imaging [**Redacted**] 
 3.5.5 Operating Cycles

 The Instrument shall be designed meet the requirements of this specification [**Redacted**] 

Table 3.5.5-1 [**Redacted**] 
 Figure 3.5.5-1 [**Redacted**] 
 3.6
Command and Telemetry 
 3.6.1 Command and Telemetry Interface 
 The Instrument shall interface with the Spacecraft Bus as below. All interfaces between the Instrument and Spacecraft Bus shall be redundant except for [**Redacted**] 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

 [**Redacted**]

 3.6.2 Reserved. 

3.6.3 Command Latency 
 Command latency on
the [**Redacted**] defined in the WV-3 SSS 1553 Command List. 
  
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 3.7 Protection 
 3.7.1 Power Fault Protection 
 3.7.1.1 Fault Detection 

Fault detection mechanisms shall include sufficient data provided to the Spacecraft Bus processor to permit identification of the fault trigger and fault
response after the fact. 
 3.7.1.2 Sudden Power Removal 
 In support of the Satellite Safe mode, the Instrument shall not be damaged if the input power in any state is removed at any time without warning. In support of ground integration and test, sudden power
loss shall include power loss on either the Payload Bus power input, or the Essential Bus power input, or both Payload Bus and Essential bus power input at the same time. The Instrument shall be designed to gracefully recover from sudden power
removal on re-start. 
 3.7.1.3 Voltage Excursion 
 The Instrument shall include provisions to protect [**Redacted**], as further specified in the WV-3 Instrument to Spacecraft ICD. Reverse voltage protection is not required during flight.

 3.7.1.4 Over-current Protection 
 The Instrument shall include provisions to limit the input power, if the Sensor Subsystem [**Redacted**]. Current may be limited at the box or power module level as available in the existing
design. 
 3.8 Test and Integration 
 3.8.1 Orbit Compatibility 
 The Instrument shall be capable of operating at any
equatorial altitude between [**Redacted**] 
 3.8.2 Stand-Alone Testing 
 The Instrument design shall permit stand-alone testing at the contractor’s facility using the appropriate GSE as well as Spacecraft Bus level testing once integrated with the Spacecraft Bus. Required
test conditions, [**Redacted**] 
 3.8.2.1 Stand-Alone Test Stimulation Lamp 

The Instrument design shall accommodate an internal stimulation lamp with [**Redacted**], with interfaces as defined in the WV-3 Instrument to
Spacecraft ICD. 
  
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 3.8.3 Instrument Integration and Checkout 

The Instrument shall incorporate provisions, including Main and [**Redacted**] and the Satellite has been integrated with the launch vehicle. These
provisions shall include, as required, the interfaces necessary to maintain connectivity with the on-site GSE as well as any launch base external interfaces necessary to maintain pre-launch connectivity with the Mission Control Segment. Detailed
integration and test interface requirements are further specified in the WV-3 Instrument Integration & Test ICD, with which the Instrument shall comply. 
 3.8.4 Satellite/Instrument Initialization and Checkout Capabilities 
 The Instrument shall
pose no constraints on operation that prevent its being placed in its normal operational attitude immediately following launch vehicle separation. 
 The Instrument initialization will include command and telemetry checkout and basic functionality of all subsystems. The Instrument shall pose no constraints on operation that prevent it being possible to
[**Redacted**] following launch vehicle separation. 
 The Instrument shall pose no constraints on operation such that it shall be
possible to perform [**Redacted**] following separation from the launch vehicle. 
 The Instrument shall pose no constraints on operation
[**Redacted**] immediately following launch vehicle separation. 
 3.8.5 Checkout Operations 

There shall be no operating characteristics of the Instrument that would prevent its being capable of having its [**Redacted**] 

The Instrument shall be capable of supporting an [**Redacted**] of launch. During this period, the Instrument design shall allow correlation of
critical Instrument performance with the Satellite and ground segments such that end-to-end Spacecraft Bus performance can be verified. All necessary satellite on-orbit calibrations and/or adjustments shall be capable of being completed during this
period. 
 3.9 Design and Construction 
 3.9.1 Quality Factors 
 The following subsections establish the Satellite high-level quality
requirements. 
 3.9.1.1 Reliability at End of Life 
 The Instrument Main capability shall have [**Redacted**] reported to DigitalGlobe. 

3.9.1.2 Single Point Failures 
 There
shall be no credible single point failures that would prevent the Instrument from meeting its Main requirements as defined in this specification, [**Redacted**] Functions unique to the [**Redacted**] other Instrument or Spacecraft Bus
components or otherwise reduce the reliability of the primary mission. 
  
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 Non-credible single points of failure shall be identified in the design and shall have compensating
provisions, [**Redacted**] 
 Cable harness and pin/socket connections shall be considered [**Redacted**] 

3.9.1.3 Commands that Induce Failure 

There shall be no single command that could cause loss of the Instrument, assuming no Instrument components have previously failed. 

3.9.1.4 Operable Main Pixel 
 A Main
pixel shall be considered operable, even if out of specification, it meets the following requirements: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

 3.9.1.5 Reserved

 3.9.1.6 Inoperable or Out of Specification Main Pixels 
 Inoperable Main Pixels may be removed from any performance averages and standard deviations for determining compliance to performance specifications. The following requirements shall apply at Instrument
delivery (Beginning of Life). 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

 3.9.1.7 Commands that
Use Relays 
 Frequently used commands, such as image [**Redacted**] commands shall use electronic switching. 

3.9.1.8 Power Converter Inhibit 
 The
power converters in each subsystem or component as appropriate shall have [**Redacted**]. This requirement is waived for power converters that [**Redacted**] 

 
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 3.9.2 Availability 
 The reliability requirement supports the system-level availability allocated to the Instrument. Additional operation-related requirements pertaining to availability include: 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

 3.9.3 Optical
Construction 
 The Instrument shall have an [**Redacted**] 
 3.9.4 Useful Life 
 3.9.4.1 Storage Life 

The Instrument design shall accommodate a program delay [**Redacted**] without the need for refurbishment when stored in a controlled environment.
The Instrument may be recalibrated if needed. 
 3.9.4.2 Mission Life 
 The Instrument shall meet all on-orbit performance requirements for [**Redacted**] 

3.9.5 Reserved. 
 3.9.6 Reserved.

 3.9.7 Cleanliness and Contamination Control 
 [**Redacted**] 
 3.9.7.1 Contamination Protection 

The Instrument shall include protective equipment designed to minimize contamination to sensitive components from the post-delivery environment and
equipment within that environment, described below, such that aforementioned cleanliness levels can be maintained. 
 [**Redacted**]

 For reference, the spacecraft and other equipment present in the post-delivery integration and test environment are characterized by
material and contamination levels as follows: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

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 3.9.8 Safety 
 The Instrument shall be designed to allow for safe handling, operation, and transportation through all mission phases. It shall comply with the specific requirements of [**Redacted**] with respect
to: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

 3.9.9 Design of
Mechanisms 
 All mechanisms shall be designed to operate [**Redacted**] 

[**Redacted**] 
 3.9.10 Computer
Resources 
  

	 	a)	Hardware – [**Redacted**] 

  

	 	b)	Software – [**Redacted**] 

3.9.11 Environmental Design 
 3.9.11.1
Structural Design Requirements 
 3.9.11.1.1 Angular Acceleration 
 The Instrument shall be designed to survive an acceleration of [**Redacted**] 

[**Redacted**] 
 3.9.11.1.2 Factors
of Safety 
 For purposes of preliminary design and analysis, the factors of safety defined [**Redacted**] 

Table 3.9.11-1 [**Redacted**] 
 [**Redacted**] 
 Table 3.9.11-2
[**Redacted**] 
 [**Redacted**] 

Calculation methodology: Ultimate and Limit Factors of Safety [**Redacted**] 
 [**Redacted**] 
  
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 3.9.11.1.2.1 Buckling Factors of Safety 
 Where buckling of a single element or unreinforced shell would be catastrophic or result in unacceptable deformation, buckling Factors of Safety (BFS) shall be [**Redacted**], with the knowledge of
predicted dynamic or acoustic loads. 
 Panel buckling shall be allowed. The post-buckling load distribution for reinforced shell
structures shall [**Redacted**] 
 For composite shell panels, the BFS shall [**Redacted**] 

3.9.11.1.3 Vibration 
 The PSU and
DPU shall be designed to survive the protoflight level random vibration test environment as specified [**Redacted**] 
 3.9.11.1.3.1
Random vibration—Acceptance & Protoflight—PSU 
 The PSU shall be designed to operate and meet performance requirements
after exposure to random vibration. [**Redacted**] 
 Figure 3.9.11-1
[**Redacted**] 
 Table 3.9.11-3 [**Redacted**] 

3.9.11.1.3.2 Random Vibration – Acceptance & Protoflight –DPU 
 The DPU shall be designed to operate and meet performance requirements after exposure to random vibration. [**Redacted**] 

Figure 3.9.11-2 [**Redacted**] 

Table 3.9.11-4 [**Redacted**] 

3.9.11.1.4 Reserved 
 3.9.11.1.5
Acoustic 
 The Instrument shall be designed to survive the protoflight acoustic test environment shown [**Redacted**]

 Table 3.9.11-5 [**Redacted**] 
 [**Redacted**] 
  
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 3.9.11.1.6 [**Redacted**] 
 Components shall be designed to survive the protoflight shock test levels specified in [**Redacted**] 
 Table 3.9.11-6 [**Redacted**] 

[**Redacted**]                    
     
 3.9.11.1.7 Pressure Profile 
 Component enclosures shall be designed to survive, without undergoing [**Redacted**] 

3.9.11.1.8 Minimum Frequency 
 All
bus-mounted SSS components shall be designed to have no [**Redacted**]. The EOA shall be designed to have no [**Redacted**]. If not practical, exceptions may be made on a case-by-case basis with the concurrence of DigitalGlobe. Waivers
granted for the star tracker mounts and PSU cover on WV-2 shall apply to WV-3, provided there are no structural design changes that will impact change coupled bus-instrument resonance behavior. 

3.9.11.1.9 Circuit Boards 
 All
circuit boards shall be [**Redacted**] 
 3.9.11.1.10 Pressure Vessels and Pressurized Components 

Pressure vessels and pressurized components shall be designed and tested to be compatible with the requirements listed [**Redacted**]

 Heat Pipes shall be designed [**Redacted**] 
 3.9.11.1.11 Steady State Acceleration 
 3.9.11.1.11.1 Steady State Acceleration –
PSU, DPU 
 The DPU and PSU shall be designed to operate and meet performance requirements after [**Redacted**] 

Figure 3.9.11-3 [**Redacted**] 

3.9.11.1.11.2 Steady State Acceleration – EOA 
 The EOA shall be designed to operate as specified in its individual component specification after exposure [**Redacted**] 

Table 3.9.11-7 [**Redacted**] 
 3.9.11.2 Thermal Vacuum Design Requirements 
 The Instrument
shall meet the following functional and performance requirements when exposed to a vacuum environment (pressures between 0 and 10-5 Torr) between the temperature limits specified in [**Redacted**] 

 
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	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

 The EOA thermal control
system design shall accommodate analytical uncertainty as follows: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

 For bus-mounted
Instrument components, the interface temperatures specified in the WV-3 Instrument to Spacecraft ICD shall be used with no additional temperature margins for analytical uncertainty [**Redacted**] 

Table 3.9.11-8 [**Redacted**] 
 [* Functions here is defined as outputting data to the AUX Electronics such that the AUX Electronics will output valid data packets to the spacecraft bus. It is understood that the FPU data may be
noise or saturated values at temperatures above the performance range.] 
 [**Redacted**] 

3.9.11.3 EMI/EMC Design Requirements 

3.9.11.3.1 [**Redacted**] 

[**Redacted**] 

Table 3.9.11-9 [**Redacted**] 
 Table 3.9.11-10 [**Redacted**] 

Figure 3.9.11-4 [**Redacted**] 
 Figure 3.9.11-4a [**Redacted**] 
 Figure
3.9.11-5 [**Redacted**] 
 Figure 3.9.11-6 [**Redacted**] 

 
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 3.9.11.3.2 Magnetic Field Susceptibility 
 The Instrument shall meet all performance requirements [**Redacted**] 
 [**Redacted**]

 3.9.11.3.3 Magnetic Field Generation 
 Instrument components shall [**Redacted**] 
 3.9.11.4 Grounding and Inrush

 3.9.11.4.1 Signal Interface Grounding 
 Single ended signal interfaces should be avoided. 
 Differential interface signals shall
[**Redacted**] 
 3.9.11.4.2 Primary Power Grounding 
 For components with either new designs or existing designs that have modified primary power circuitry, primary power circuits shall be isolated [**Redacted**] 

3.9.11.4.3 Secondary Power Grounding 

Secondary power, inherently isolated from primary power by dc-dc converters or isolation transformers, and routed external to the equipment, shall be
grounded to the structure as specified in the WV-3 Instrument to Spacecraft ICD. Care should be taken to isolate signal, command, and control lines such that separate, independently grounded power supply returns will not be inadvertently
interconnected. 
 Components with single ended interfaces should not have secondary returns tied to chassis, in order to avoid ground offsets.
In such cases, secondary returns shall be referenced to spacecraft chassis at a designated spacecraft signal single point ground. [**Redacted**] 
 3.9.11.4.4 PSU In-Rush Current 
 The PSU shall meet the PSU in-rush current interface
requirements defined in the WV-3 Spacecraft to Instrument ICD. 
 3.9.11.4.5 Other EOA Electronics In-Rush Current 

Other EOA electronics and the AUX electronics shall meet the in-rush current interface requirements for other EOA electronics defined in the WV-3
Spacecraft to Instrument ICD. 
 3.9.11.5 Radiation Exposure Design Requirements 
 The Instrument shall be designed to meet operational requirements during and after exposure to the space radiation environment defined herein. [**Redacted**] 

3.9.11.5.1 Total Ionizing Dose 
 The
Total Ionizing Dose (TID)[**Redacted**] 
  

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 Table 3.9.11-11 [**Redacted**]

 Figure 3.9.11-7 [**Redacted**] 
 3.9.11.5.2 Displacement Damage Dose 
 Displacement Damage Dose (DDD) is the energy
imparted to a unit mass that results in displacement damage, as opposed to ionization. [**Redacted**] 
 Table
3.9.11-12 [**Redacted**] 
 Figure 3.9.11-8 [**Redacted**] 

3.9.11.5.3 Radiation Energy Spectra 

Detailed shielding analyses may be used in lieu of the dose depth curves [**Redacted**] 

3.9.11.5.4 Enhanced Low Dose Rate Susceptibility (ELDRS) 
 Semiconductor components with a linear or mixed signal application using [**Redacted**]. Components shall be binned into three categories: [**Redacted**] 

The Instrument Contractor shall document the ELDRS evaluation, including a justification for each part’s categorization, and submit this to
DigitalGlobe for independent review. DigitalGlobe will then determine which parts (if any) require additional ELDRS testing. [**Redacted**]. 
 3.9.11.6 Single Event Effects 
 Single Event Effects include [**Redacted**] are as
follows: 
 The Instrument shall be designed such that no single event effect can cause permanent damage (including loss of redundancy) to a
system, subsystem, or component. 
 SEU effects on component operations shall be temporary and correctable by automatic reset or ground command.

 The Instrument shall meet performance requirements during exposure [**Redacted**] 

As specified in the component Statement of Work (SOW) or Product Functional Specification, certain critical spacecraft electronics components which are
required to perform during [**Redacted**] 
 All MOS devices shall have SEL data showing that the device is immune to SEL up to
[**Redacted**] 
 The incorporation of latchup mitigation circuitry does not automatically obviate this requirement; DigitalGlobe
approval of the latchup mitigation strategy and its test requirements is required to preclude the necessity of a waiver in this instance. (WorldView specific requirement) 

 
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 [**Redacted**] 
 3.9.11.7 Reserved 
 3.9.11.8 Electrostatic Discharge 

[**Redacted**] or an approved substitute shall be used as a guideline for handling of ESD-sensitive components. 

3.9.11.9 Atomic Oxygen 
 The Instrument
shall be designed to withstand exposure to atomic oxygen environment for [**Redacted**] shall be reported to DigitalGlobe. 

3.9.11.10 Mechanism Torque/Force 

The minimum available driving torque or force for mechanisms shall be determined based on the Factor of Safety (FS) table below. [**Redacted**]

 Driving Torques: 
  

	 	•	[**Redacted**] 

 Resistive Torques:

  

	 	•	[**Redacted**] 

  

	 	•	[**Redacted**] 

 [**Redacted**]

 Table 3.9.11-13 [**Redacted**] 
 3.9.11.11 Reserved 
 3.9.11.12 Metal Enclosure and Mechanical Component Bonding

 The Instrument shall be designed to be compliant with [**Redacted**] 
 3.9.11.13 Composites Bonding and Grounding 
 Composite structures shall be designed to have
bond impedances [**Redacted**] 
 3.9.11.14 Primary Power Subsystem Characteristics 

The instrument shall be designed to comply with the following requirements. 

 
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 3.9.11.14.1 [**Redacted**] 
 [**Redacted**] 
 3.9.11.14.2 [**Redacted**] 

[**Redacted**] 
 3.9.11.14.3
[**Redacted**] 
 [**Redacted**] 
 3.9.11.14.4 [**Redacted**] 
 [**Redacted**] 

3.9.11.15 Parts 
 3.9.11.15.1 EEE Part
Reliability 
 Standard parts shall meet the following requirements: 

 

			
	    Microcircuits and hybrids:	  	[**Redacted**]
	    Semiconductors:	  	[**Redacted**]
	    Passive components:	  	[**Redacted**]

 Non-standard parts shall have reliabilities consistent with the nearest standard parts. This confidence may be obtained
by screening the non standard parts consistent with the screening requirements of the nearest standard part. Any part that cannot be screened to bring it up to the [**Redacted**] shall have DigitalGlobe signature approval prior to
requisition. 
 Non-standard active parts shall be subject to destructive physical analysis of parts with the same lot date code per
[**Redacted**] or equivalent. 
 All EEE parts shall be subject to a part history evaluation. 

3.9.11.15.2 Plastic Parts 
 DigitalGlobe
shall be notified before flight assembly when plastic encapsulated electronic parts (hereinafter referred to simply as plastic parts) are selected for incorporation in a design. The contractor shall provide lot qualification data for any plastic
parts used. The use of plastic parts is strongly discouraged. Unfortunately there are situations where they cannot be avoided. A software tool such as [**Redacted**] in this case for computing the reliability impact felt due to plastic parts.

 3.9.11.15.3 Lot Date Codes 

Parts selection shall comply with the following Lot Date Code requirements, where part age is defined as the difference between the part Lot Date Code and
the start of the WorldView-3 Instrument contract: 
  

	 	a)	[**Redacted**] 

  

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	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

 3.9.11.15.4 Part
Derating 
 The preferred derating of components shall be in accordance with [**Redacted**]. An allowable exception is the operation
of microcircuits at manufacturer’s published recommended or characterized supply voltages in lieu of derating. 
 3.9.11.16 Materials

 3.9.11.16.1 Material Selection Criteria 
 The selection of materials shall consider the application, requirements, environmental requirements, usage restrictions and the items in the following paragraphs, as applicable. 

 

	 	a)	Previous successful usage on long life space programs shall be applicable. 

 

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

  

	 	e)	[**Redacted**] 

  

	 	f)	[**Redacted**] 

  

	 	g)	[**Redacted**] 

  

	 	h)	[**Redacted**] 

  

	 	i)	[**Redacted**] 

  

	 	j)	[**Redacted**] 

  

	 	k)	[**Redacted**] 

 3.9.11.16.2 Material
Specifications 
 Materials shall be controlled by a detailed specification that will include, as applicable, material configuration and
performance requirements, lot identification, lot acceptance/qualification tests, and protective packaging and handling requirements. If official specification, [**Redacted**] for the procurement of materials. All material shall be traceable
to the manufacturer. Age sensitive materials shall have shelf-life control. The materials that exceed the expiration date shall not be used without appropriate recertification by MRB. 
 3.9.11.16.3 Magnetic Design Requirements 
 Non-magnetic material should be used whenever
possible [**Redacted**] except as required in inductive components and cores. DigitalGlobe shall be notified before flight assembly when magnetically soft materials are selected for incorporation in a design. 

 
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 3.9.11.17 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 two times the predicted number of cycles, including all cycles
incurred during both the Mission Life and during ground testing. The Instrument Contractor shall identify all life-limited Cycle-limited items, which shall at a minimum include: 

 

	 	•	[**Redacted**] 

  

	 	•	[**Redacted**] 

  

	 	•	[**Redacted**] 

  

	 	•	[**Redacted**] 

 For all cycle-limited
items, the known cycle-limit (cycles to failure or loss of performance) shall be reported to facilitate evaluation of margin. If the cycle-limit is not known, e.g. the component was not tested to failure, then a best estimate shall be provided.

 3.9.11.17.1 EEPROMs 
 The
more conservative [**Redacted**] 
 3.9.11.17.2 Interface Connectors 
 The use of connector savers is required for flight hardware external interfaces. 

[**Redacted**] 
 3.9.11.17.3
Electromechanical Relays 
 Electromechanical relays shall not be used for routine operational functions. 

3.9.11.18 Metal Finishes 
 The Instrument
shall be designed to be compliant with the following requirements 
 3.9.11.18.1 [**Redacted**] 

[**Redacted**] 
 3.9.11.18.2 Finish
Adhesion Testing 
 Vendors of painted and plated surfaces shall have processes and procedures in place to ensure adequate finish adhesion of
anodized, plated, and painted surfaces. 
 One way to ensure adequate finish adhesion is specified in [**Redacted**]. This test shall be
considered to pass if the finish adhesion is not compromised on the article under test apart from that due to the scribing operation itself given in paragraph 4.1 of the test method. The 24 hour immersion in distilled water requirement is not
applicable when testing anodized surfaces; [**Redacted**] 
 [**Redacted**] 

 
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 3.10 [**Redacted**] Performance Requirements 

3.10.1 [**Redacted**] 
 [**Redacted**]

 3.10.2 [**Redacted**] 

[**Redacted**] 
 3.10.3 [**Redacted**]

 [**Redacted**] 

[**Redacted**] 
 3.10.4 Total Field
of View 
 The total field of view shall correspond to at [**Redacted**] 
 3.10.5 Distortion Stability 
 The operational distortion stability of the Instrument
distortion shall [**Redacted**] 
 3.10.6 Geometric Precision – Line of Sight Stability 

The following requirements are for the stability of the Line-Of-Sight (LOS) for each pixel of the [**Redacted**] 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

  

	 	e)	[**Redacted**] 

 3.10.7 On-Orbit Focus
Adjustment 
 [**Redacted**] 

3.10.8 Stray Light Rejection and Internal Light Scattering 
 The Instrument shall limit stray light [**Redacted**] 
 [**Redacted**]

 3.10.9 Sensor Spectral Properties 
 The following paragraphs define the basic requirements relative to the [**Redacted**] 
  

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 3.10.9.1 Sensor Spectral Bands Definitions 

[**Redacted**] 

Table 3.10.9-1 [**Redacted**] 
 3.10.9.2 Filter Spectral Flatness Between Band Edges 
 Flatness Between Band Edges:
[**Redacted**] shall have the following properties: 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

 3.10.9.3 Filter
Spectral Flatness Between [**Redacted**] Relative Response Points 
 The peak normalized filter transmission between the minimum wavelength
with a [**Redacted**] relative response point and the maximum wavelength with a [**Redacted**] relative response point shall always exceed [**Redacted**]. 
 3.10.9.4 Integrated Out of Band Response 
 The ratio of the integrated response of
the instrument beyond [**Redacted**] 
 3.10.9.5 Band Edge Slope 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

 3.10.9.6 Spectral
Bandwidth Uniformity 
 Within a band, all pixels bandwidths shall be uniform [**Redacted**] 

3.10.9.7 Center Wavelength Uniformity 

Within a band, all pixels shall have a center wavelength within [**Redacted**] 

Table 3.10.9-2 [**Redacted**] 
 3.10.9.8 Filter Spectral Stability 
 Band center wavelengths and band edges shall not change
[**Redacted**] 
 3.10.10 Line Rates 
 The [**Redacted**] shall provide as a minimum [**Redacted**] commandable line rates, selectable on an image by image basis as defined in [**Redacted**] 

 
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 Table 3.10.10-1 [**Redacted**] 

The [**Redacted**] shall have the on-orbit capability to implement additional line rates to allow simultaneous operation with all Main sensor
Modes shown in [**Redacted**]. 
 3.10.11 Band Selections 
 The [**Redacted**] shall be able to be commanded to collect data [**Redacted**].  

3.10.12 Knowledge of Capture Time 
 The
[**Redacted**] shall utilize a time and tone line method, as described below and further in the WV-3 Instrument to Spacecraft ICD, [**Redacted**]. The time tag shall be included in the image data, continuing until the AUX sensor is
commanded to complete an image capture. In general, the time and tone method is as follows: 
  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 [**Redacted**] 

 3.10.13 AUX Modulation Transfer Function 
 The instrument end to end geometric mean
of the along scan and cross scan [**Redacted**] 
 [**Redacted**] 
 3.10.14 Signal to Noise Ratio 
 The zero spatial frequency Signal to Noise Ratio
(SNR) in imaging mode [**Redacted**] 
 Table 3.10.14-1 [**Redacted**]

 [**Redacted**] 

3.10.15 Detector Full Well Capacity 
 The
full well capacity for each band shall be established to preclude saturation for the at-aperture radiances, [**Redacted**] 
 3.10.16
Exposure Optimization 
 The [**Redacted**] shall provide on an image by image basis, the capability to control exposure over the
range of imaging modes [**Redacted**] 
  

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 Table 3.10.16-1 [**Redacted**] 

[**Redacted**] 
 3.10.17 Bit Depth

 [**Redacted**] 

3.10.18 No AUX Image Data Compression 

[**Redacted**] 
 3.10.19 Absolute
Radiometric Accuracy 
 For this and subsequent paragraphs, [**Redacted**] standards. This requirement applies to extended, spatially
uniform, unpolarized targets with a known spectral shape. 
 The at-aperture spectral radiance shall be determined analytically from the EOA
system [**Redacted**] 
 3.10.20 Noise Equivalent Spectral Radiance 
 [**Redacted**] 
  

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

 Table
3.10.20-1 [**Redacted**] 
 [**Redacted**] 
 3.10.21 Quantum Step Equivalent Spectral Radiance 
 The quantum step equivalent spectral
radiance [**Redacted**] specified in paragraph 3.10.20. 
 3.10.22 Operable Pixel 

A pixel shall be considered operable, even if out of specification, it meets the following requirements: 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

  

	 	d)	[**Redacted**] 

  

	 	e)	[**Redacted**] 

  

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 3.10.23 Inoperable and Out of Specification Pixels 

Inoperable [**Redacted**]. The following requirements shall apply at Instrument delivery (Beginning of Life). 

 

	 	a)	[**Redacted**] 

  

	 	b)	[**Redacted**] 

  

	 	c)	[**Redacted**] 

 3.10.24 Banding and
Streaking 
 For each operating mode for which a Noise Equivalent Irradiance (NEI) requirement exists, [**Redacted**]. The banding
metric is: 
 [**Redacted**] 

For each operating mode, each banding metric [**Redacted**] of required dynamic range. 
 3.10.25 Coherent Noise 
 Coherent noise is defined as the magnitude of the
autocorrelation of a dark [**Redacted**] scene, computed after subtraction of [**Redacted**] 
 [**Redacted**] 

3.10.26 Reserved 
 3.10.27
Pixel-to-Pixel Crosstalk 
 The image data shall be such that the electrical crosstalk-induced artifacts in receiver pixels caused by
regions of sender [**Redacted**] 
 3.10.28 Bright Target Recovery 
 Bright target recovery from a [**Redacted**] 
 3.10.29 Polarization 

[**Redacted**] 
 3.10.30 Pixel to
Pixel Calibration and Stability 
 All detectors in a given band shall be calibrated and stable to [**Redacted**] of the required
dynamic range. 
 3.10.31 Radiometric Stability 
 For signals between [**Redacted**], the response of each channel shall be stable to the values listed for the following timescales: 

 

	 	•	 	 [**Redacted**] 

This requirement includes radiometric stability under the operational FPA thermal stability over the timescales addressed. If it is part of the CONOPS
for this sensor, [**Redacted**] 
  

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 3.10.32 Image Data Content 
 Image data shall be packetized separately for each [**Redacted**]. All of the information needed to accurately reconstruct the image data and verify data integrity shall be contained in
[**Redacted**], including at least the following:
  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 Line rate 

  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 Identification of specific [**Redacted**] 

  

	 	•	 	 [**Redacted**] 

  

	 	•	 	 A sequentially [**Redacted**] 

  

	 	•	 	 Time tag 

  

	 	•	 	 [**Redacted**] 

Precise definition of [**Redacted**] to ensure compatibility with spacecraft bus and ground processing interfaces and are expected to be very
similar to those of the main sensor. 
 4. Verification 
 4.1 Verification Methods 
 4.1.1 Test (T) 

Test is an action by which the operability, supportability, performance capability or other specified qualities of an item are verified when subjected to
controlled conditions that are real or simulated. These verifications may require the use of special test equipment and instrumentation to obtain quantitative data for analysis as well as qualitative data derived from displays and indicators
inherent in the item(s) for monitor and control. Requirements shall be verified by test to the maximum extent practical. Verification shall also be performed at the highest level of assembly practical. 

4.1.2 Inspection (I) 
 Inspection is the
qualitative demonstration of a functional requirement or an observation or examination of the item against the applicable documentation to confirm compliance with requirements. 
 4.1.3 Analysis (A) 
 Analysis is a process used in lieu of or in addition to testing to
verify compliance with specifications. The technique typically includes an interpretation, or interpolation and extrapolation, of analytical or empirical data under defined conditions or reasoning to show theoretical compliance with stated
requirements. 
  
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Confidential 
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 4.1.4 Similarity (S) 
 Similarity is an analysis process of comparing a current item with a previous item which takes into consideration configuration, test data, application and environment. The evaluation shall be documented
and shall include: the test procedures/reports of the item to which similarity is claimed, a description of the difference(s) between the items and the rationale for verification by similarity. All operational experience shall be documented and
available for review. 
 4.2 Instrument Level Verification 
 Form/fit/function testing shall be performed at the instrument level. 
 4.3 Satellite Level of
Verification 
 Instrument interface requirements, including those defined in the WV-3 Instrument to Spacecraft ICD and WV-3 Instrument
Integration & Test ICD shall be verified ahead of Instrument to Spacecraft Bus integration. 
 4.4 Unit Level of Verification

 Minimum unit-level environmental tests shall be performed as specified in Section 4.6.5. Additional unit-level testing shall be
performed as needed to verify unit functionality and performance needed to support higher-level requirements. 
 4.5 Reserved 

4.6 Test Program 
 4.6.1 Test
Connections 
 Unless otherwise specified herein, all power connections, measurements, and signal inputs shall be made through the external
connectors. [**Redacted**] 
 4.6.2 Baseline Performance Tests 
 Components shall be tested to demonstrate compliance with the performance requirements specified herein to establish the ambient baseline prior to initiation of environmental testing, and at the
conclusion of environmental testing prior to shipment. 
  
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 4.6.3 Abbreviated Functional Test 
 Abbreviated functional tests shall be performed at the contractor’s option, between environments. The tests reduce schedule risk by providing an early indication of anomalies or failures due to
environmental exposure. In general the abbreviated functional test is a subset of the baseline performance test and provides a reasonable level of certainty that the unit is still performing to specification requirements. In some cases the
abbreviated functional test may also specifically evaluate a given parameter to verify performance budget allocations. The contractor shall determine the limits for these tests. 
 4.6.4 Reserved 
 4.6.5 Environmental Test 

4.6.5.1 Mass Properties 
 Individual unit
weight and space envelope shall be measured. Center of gravity and moments of inertia shall be verified by analysis. 
 4.6.5.2
Contamination/Cleanliness 
 The Instrument components shall be delivered clean according to the contractor’s Contamination Control
Plan. 
 4.6.5.3 Metal Enclosure and Mechanical Component Bonding 
 The resistance between each discrete metal enclosure and the mounting plate of the component shall be measured. The resistance between the two surfaces shall be less than 1 ohm. If positive design
features, such as conducting mating surfaces fastened with multiple fasteners, are present then the measurement is not required. 
 4.6.5.4
Limited Performance Tests 
 Limited performance tests shall be conducted before, during, and after environmental tests, as appropriate, in
order to demonstrate that functional capability has not been degraded by the environmental tests. Limited performance tests shall demonstrate that the performance of selected functions is within acceptable limits. 

4.6.5.5 Leak Detection 
 All Instrument
components which contain a gas or liquid shall be subjected to leak checks. Additionally, subsystems/subassemblies that contain a gas or liquid shall be leak checked at the subsystem/subassembly level (external leak). Time of performance of the
post-environmental leak-check shall be determined by the contractor. Maximum allowable component leak rates are defined in the component product functional specifications. [**Redacted**] 

4.6.5.6 Proof Pressure 
 Heat pipes shall
be tested according to the requirements given in [**Redacted**] 
  
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 4.6.5.7 Vibration Testing 
 4.6.5.7.1 [**Redacted**] 
 [**Redacted**] 

If either the DPU or PSU remains fundamentally unchanged from previously qualified designs, testing to acceptance levels for the unit will be approved on
a case-by-case basis by DigitalGlobe. 
 Parameters of the [**Redacted**] such that the overall EOA requirement is satisfied, where the
acoustic information is based on the launch vehicle vendor data. Notching may be required at certain frequencies to ensure that structures are not exercised beyond their allowable loads, and will be approved on a case-by-case basis by DigitalGlobe.

 [**Redacted**] 
 4.6.5.7.2
[**Redacted**] 
 [**Redacted**] 
 Figure 4.6.5-1 [**Redacted**] 
 [**Redacted**]

 [**Redacted**] 

4.6.5.7.3 [**Redacted**] 

[**Redacted**] 
 4.6.5.8 Thermal
Testing 
 4.6.5.8.1 [**Redacted**] 
 [**Redacted**] 
 Table 4.6.5-1
[**Redacted**] 
 4.6.5.8.2 [Ambient Pressure Thermal Cycling] 

[**Redacted**] 
 4.6.5.8.3
[**Redacted**] 
 [**Redacted**] 
 4.6.5.8.4 [**Redacted**] 
 [**Redacted**] 

 
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 4.6.5.9 [**Redacted**] 
 [**Redacted**] 
 4.6.5.10 [**Redacted**] 

4.6.5.10.1 [**Redacted**] 

[**Redacted**] 

Table 4.6.5-2 [**Redacted**] 

4.6.5.10.2 [**Redacted**] 

[**Redacted**] 
 4.6.5.10.3
[**Redacted**] 
 [**Redacted**] 
 4.6.5.11 [**Redacted**] 
 [**Redacted**] 

4.6.5.11.1 Total Dose Testing 

Should total dose testing be required due to lack of data or inadequate design margins, [**Redacted**] 

4.6.5.11.2 Single Event Effects Testing 

Should Single Event Effects testing be required, it shall be performed using [**Redacted**] 

4.6.5.12 Mechanism Force/Torque Testing 

For design verification, the driving force/torque margin shall be verified by testing [**Redacted**] 

4.6.6 Main Charge Transfer Efficiency (CTE) Screening 
 Imagery artifacts such as local MTF degradation and banding can be [**Redacted**]; additional testing may also be performed at the Instrument Contractor’s discretion. 

To support these tests and to provide radiometric correction data on-orbit, [**Redacted**] 

4.6.6.1 SSS Level Screening 

[**Redacted**] 
 4.6.6.2 FPU Level
Screening 
 At minimum operating voltage, [**Redacted**], without necessarily including all combinations, or all intermediate TDI
settings. Combinations shall be selected, as far as possible, to capture any anticipated problem areas. 
  

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 4.6.6.3 Test Success Criteria 
 The difference between [**Redacted**] 
 Table
4.6.6-1 [**Redacted**] 
 [**Redacted**] 
  
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 4.7 Verification Matrix 
 [**Redacted**] 
 [**Redacted**] 

 
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EXCHANGE COMMISSION 
  

 Modification #17 
 (Proposal #12-382 – [**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 1601Dry 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:

 ITT to add [**Redacted**] to the WV3 Instrument to protect the [**Redacted**] during TVAC testing at Ball. 

 

							
	 Original Contract Value
	  	[**Redacted**]	  	$	167,726,933	  
	 This Modification (12-382)
	  	[**Redacted**]	  	$	63,000	  
	 Adjusted TOTAL Contract Value
	  		  	$	167,789,933	  

 The total contract price is herein changed from $167,726,933 to $167,789,933 

This modification will result in one (1) new milestone payment: 
  

	 	•	 	 Installation of the [**Redacted**] 

 Exelis is expecting completion of this activity in March of 2013. 
 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**]

[**Redacted**]
	  	 Name: Neal T. Anderson

Title: VP, Technology Development

		
	Date: 6 December 2012	  	Date: 5 December 2012

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