Section D NASA Launch Services II (NLS 11)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-12
QUICK LOOK FLIGHT REPORT
DESCRIPTION/PURPOSE:
After each launch, a quick look post-flight analysis shall be performed using preliminary
evaluations of all available vehicle telemetry and insertion performance. A briefing may satisfy
the intent of this report.
DATA REQUIREMENTS:
The data report shall include:

(A) Preliminary trajectory and performance data

(B) Orbital accuracy estimates

(C) Preliminary vehicle subsystem system performance

(D) Preliminary evaluations

D2-44


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

32.2

32.3

Definitions:

Covered Launch Activities: Any and all activities involved in the preparation of a launch
vehicle and payload for launch, and conduct of the launch, when those activities take
place at a launch site in the United States.

Launch: The intentional ignition of the first-stage motor(s) of the launch vehicle that has
been integrated with the payload.

Launch Vehicle: The baseline LVS consisting of a common core booster section and
any strap on motors attached, one (1) interstage, an orbital adjust module, the payload
fairing and the payload adapter.

Party or Parties: The Contractor or NASA, or both.

Payload: All NASA or NASA-sponsored equipment that has been or will be integrated
with the launch vehicle for transportation into earth orbit or escape trajectories.

Related Party: (i) Any of the Parties’ directors, officers, agents, employees or
customers

(ii) Any of the Parties’ contractors, subcontractors, or suppliers at any
tier involved directly or indirectly in the performance of this Contract

(iii) Any entity having any right, title or interest, whether through sale,
lease or service arrangement or otherwise, directly or indirectly, in
the payload, the launch vehicle, or the launch service.

Third Party:Any person or entity other than NASA, the Contractor and Related Parties.
Required Insurance for Liability to Third Parties

(A) The Contractor shall continue in effect or acquire insurance to protect the Parties
and the Related Parties from liability for claims from Third Parties for damage to or
loss of property or personal injury or death arising in connection with the covered
launch activities under this contract. The amount of the required insurance shall be
the maximum amount available in the commercial marketplace at reasonable cost,
but shall not exceed $500 million for each launch. The policy or policies shall name
NASA and the related parties as additional insured parties. Required insurance
coverage shall attach no later than the arrival of the launch vehicle at the launch
site and shall remain in force for at least thirty (30) days following launch.

(B) The Contractor shall provide acceptable evidence to the Contracting Officer of
required insurance no later than thirty (30) days prior to the beginning of the
covered launch activities. The amount of required insurance and the terms and
conditions for the policy or policies shall be subject to review by the Contracting

C-50


In Reply
Refer To

DEFENSE CONTRACT MANAGEMENT AGENCY
DEFENSE CONTRACT MANAGEMENT AGENCY WEST
DEFENSE CONTRACT MANAGEMENT AGENCY OPERATIONS
Two Renaissance Square, 40 North Central Ave. Suite 400
Phoenix Arizona 85004

DCMAW-GPOC February 26, 2004

Ms. Linda Pufpa(t

Orbital Sciences Corporation/Launch systems Group
3380 South Price Road

Chandler, AZ 85284

Dear Ms. Pufpaff,
On 11 February 2004, the DCMA Phoenix Assistant Director of Small Business conducted a review of your
Small Business Utilization Program. Based on this review, a rating of “Acceptable” has been assigned and it has

been determined to be in compliance with Public Laws and Federal Acquisition Regulation.

Provided as an enclosure is a copy of Orbital Sciences Corporation Small Business Utilization Program

Subcontracting Master Plan.
_ Sincerely,
Lbs pacetion

Administrative Cohtracting Officer

Enclosure

Ce:

Mr. James Utter, Sr. Vice President

Ms. Catharine H. Szlembarski, Assistant Director of Small Busincss

04-3


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

21

Standard Launch Services List which shall comply with the requirements of the SOW.
All hardware, software, analyses, and support required to provide each item listed in
Exhibit 2, shall be included in the standard launch service.

All Contract Data Requirements List (CDRL) and Supplemental Data Requirements List
(SDRL) items, identified in Attachment D2 and D3 respectively, shall be included in the
standard launch service.

Launch Vehicle

The standard launch service shall include, as a minimum, the following:

(A) Launch timing capabilities with
(i) Reserved

(ii) Multiple approximately twenty-four (24) hour re-launch attempts in the event of
a launch scrub (with exception of abort inside 16 seconds)

(iii) Launch window as short as 2 seconds

(B) A launch vehicle and Payload Adapter (PA) with appropriate electrical and
mechanical interfaces (as described in Exhibit 1) required for payload integration
and testing.

(C) A payload separation system with the following characteristics:

(i) The payload shall be protected from debris generated by the separation
system.

(ii) The separation system shall function in a manner that prevents any re-contact
with the payload, including Contractor-provided attach hardware on the
payload, by the upper stage or any element of the separation system once
separation has been initiated

(iii) Redundant payload separation indications.
(D) A Payload Fairing (PLF) with the following items, as a minimum:

- (i) Two payload access doors of sizes 305 mm x 305 mm (12 in. x 12 in.) for the
63” fairing and 457 mm x 610 mm (18 in. x 24 in.) for the 92” fairing, whose
locations shall be mission unique within the stated structural limitations of the
fairing (defined in Exhibit 1). Additional or different size doors shall be provided
as a non-standard service. The Contractor shall provide payload personnel
access through all standard and non-standard access doors from fairing mate
through final vehicle closeout.

D1B-8


Section C NASA Launch Services Il (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

3.3

3.4

4.0

41

42

(F) Prior to launch of the NASA payload, the proposed common launch vehicle
configuration shall be certified to the required payload risk category

(G) NASA reserves the right to require a specific launch vehicle certification category
and alternative for selected payloads, regardless of the payload risk classification
This determination will be made prior to the Launch Services Task Order (LSTO)
competition.

(H) A launch vehicle certified to a higher category is inherently qualified to launch
payloads designated as a lower risk classification (i.e., launch vehicles certified to
launch vehicle risk category 3 are also certified to launch vehicle risk category 1
and 2).

(I) If no certified launch vehicle configurations exist to meet specific mission
requirements solicited under a NASA request for contract proposal, the Launch
Service Program (LSP) may elect to award a mission contingent on the launch
vehicle configuration achieving certification requirements tailored by NASA

For new launch vehicles and major modifications to certified launch vehicles that do not
require a new certification, NASA may require additional technical insight into the
design, manufacturing, testing, integration, and first launch of the effected systems and
launch vehicle.

In the event of a launch failure of a certified common launch vehicle configuration, LSP
may participate in or perform a failure investigation/return-to-flight board to approve the
cause and corrective action for the launch vehicle configuration to maintain a particular
risk mitigation certification category.

OFF-RAMP CLAUSE
Notification of Discontinued Launch Service Availability

The Contractor may determine, during the life of this contract, that launch services
contracted hereunder are no longer economically viable in the marketplace. In such
event, the Contractor shall provide written notification to the Government at least 12
months prior to the proposed discontinuation of any launch service available under this
contract. The Contractor's notification shall include a brief explanation for the
discontinuation and a request for a contract modification to remove the launch service
If the launch service is the only launch service available under the contract, the
Contractor shall submit a request for a contract modification to terminate the contract at
no cost to either party after the completion of all current contracted orders for the
discontinued launch service. In any event, Launch Service Task Orders existing at the
time of notification shall not be affected.

Reserved


Section D NASA Launch Services II (NLS II)
Exhibit 1B:_ Taurus Capabilities, Specifications and Environments Contract NNK10LB01B

This page left intentionally blank.

E1B-2


Section D NASA Launch Services II (NLS I!)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

8.0 RESERVED

D1B-34


Section B
SF 1449 Continuation

NASA Launch Services II (NLS II)
Contract NNK10LB01B

SECTION B

SF1449 CONTINUATION

B-1


Section D NASA Launch Services II (NLS Il)

Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B
3.0 NON-STANDARD SERVICES ................... becteeeeees D1B-30
4.0 MISSION UNIQUE REQUIREMENTS. bette teeteeteeesreer eee D1B-31
41 Mission Unique Hardware : vette tee ees een see ee veers, D1B-31
42 Mission Unique Software becseeeees bees see D1IB-31
43 Unanticipated Mission Unique Services...........0... 0.00000 DIB-31
5.0 SPECIAL TASK ASSIGNMENTS..............0..0...... bectreeeeeee, DIB-32
6.0 INFORMATION TECHNOLOGY SECURITY......00.0000.0.. eee DIB-32
7.0 GUIDELINE DOCUMENTS............ 0.0.00... biti ttre eee, DIB-32
8.0 RESERVED .............. D1B-34

EXHIBIT 1B TAURUS CAPABILITIES, SPECIFICATIONS AND ENVIRONMENTS
E1B.1 VEHICLE CONFIGURATION
E1B.2 PAYLOAD DELIVERY CAPABILITY
E1B.3 INSERTION ACCURACIES
E1B.4 PAYLOAD SEPARATION ATTITUDE ACCURACY AND RATES
E1B.5 PAYLOAD FAIRING (PLF)
E1B.6 MECHANICAL INTERFACE
E1B.7 ELECTRICAL INTERFACE
E1B.8 PAYLOAD ENVIRONMENT
E1B.9 PAYLOAD ENVIRONMENT INSTRUMENTATION
E1B.10 GENERIC SECONDARY PAYLOAD CHARACTERISTICS/INTERFACE
EXHIBIT 2B TAURUS STANDARD LAUNCH SERVICES LIST
EXHIBIT 3B TAURUS NON-STANDARD SERVICES LIST
EXHIBIT 4 SAMPLE CERTIFICATE OF FLIGHT READINESS
EXHIBIT 5 RESERVED
EXHIBIT 6 RESERVED
EXHIBIT 7 LAUNCH VEHICLE CERTIFICATION DATA
EXHIBIT 8 MISSION INTERFACE CONTROL DOCUMENTS (ICD)

EXHIBIT 9 LAUNCH SERVICE TASK ORDER MISSION SOLUTIONS

D1B-4



Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

35.0 RESERVED
36.0 LISTING OF CLAUSES INCORPORATED BY REFERENCE

NOTICE: The following contract clauses pertinent to this section are hereby
incorporated by reference:

36.1 FEDERAL ACQUISITION REGULATION (48 CFR CHAPTER 1) CLAUSES

FAR 52.202-1 Definitions (Jul 2004)

FAR 52.211-14 Notice of Priority Rating for National Defense, Emergency
Preparedness, and Energy Program Use (Apr 2008)

FAR 52.215-1(c)(3) Instructions to Offerors-Competitive Acquisition (Jan 2004)

FAR 52.222-1 Notice to the Government of Labor Disputes (Feb 1997)
FAR 52.227-14 Rights in Data—General (Dec 2007)

FAR 52.227-14 Rights in Data—General (Dec 2007) Alternate II (Dec 2007)
FAR 52.227-14 Rights in Data—General (Dec 2007) Alternate Ill (Dec 2007)
FAR 52.232-18 Availability of Funds (Apr 1984)

FAR 52.233-1 Disputes (July 2002)

FAR 52.242-15 Stop-Work Order (Aug 1989)

FAR 52.243-1 Changes—Fixed-Price (Aug 1987) Alternate | (Apr 1984)
FAR 52.246-4 Inspection of Services—Fixed-Price (Aug 1996)

FAR 52.246-25 Limitation of Liability--Services (Feb 1997)

C-59


Section D

NASA Launch Services II (NLS I!)

Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C5-4

MISSION UNIQUE DRAWINGS

DESCRIPTION/PURPOSE:

This data item identifies the mission unique configuration

DATA REQUIREMENTS:

All Launch Vehicle and Ground Support equipment mission unique drawings showing all sub-
tier mission specific installations, including all mechanical and electrical interfaces. This shall
include, but is not limited to:

(A)

(B)

Upper stage and payload adapter mission specific drawings showing all sub-tier
mission unique installations, including all payload mechanical interfaces.

All payload adapter and fairing installation drawings showing all sub-tier mission
unique installations.

Top-level vehicle system specification drawings showing all sub-tier mission
unique installations.

All schematics harness drawings, and assembly drawings for mission unique
electrical hardware

A drawing tree showing all mission specific drawings

D2-49


Section D NASA Launch Services II (NLS II)
Exhibit 1A: Pegasus Capabilities, Specifications and Environments Contract NNK10LB01B

This page left intentionally blank

E1A-30


Section C NASA Launch Services I (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

44.0 USE OF GOVERNMENT PRODUCTION, RESEARCH PROPERTY, TOOLING, AND
FACILITIES ON A NO-CHARGE BASIS

In performing this contract, the Contractor and its Subcontractors are authorized to use on a
no-charge, noninterference basis the Government-owned production, research property
(including tooling, test equipment, and facilities), provided under the contract(s) specified
below and identified in the cognizant Contracting Officer's letter approving use of the property.
Use is authorized on the basis that it will not interfere with performance of the Government
contract(s) under which the property was originally furnished and is accountable. Use shall be
in accordance with the terms and conditions of these contracts and the cognizant Contracting
Officer's approval letter.

C-70


Section D NASA Launch Services (NLS I!)
Attachment D5: Safety and Health Plan Contract NNK10LB01B

ATTACHMENT D5

SAFETY AND HEALTH PLAN


Section C

NASA Launch Services || (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

CONTRACT TERMS AND CONDITIONS

1.0 FAR 52.212-4 CONTRACT TERMS AND CONDITIONS--COMMERCIAL ITEMS (MAR
2009) (TAILORED)

(a)

Inspection/Acceptance. Pursuant to FAR Subpart 12.402(b), FAR clause 52.246-
11 Higher-Level Contract Quality Requirement (Feb 1999) shall govern and apply to
this contract and is provided in full text in Section C, Clause 16.0. For launch
service Contract Line Item Numbers (CLINs) prior to launch, the provisions of FAR
clause 52.246-4 Inspection of Services—Fixed-Price (Aug 1996) shall govern and
apply to this contract and is incorporated by reference under contract Section C,
Clause 36.0. The Government reserves the right to perform in-process inspection
or testing of any supplies or launch services tendered for acceptance prior to
launch. .

The Government will accept only those launch services that successfully deliver a
separated and undamaged payload to the proper orbit conditions and insertion
accuracies and do not exceed the environmental parameters stated in the Interface
Control Document (ICD) except as otherwise provided in this contract. Acceptance
of launch service CLINs, and remedies for partial or failed missions shall be in
accordance with contract Section C, Clause 24.0, Mission Success Determination,
Investigation, and Corrective Actions The Contractor shall only tender for
acceptance those items conforming to the contract requirements. For supplies or
services other than launch services, the Government will require repair or
replacement of nonconforming supplies or re-performance of nonconforming
services at no increase in contract price. For launch services, the Government
must exercise its post-acceptance rights within the time specified in contract
Section C, Clause 24.0, Mission Success Determination, Investigation, and
Corrective Actions. For supplies or services other than launch services, the
Government must exercise its post-acceptance rights:

(1) Within a reasonable time after the defect was discovered or should have been
discovered; and

(2) Before any substantial change occurs in the condition of the item, unless the
change is due to the defect in the item

Assignment. The Contractor or its assignee may assign its rights to receive
payment due as a result of performance of this contract to a bank, trust company,
or other financing institution, including any Federal lending agency in accordance
with the Assignment of Claims Act (31 U.S.C.3727). However, when a third party
makes payment (e.g., use of the Government wide commercial purchase card), the
Contractor may not assign its rights to receive payment under this contract.

Changes. FAR clause 52.243-1 Changes - Fixed-Price (Aug 1987) Alt | (Apr 1984)
is hereby incorporated by reference under contract Section C, Clause 36.0. The

C6


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-13
FINAL FLIGHT REPORT
DESCRIPTION/PURPOSE:

After each launch, a final post-flight report shall be provided. This report will support the NASA
Contracting Officer's mission success determination.

DATA REQUIREMENTS:

(A) This report shall include, in its entirety, the Contractor's internal post-flight report
produced for each mission.

This report shall also include:

(i) Orbit elements determined from vehicle guidance data

(ii) Vehicle data indicating payload separation

(iii) Pre-flight prediction of expected flight environments (i.e., acoustic/vibration,
quasi-static acceleration, thermal, and pressure). Generic vehicle environmental
data may be submitted unless mission unique environmental requirements are
identified in the ICD

(iv) Post flight determination of actual flight environments

(v) Explanation of significant differences between the predicted and actual flight
environments

(vi) | Vehicle sequence and attitudes data

(vii) Payload tracking and telemetry data that is interleaved in the launch vehicle data
stream

(B) This report shall also specifically address each ICD orbital parameter and environmental

condition using flight data, ground observations, or other data sources in accordance
with the determination methods proposed by the Contractor under CDRL C2-5.

0245


CDM RELEASED

ortyjfal

NASA LAUNCH SYSTEMS (NLS) RELIABILITY PLAN

to the export control laws of the U.S. Government.

WARNING: INFORMATION SUBJECT TO U.S. EXPORT CONTROL LAWS. The attached documents
contain technical data within the definition of the International Traffic in Arms Regulations, and are subject

PREPARED BY

Orbital Sciences Corporation
Launch Systems Group
CAGE Code 9X711

ORIGINAL ISSUE DATE
11 JUNE 2004

TM-18473
1 SEPTEMBER 2009
CODE A1-0-A7

REVD



Section D NASA Launch Services I! (NLS II)
Attachment D10: Acronyms and Abbreviations Contract NNK10LB01B

This page left intentionally blank.

D10-8


Section D NASA Launch Services I! (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C1-5

OPERATIONS DOCUMENTATION FOR PROCESSING IN NASA PROVIDED PAYLOAD
PROCESSING FACILITIES

DESCRIPTION/PURPOSE:

This item covers the submission of documentation to NASA when performing operations in a
NASA-provided facility in support of this contract.

DATA REQUIREMENTS:

The following items shall be submitted for the launch vehicle hardware and operations to be
brought in a NASA-provided PPF.

« Launch Vehicle requirements for operations in the NASA-provided facility, including
facility, processing, security, contamination and processing contingency plans.
o Initial submittal date 18 months prior to launch.
« Documentation of any hazardous waste that the launch vehicle will produce in the
NASA-provided facility
o Initial submittal date sixty (60) days prior to arrival.
e Non-hazardous Launch vehicle standalone procedures to be used in the NASA-
provided facility.
o Initial submittal date forty-five (45) days prior to use.
e Launch vehicle personnel badging and training requirements to include any medical
certifications.
o Initial submittal date ninety (90) days prior to arrival

D2-12


Section D

NASA Launch Services II (NLS II)

Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

(i) All technical problems and design anomalies have been resolved without
compromising system performance, reliability and safety.

(ii) The detailed design will meet performance, functional requirements, and
schedule

(iii) Software simulations and prototyping results do not present any potential
mission risks.

(iv) All key subsystem and/or component engineering analyses are complete.

(v) Integrated safety analysis identifying any remaining hazards and proposed
resolution.

(vi) Launch vehicle/payload compatibility test plans have been defined.
(vii) 90% mission unique drawings released
Mission Specific System Acceptance Review (MSSAR)

The NLS Contractor shall conduct an MSSAR after the design, fabrication,
qualification testing and analysis is complete and shall incorporate any flight data
available as part of the launch service. The Contractor shall address all mission
specific items for the payload and mission requirements to verify qualification,
compliance, and systems-level compatibility using completed analyses, test,
inspection, and demonstrations results. The mission unique system acceptance
shall be subject to NASA’s approval. NASA reserves the right to withhold approval
until all action items have been closed. As a minimum, the Contractor shall provide
verification of the following items at the MSSAR:

(i) Results of the mission specific acceptance reviews of the major suppliers or
major subsystems;

(ii) Design changes that occurred subsequent to MSCDR or changes as a result of
new flight data;

(iii) Summary of applicable component tests (test setups, test cases, results and
significant anomalies), analyses, margins, or similarity assessments. Included
in the summary is component qualification rationale (similarity, test, analysis)
for all affected components that are new, changed or subject to new
environments or functional requirements;

(iv) Qualification rationale for the system as a whole;

(v) Methodology and results of current analyses.

D1B-13


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.3.3

2.4

2.4.1

Limiting Orbital Debris. The number of submittals for the Standard Mission Analyses
are identified in Table D2-A.

Mission Success Determination

Mission success will be based on the criteria set forth in Section C, paragraph 24.1,
Mission Success Criteria. Mission success determination requirements are detailed in
Section C, paragraph 24.2, Mission Success Determination.

The Contractor shall prepare and submit a Quick Look Flight Report (CDRL C4-12) and
a Final Flight Report (CDRL C4-13). Within thirty (30) days of receipt of the Final Flight
Report, the Contracting Officer will either determine the launch a Mission Success or
inform the Contractor of the Government's intent to withhold determination for payload
evaluation

Launch Site Support

Pre-Launch Checkout and Launch Support

2.4.1.1. Launch Vehicle Preparation and Launch

For launch services provided under this contract, the Contractor shall, as a minimum;

(A) Perform all launch vehicle preparations and launch site operations necessary to
safely and successfully deliver the payload to the desired orbit.

(B) Generate the required documents (CDRL C3-7) and obtain all required safety
approvals for the launch vehicle system and integrated payload/launch vehicle
system operations including payload/launch vehicle system integration and launch
operations

(C) Provide NASA insight as defined in Article C25, to schedule meetings, test
briefings, and technical meetings. Upon request, the Contractor shall provide
copies of schedules, test briefings, and other material presented at technical
meetings.

(D) Conduct launch vehicle/launch site walk-downs with NNC participation.
(E) Comply with the submittal and operational requirements for all NASA provided

facilities occupied during launch vehicle processing (CDRL C1-5). Failure to
comply may result in denied access to the NASA provided facility.

2.4.1.2 Telemetry Data and Launch Countdown Support

D1B-19


Section D NASA Launch Services II (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: S6-2
END TO END LINK TEST PLAN
DESCRIPTION/PURPOSE:

To provide a test plan that verifies the telemetry (RF and hardwire), voice communication
channels and video links from the Contractor's site to NASA’s designated NASA LSP Data
Center. The plan will describe the telemetry links from the launch vehicle through the Range
and down range deployable telemetry receiving assets specific to that mission. This plan will
verify NASA's ability to receive, process, display and verify telemetry, voice communication
channels and video from the Contractor's site prior to launch vehicle testing.

DATA REQUIREMENTS:

The end-to-end link test plan shall address how the Contractor will test all links from the
Contractor's site to NASA's designated NASA LSP Data Center. The plan shall address scope;
organizations involved and points of contact for each; facilities used and/or involved; detailed
information on telemetry signals, voice communication channels and video sources and
transmission rates. The plan shall identify and/or suggest orbiting or ground locations and/or
mobile assets to meet LSP telemetry coverage requirements prior to launch. The plan shall
describe the coordination/scheduling/conducting of pre-launch data flow tests to ensure real-
time connectivity of voice and data paths between the down range assets and the NASA
designated NASA LSP Data Center.

D3-13


Section D NASA Launch Services II (NLS II)

Attachment D2: Contract Data Requirements List Contract NNK10LB01B
Item Document Approval! Initial Submittal | Subsequent | No. of
Review Date Submittal Date] Copies

C2: Mission Integration

IC2-1.1" |Interface Control Document (ICD) Approval Preliminary ICD at |Baseline ICD at 10
ATP+ 6M L-15M and
AJR
IC2-1.2* Interface Control Document (ICD) Approval NLT 3 months after} A/R or with 3
Requirements Verification Matrix Preliminary ICD each ICD
CDRL approval revision
IC2-2* |Mission Specific Program Requirements |Approval AIR As Changed 3
[Document/ Operational Requirements
(PRD/OR)
IC2-3*  |Launch Vehicle Detailed Mission Approval AJR As Changed 3

Requirements (DMR)
IC2-4*  |Reserved

IC2-5* —_|Mission Success Criteria & Approval NLT L-4M As Changed 5
Determination Methodology

* Required per mission

Item Document Approval/ Initial Submittal | Subsequent | No. of
Review Date Submittal Date] Copies

C3: Safety & Mission Assurance

C3-1 Alert System Documentation Review Dispo + 1M AIR 2
IC3-2 Mishap Notification, Investigation and {Review AIR in CORL AIR 2
Mishap Preparedness, and Contingency
Plan
C3-3 !SO 9001/2000 Certification Certificate {Review Upon Upon 1
(ISO 9001/2008 Certification Certificate Recertification Recertification
after November 2010)
IC3-4 Quality Management System (QMS) Review Contract Award | When Revised 2
land SupplierM/endor Audit/Assessment +45 Days
Schedules
IC3-5 QMS and Supplier/Vendor Review As Generated Per Internal or 2
|Audit/Assessment Report External Audit
iC3-6 Risk Management Plan Approval At Contract Annual Review 2
Award Plus 90 And Updates
Days AJR
(1 Electronic
and 1 Paper
Copy)
IC3-7* _|Safety Documentation for Processing In {Approval for AYR in CORL AIR 2
NASA Provided Facilities INASA owned
facilities; Review
for NASA
procured
facilities

* Required per mission
TABLE D2-A: CDRL INDEX (Cont.)

D2-4


Section D . NASA Launch Services II (NLS I!)
Exhibit 6: Reserved Contract NNK10LB01B

EXHIBIT 6

RESERVED

Table D1-Y: Reserved

E6-1


Section C
Contract Terms and Conditions Contract NNK10LB01B

NASA Launch Services II (NLS II)

42.0

(i)

(k)

(I)

Criminal penalties. Any individual director, officer, or employee of the contractor
or of its subcontractors and suppliers who are indemnified under the provisions of
this clause are subject to criminal penalties, pursuant to 223(c) of the Act, for
knowing and willful violation of the Atomic Energy Act of 1954, as amended, and
applicable DOE nuclear safety-related rules, regulations or orders which violation
results in, or, if undetected, would have resulted in a nuclear incident.

Inclusion in subcontracts. The contractor shall insert this clause in any
subcontract which may involve the risk of public liability, as that term is defined in
the Act and further described in paragraph (d)(2) above. However, this clause
shall not be included in subcontracts in which the subcontractor is subject to
Nuclear Regulatory Commission (NRC) financial protection requirements under
section 170b. of the Act or NRC agreements of indemnification under section
170c. or k. of the Act for the activities under the subcontract.

Effective date. This indemnity agreement shall be applicable with respect to
nuclear incidents occurring on or after August 20, 1988.

1852.228-78 CROSS-WAIVER OF LIABILITY FOR SCIENCE OR SPACE

EXPLORATION ACTIVITIES UNRELATED TO THE INTERNATIONAL SPACE
STATION (DEVIATION) (OCT 2009)

(a) The purpose of this clause is to extend a cross-waiver of liability to NASA
contracts for work done in support of Agreements between Parties involving
Science or Space Exploration activities, unrelated to the International Space
Station (ISS), but which involve a launch. This cross-waiver of liability shall be
broadly construed to achieve the objective of furthering participation in space
exploration, use, and investment.

(b) As used in this clause, the term:

(1) “Agreement” refers to any NASA Space Act agreement that contains the cross-

waiver of liability provision authorized in 14 CFR 1266.104.

(2) "Damage" means:
(i) Bodily injury to, or other impairment of health of, or death of, any person;
(ii) Damage to, loss of, or loss of use of any property;
(iii) Loss of revenue or profits; or

(iv) Other direct, indirect, or consequential Damage;

C-65


Section D NASA Launch Services II (NLS II)
Attachment D4: SB and SDB Subcontracting Plan Contract NNK10LB01B

ATTACHMENT D4

SMALL BUSINESS AND SMALL DISADVANTAGED BUSINESS
SUBCONTRACTING PLAN

D4-1


Section C NASA Launch Services II (NLS Il)
Contract Terms and Conditions Contract NNK10LB01B

7.5

8.0

8.1

8.2
8.3

8.4

8.5

(E) The Contractor has the power to enter into this contract and accept payments, and
has taken all necessary actions to authorize the acceptance under the terms of this
contract.

(F) The assets of the Contractor are not subject to any lien or encumbrance of any
character, which would jeopardize performance under this contract, except for
current taxes not delinquent and except as shown in the financial statements
There is no current assignment of claims under any contract affected by these
payment provisions.

(G) All information furnished by the Contractor to the administering office in connection
with each request for payment is true and correct.

(H) These representations and warranties shall be continuing and shall be considered
to have been repeated by the submission of each invoice for payments.

Work Plan Submission. The Contractor shall comply with the Work Plan that identifies
the major milestone events and a corresponding narrative of the work activity necessary
to accomplish the major milestone events.

SCOPE OF WORK - SPECIAL TASK ASSIGNMENTS (STUDIES AND ANALYSES)
(CLIN 10)

The Contractor shall perform specific task assignments that will be defined through the
issuance of task orders in accordance with contract Section C, Clause 9.0, Ordering
Procedure and Payment for Special Task Assignments (Studies and Analyses) (CLIN
10) and paragraphs 8.3 and 8.4 herein.

Reserved

Only hours expended against specific written task orders authorized by the Contracting
Officer shall be paid under this contract. Task orders shall be performed on an FFP,
completion-effort basis. The Government is under no obligation to reimburse the
Contractor for any costs, which exceed the Firm-Fixed-Price authorized on each task
order.

The Government may require Special Task Assignments (Studies and Analyses) in any
calendar year from 2010 (Jul-Dec) through 2022 at the FFP composite labor rates
identified in Section B, paragraph 1.5. Pricing may be offered for any or all of the
calendar years remaining on the NLS contract, i.e., calendar years 2010 (Jul-Dec)
through 2022. At a minimum, the Contractor shall provide pricing through 2015. The
Contractor shall submit pricing for calendar years beyond 2015 not yet proposed, no
later than the CY 2014 On-Ramp period. The proposed labor rates shall be negotiated
using the applicable procedures of FAR Part 15 and incorporated herein.

Reserved

C-23


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-8
INTEGRATED THERMAL ANALYSIS
DESCRIPTION/PURPOSE:

The purpose of this CDRL is to quantify payload thermal environments in various operational
configurations (pre-launch and in-flight). The scope of this analysis may vary depending on
the complexity of the payload and upper stage thermal interfaces.

DATA REQUIREMENTS:

The integrated thermal analysis that is performed using the PGAA shall utilize current standard
methodologies (e.g. Monte Carlo ray tracing techniques), not restrict the payload model size to
less than 1000 thermal nodes or 2000 geometric surfaces and shall include, to the fidelity
required by the thermal interfaces:

(A) | Temperature time histories at selected locations (identified by the payload) in the
payload thermal model

(B) Description of all inputs, assumptions, boundary conditions, and analytical
methods used to perform the analysis, including the following components:

(i) Pre-launch payload fairing ECS gas conditioning analyses

(ii) Payload fairing aeroheating

(iii) Trajectory simulation assumptions relative to the actual PGAA.
(iv) | Ascent and on orbit (up to payload separation) analyses.

(C) Summary of results identifying maxima and minima (for the selected locations of
interest, identified by the payload) and the times and flight events at which they
occur.

(D) — Input and output thermal analysis files used for the documented analyses.

D2-39


Section D NASA Launch Services II (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

2.4.1.2.3, Launch Countdown and Flight Support

The Contractor shall provide launch countdown procedures, Mission Constraints
Documents (CDRL C1-2) and a Mission Console Notebook (CDRL C1-3) for the launch
dress rehearsal and launch in hard copy and a mutually agreed upon electronic format.

The Contractor shall provide up to eight NASA personnel access to consoles, with
vehicle monitoring capabilities, co-located within the Contractor's launch control center.
The Contractor shall provide access to real-time telemetry (RF and hardwire), voice
communication channels with talk/listen capabilities, video and telephones for the co-
located NASA personnel. To the extent possible, the Contractor shall implement the
NASA provided console communications configuration for those consoles occupied by
the NASA team within the Contractor's launch control center. The Contractor shall
support validation of this configuration with the designated NASA LSP Data Center prior
to launch dress rehearsal and launch

The Contractor shall deliver real-time launch vehicle and GSE telemetry (RF and
hardwire), voice communication channels and video to the designated NASA LSP Data
Center from the start of launch countdown through Range Loss of Signal (LOS) when in
range of an existing ground receiving station, or as supplemented as described in SOW
paragraph 2.4.3, Range Support and Services. If the launch vehicle telemetry, voice
communication channels or video is uniquely encoded, the Contractor shall provide the
decoded launch vehicle telemetry, voice communication channels, and video to the
NASA LSP Data Center.

The Contractor shall receive and record the raw launch vehicle telemetry data for all
phases of powered flight, from two (2) minutes prior to stage ignition through 10
seconds after payload separation IAW NASA Policy LSP-PD-120.05. NASA shall
provide any downrange telemetry assets required if the Range utilized is unable to
support with its existing ground assets.

The Contractor shall provide real-time transmission back to the NASA designated NASA
LSP Data Center of all mandatory receive and record launch vehicle telemetry coverage
times IAW NASA Policy LSP-PD-120.05. The Contractor shall provide the raw
telemetry data recorded post launch (SDRL S6-3)

During the Launch Countdown, the Contractor shall poll NASA at key milestone events
for GO/NO-GO status. The final poll shall include the NASA Launch Manager's
GO/NO-GO status for launch. The Contractor shall provide NASA access to anomalies
and concurrence with anomaly resolution prior to proceeding with Launch Countdown.
The Contractor shall poll NASA for any recycle of the Launch Countdown

On day of launch, the Contractor shall maintain voice contact with the downrange
assets and provide status/readiness to the launch team as requested.

D1A-22


Section C

NASA Launch Services II (NLS Il)

Contract Terms and Conditions Contract NNK10LB01B

(iii)

Pursuant to FAR 16.505(a)(9), No protest under Subpart 33.1: is
authorized in connection with the issuance or proposed issuance of an
order under a task-order contract or delivery-order contract, except for—

(A) A protest on the grounds that the order increases the scope, period,
or maximum value of the contract; or

(B) A protest of an order valued in excess of $10 million. Protests of
orders in excess of $10 million may only be filed with the Government
Accountability Office, in accordance with the procedures at 33.104.

The authority to protest the placement of an order under FAR 16.505(a)(9)
expires on May 27, 2011. (10 U.S.C. 2304a(d) and 2304c(d), and 41
U.S.C. 253h(d) and 253)(d)).

Pursuant to FAR 16.505(b)(1)(iii), for task or delivery orders in excess of
$5 million, the requirement to provide all awardees a fair opportunity to be
considered for each order shall include an opportunity for a post-award
debriefing in accordance with FAR 16.505(b)(4).

Launch Service Task Order Mission Solutions will be attached to the contract
(Exhibit 9) upon award of task orders.

(F) Modifications to LSTOs. After an LSTO is issued, it may be necessary to add
priced non-standard services to the LSTO. These additions will be accomplished
via modifications to the original LSTO. In addition, mission uniques that are not
included in the priced non-standard services may be added to, or deleted from
LSTOs via modification to the original LSTO. In this instance, the terms of the
existing LSTO, such as price, milestone events, and Work Plan completion criteria,
may be modified to reflect the change. The remainder of the price of the
modification will be applied to the remaining payment milestone event amounts, as
performance dictates.

(G) Task Order Authorization and Content. The only persons authorized to issue task
orders under this contract are the KSC Contracting Officers. Task orders will be
issued in writing. However, any facsimile, or electronic, task orders issued by the
Contracting Officer will be confirmed in writing within five (5) business days. The
Contractor will acknowledge receipt and acceptance of the task order by signing the
task order and returning it to the Contracting Officer. Each task order will include
the following information:

(i)
(ii)
(iii)

Date of the task order
Contract number and task order number

Statement of Work and any other documentation on which the price is based

C-30


Section D NASA Launch Services II (NLS Il)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: S5-1
VEHICLE TEST PROCEDURES

DESCRIPTION/PURPOSE:

Procedures for various operations involving launch vehicle processing, testing, and checkout.
DATA REQUIREMENTS:

Launch Vehicle processing procedures will be made available for review in support of NASA
insight requirements (in accordance with Contract Clause C25.8) at the site where specific
vehicle processing occurs. On a case-by-case basis, the Contractor will provide electronic

versions of these test procedures. The Contractor will provide a current list of vehicle
processing procedures upon request.

D3-11


Section D NASA Launch Services II (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: S3-3
AS BUILT CONFIGURATION LIST

DESCRIPTION/PURPOSE:

A document describing the as-built configuration of each launch vehicle.

DATA REQUIREMENTS:

The document shall include a listing of all serialized components. The listing shall identify the
“As-Designed” part number, revision, and description, as well as the “As-Built” part number,

revision, serial number, installation work package and any applicable incorporated changes for
each item listed.

D3-7


Section D
Exhibit 2B: Taurus Standard Services

NASA Launch Services ! (NLS I!)

Contract NNK10LB01B

4

SOW

Dara

Standard Service

E2B-4

Description



Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

X (26) 52.222-54, Employment Eligibility Verification (Jan 2009) (Executive
Order 12989). (Not applicable to the acquisition of commercially available off-
the-shelf items or certain other types of commercial items as prescribed in
22.1803.)

(27) (i) 52.223-9, Estimate of Percentage of Recovered Material Content for
EPA-Designated Items (May 2008)(42 U.S.C. 6962(c)(3)(A)(ii)). (Not
applicable to the acquisition of commercially available off-the-shelf items.)

(ii) Alternate | (May 2008) of 52.223-9 (42 U.S.C. 6962(i)(2)(C)). (Not
applicable to the acquisition of commercially available off-the-shelf items.)

(28) 52.223-15, Energy Efficiency in Energy-Consuming Products (Dec 2007)
(42 U.S.C. 8259b).

(29) (i) 52.223-16, IEEE 1680 Standard for the Environmental Assessment of
Personal Computer Products (Dec 2007) (E.O. 13423).

(ii) Alternate 1 (Dec 2007) of 52.223-16

(30) 52.225-1, Buy American Act-Supplies (Feb 2009)(41 U.S.C. 10a-10d).
(31) (i) 52.225-3, Buy American Act-Free Trade Agreements-Israeli Trade Act
(Jun 2009) (41 U.S.C. 10a-10d, 19 U.S.C. 3301 note, 19 U.S.C. 2112 note,
19 U.S.C. 3805 note, Pub. L. 108-77, 108-78, 108-286, 108-301, 109-53,
109-169, 109-283, and 110-138).

(ii) Alternate | (Jan 2004) of 52.225-3.

(iii) Alternate II (Jan 2004) of 52.225-3

(32) 52.225-5, Trade Agreements (Aug 2009) (19 U.S.C. 2501, et seq., 19
U.S.C. 3301 note).

(33) 52.225-13, Restrictions on Certain Foreign Purchases (Jun 2008)(E.0O.'s,
proclamations, and statutes administered by the Office of Foreign Assets
Control of the Department of the Treasury).

(34) 52.226-4, Notice of Disaster or Emergency Area Set-Aside (Nov 2007)
(42 U.S.C. 5150)

(35) 52.226-5, Restrictions on Subcontracting Outside Disaster or Emergency
Area (Nov 2007) (42 U.S.C. 5150).

C-55


Section D NASA Launch Services II (NLS II)
Attachment D4: SB and SDB Subcontracting Plan Contract NNK10LB01B

Table |

Individual Subcontracting Goals for: NASA LAUNCH SERVICES (NLS)

Contract/Proposal Number: RFP 10-99-0021- Rev D

The Subcontract value of direct material has been purposed at an unburdened total of:

$ TBP
Category Pegasus Taurus
Large Business Subcontract Dollars TBP TBP
Large Business Subcontract Percentage Goal
Small Business Subcontract Dollars* TBP TBP
Small Business Subcontract Percentage Goal* 5% 5%
Veteran-Owned Small Business Subcontract Dollars TBP TBP
Veteran-Owned Small Business Subcontract Percentage Goal 25% 25%
Service-Disabled VO Small Business Subcontract Dollars TBP TBP.
Service-Disabled VO Small Business Subcontract Percentage Goal 25% 25%
HUBZone Small Business Subcontract Dollars TBP TBP
HUBZone Small Business Subcontract Percentage Goal 25% 25%
Small Disadvantaged Business Subcontract Dollars** TBP TBP
Small Disadvantaged Business Subcontract Percentage Goal** 1% 1%
Women-Owned Small Business Subcontract Dollars TBP TBP
Women-Owned Small Business Subcontract Percentage Goal 1% 1%

* The Small Disadvantaged Business, Veteran-Owned Small Business, Service-Disabled Veteran-Owned Small
Business, HUBZone Small Business, Small Disadvantage Business, Women-Owned Small Business, HBCUs and
OMEIs (or Mls) dollars and percentages are rolled into the Small Business dollars and goals.

** HBCUs and OMEIs (or Mls) dollars (TBP) and percentages (.25%) are rolled into the Small Disadvantaged
Small Business dollars and goals.

See Master Subcontracting Plan for additional plan elements.

D4-11


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10L801B

CDRL DESCRIPTION Number: C2-2

MISSION SPECIFIC PROGRAM REQUIREMENTS DOCUMENT/OPERATIONAL
REQUIREMENTS (PRD/OR)

DESCRIPTION/PURPOSE:

The Mission Specific Program Requirements Document (PRD) and Operational Requirements
(OR) identifies specific support services provided by the Range. Range support services
required by NASA and the Contractor are submitted to the Range through the PRD and OR

DATA REQUIREMENTS:

The Mission Specific PRD/OR, or equivalent mission specific Range support request
documentation for the proposed launch site(s), shall be submitted to obtain Range support.
The Contractor, with support from NASA/KSC, completes all forms appropriate to the mission
in the format required by the Range and submits them to the appropriate Range for formal
acceptance.

D2-18


Section D

NASA Launch Services II (NLS II)

Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B
Document No Rev. Document Title
MIL-STD-176 A, Weight and Balance Data Reporting Forms for Guided
Notice 1 Missiles and Space Launch Vehicles
MIL-STD-1773 Notice 1 Fiber Optics Mechanization of an Aircraft Internal Time
Division Command/Response Multiplex Data Bus
IEST-STD-CC1246 D Product Cleanliness Levels and Contamination Control
2002 Program
MIL-PRF-27401 F Propellant Pressurizing Agent, Nitrogen
2008
ASTM E1216 2006 Standard Practice for Sampling for Particulate
Contamination by Tapelift
ASTM E1235 2008 Standard Test Method for Gravimetric Determination of
Nonvolatile Residue (NVR) in Environmentally Controlled
Areas for Spacecraft
NASA RP-1124 4 Outgassing Data for Selecting Spacecraft Materials
1997
NPR 2810.A 2006 Security of Information Technology

NASA-STD-8729.1

NPD 8610.23
NPD 8610.24

NPD 8610.7

LSP-PLN-324.01
NPR 8621.1

LSP-PLN-353.01
NPD 1280.1
NPR 7120.5

NPR 8715.3
1

Planning, Developing and Managing an Effective Reliability
and Maintainability (R&M) Program

Launch Vehicle Technical Oversight Policy

Launch Services Program (LSP) Pre-Launch Readiness
Reviews

Launch Services Risk Mitigation Policy for NASA-Owned
and/or NASA-Sponsored Payloads/Missions

Expendable Launch Vehicle Certification

NASA Procedural Requirements for Mishap and Close Call
Reporting, Investigating, and Recordkeeping

Launch Services Program Risk Management Plan
NASA Management System Policy

NASA Space Flight Program and Project Management
Requirements

NASA General Safety Program Requirements

MIL-STD-1773 may be substituted

D1B-33


Section C
Contract Terms and Conditions Contract NNK10LB01B

NASA Launch Services II (NLS II)

13.0

(b)

Maximum-order. The Contractor is not obligated to honor—
(1) During any calendar year, any order for a single item in excess of

6 Pegasus and 6 Taurus Launch Services or
Unlimited Special Task Assignments or
Unlimited Non-Standard Services

(2) Any order for a combination of items in excess of 6 Pegasus and 6 Taurus
Jaunch services; or

(3) A series of orders from the same ordering office within thirty (30) days that
together call for quantities exceeding the limitation in paragraph (b) (1) or (2) of
this clause

Reserved

Notwithstanding paragraphs (b) and (c) of this clause, the Contractor shall honor
any order exceeding the maximum order limitations in paragraph (b), unless that
order(s) is returned to the ordering office within thirty (30) days after issuance, with
written notice stating the Contractor's intent not to ship the item(s) called for and the
reasons. Upon receiving this notice, the Government may acquire the supplies or
services from another source.

52.216-22 INDEFINITE QUANTITY (OCT 1995) [Note: Applicable to IDIQ contract
portion only]

(a)

This is an indefinite-quantity contract for the supplies or services specified and
effective for the period stated, in Section B and C of the Schedule. The quantities of
supplies and services specified in the Schedule are estimates only and are not
purchased by this contract.

Delivery or performance shall be made only as authorized by orders issued in
accordance with contract Section C, Clause 11.0, FAR 52.216-18, Ordering (Oct
1995). The Contractor shall furnish to the Government, when and if ordered, the
supplies or services specified in the Schedule up to and including the quantity
designated in the Schedule as the "maximum." The Government shall order at least
the quantity of supplies or services designated in the Schedule as the "minimum."

Except for any limitations on quantities in contract Section C, Clause 12.0, FAR
52.216-19 Order Limitations (Oct 1995) or in the Schedule, there is no limit on the
number of orders that may be issued. The Government may issue orders requiring
delivery to multiple destinations or performance at multiple focations.

Any order issued during the effective period of this contract and not completed
within that period shall be completed by the Contractor within the time specified in

C-26


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

concerns) exceeds $550,000 ($1,000,000 for construction of any public
facility), the subcontractor must include 52.219-8 in lower tier
subcontracts that offer subcontracting opportunities.

(ili) Reserved
(iv) 52.222-26, Equal Opportunity (Mar 2007) (E.O. 11246).

(v) 52.222-35, Equal Opportunity for Special Disabled Veterans, Veterans of
the Vietnam Era, and Other Eligible Veterans (Sep 2006) (38 U.S.C
4212)

(vi) 52.222-36, Affirmative Action for Workers with Disabilities (Jun 1998) (29
U.S.C. 793).

(vii) Reserved

(viii) 52.222-41, Service Contract Act of 1965, (Nov 2007), flow down required
for all subcontracts subject to the Service Contract Act of 1965 (41
U.S.C. 351, et seq.)

(ix) 52.222-50, Combating Trafficking in Persons (Feb 2009) (22 U.S.C.
7104(g)).

Alternate | (Aug 2007) of 52.222-50 (22 U.S.C. 7104(g)).

(x) 52.222-51, Exemption from Application of the Service Contract Act to
Contracts for Maintenance, Calibration, or Repair of Certain Equipment--
Requirements (Nov 2007) (41 U.S.C. 351, et seq.)

(xi) 52.222-53, Exemption from Application of the Service Contract Act to
Contracts for Certain Services--Requirements (Feb 2009) (41 U.S.C.
351, et seq.)

(xii) 52.222-54, Employment Eligibility Verification (Jan 2009).

(xiii) 52.226-6, Promoting Excess Food Donation to Nonprofit Organizations.
(Mar 2009) (Pub. L. 110-247). Flow down required in accordance with
paragraph (e) of FAR clause 52.226-6.

(xiv) 52.247-64, Preference for Privately-Owned U.S. Flag Commercial
Vessels (Feb 2006) (46 U.S.C. Appx 1241(b) and 10 U.S.C. 2631) (flow
down required in accordance with paragraph (d) of FAR clause 52.247-
64)

While not required, the contractor may include in its subcontracts for
commercial items a minimal number of additional clauses necessary to satisfy
its contractual obligations.


Section D
Attachment D2: Contract Data Requirements List

NASA Launch Services II (NLS I!)
Contract NNK10LB01B

Item Document Approval/ Initial Submittal Subsequent No. of
Review Date Submittal Date | Copies
C4: Analysis
IC4-1*  |Performance and Guidance Initial Later of Later of 3
Accuracy Analysis (PGAA) Submittal = ATP+ 7M L-12M; L-6M
Review, or or
Subsequent | Receipt of Approved Receipt of
Submittals = P/L Data + 2M Approved P/L
Approval Data + 2M
IC4-2*  |Final Mission Analysis (FMA) Approval Receipt of Final P/L AIR 3
Data + 2M
IC4-3* |Payload/Expended Stage Approval Later of L-2M 3
Separation Analysis L-13M
or
Released ICD + 2M
IC4-4*  |Payload Fairing Venting Analysis Approval Receipt of Approved AIR 3
P/L Data + 1M
IC4-5*_|Payload Fairing Clearance Analysis |Approval Receipt of Approved Later of 3
P/L Model + 4M L-15M; L-5M
or
Receipt of
Approved P/L
Model + 4M
IC4-6*  |Pre-Flight Controls and Stability Approval L-1M AIR 3
Analysis
IC4-7* |Coupled Dynamic Loads Analysis — |Approval Receipt of Approved| Later of L-15M; 3
P/L Model + 3M L-26W
or
Receipt of
Approved P/L
Data + 3M
IC4-8* {Integrated Thermal Analysis Approval Later of AIR 3
L-9M
or
Approved PGAA +
2M
IC4-9* — |RF Link Analysis Approval Later of AIR 3
L-12M
or
Approved PGAA +
2M
C410" |Payload/Launch Vehicle EMC, RF, |Approval (B,C,D) L-12M (B.C,D) L-3M 3
and EED Compatibility Analysis (A&E) A/RinCDRL} (A&E) A/Rin
CDRL
IC4-11* |Mission Unique Software Approval Preliminary = L-20W Final = L-3W 3
IC4-12* |Quick Look Flight Report Review L+5 Working Days N/A 3
IC4-13* |Final Flight Report Review L+60 Days AIR 3

* Required per mission

TABLE D2-A: CDRL INDEX (Cont.)

D2-5



Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C1-4
MANIFEST POLICY

DESCRIPTION/PURPOSE:

The contractor shall provide at a minimum: the definition of standard setback guidelines
(including setback guidelines against other product lines that are offered to other non-NASA
customers), manifest separation ground rules, priorities, and assumptions, or equivalent.

DATA REQUIREMENTS:

Documentation shall be delivered in a mutually acceptable format.

02-11


Section D NASA Launch Services II (NLS I!)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

The Contractor shall be responsible for coordinating and ensuring all tracking and data
recovery support meets mission requirements (CDRL C2-3)

The Contractor shall arrange for the shipping of the recorded telemetry media(s) from
the downrange assets to the NASA designated NASA LSP Data Center no later than
five (5) calendar days following launch

2.4.1.3. Launch Dress Rehearsal

The Contractor shall conduct a minimum of one Dress Rehearsal prior to launch. The
rehearsal shall exercise the launch countdown procedure, and will have the participation
of the NNC and launch vehicle Contractor launch teams. The rehearsal may use an
abbreviated countdown script with simulated payload/vehicle conditions, including
anomalies

2.4.2 Launch Site Payload Support
2.4.2.1 Payload Processing Facility

For launches conducted from CCAFS, VAFB, and WFF, NASA will provide the Payload
Processing Facility (PPF) unless processing services are purchased as a non-standard
service. In the event (1) the Contractor proposes and NASA approves an alternate
launch site, and (2) the alternate launch site is not a ferry site, the Contractor shall be
responsible for providing a PPF, subject to NASA approval, meeting the payload
requirements.

2.4.2.2 Launch Site Payload Integration Support

The Contractor shall provide all services, equipment, and support required for the
integration and launch of each payload. Services shall include, as a minimum, the
following:

(A) Mating the payload with the launch vehicle, installing the payload fairing, and
performance of integrated checkout activities.

(B) Verification of the end-to-end functionality of the umbilical lines provided for payload
use

(C) Support for the installation and checkout of the payload GSE (provided by the
payload customer) in the Orbital Carrier Aircraft (OCA) as defined in the Mission
ICD.

(D) Provision of the mountings for, and the installation of, the payload GSE (provided
by the payload customer) in the OCA.

(E) Provisions for access to the payload for contingency off-loading of payload
propellants in accordance with the appropriate Range Safety requirements and
appropriate payload procedures.

D1A-23


Section D

Exhibit 2B: Taurus Standard Services

NASA Launch Services I! (NLS II)

Contract NNK10LB01B

sow
Para.

Standard Service

E28-7

Description



Section D

NASA Launch Services II (NLS I!)

Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.2.1.2. Design Reviews — Mission Specific

The Contractor shall conduct and chair/co-chair design reviews, as described below,
that apply to the system, subsystem, component, and software level for all mission
specific items. Where there is not a direct match between a SOW specified mission
specific design review(s) and the Contractor's standard review(s), the Contractor's
review process will be acceptable provided it addresses equivalent content. All derived
requirements from all system requirements must be identified and addressed in each of
these reviews. NASA will approve the Mission Unique items in these reviews.

(A) Mission Specific Requirements Review (MSRR)

The Contractor shall conduct an MSRR prior to the Mission Specific Preliminary
Design Review (MSPDR) with NNC to review the mission specific design
requirements for the following items:

(i)

(ii
(iii)

(iv)

(v)
(vi)

System requirements’ identification and definition to a level adequate to verify
launch vehicle performance capabilities

Design restrictions, limitations, and known violations.

Physical and mechanical interfaces (e.g., payload to launch vehicle, payload
envelope, and access provisions)

Electrical interfaces (e.g., launch vehicle to payload, payload to umbilical,
interfaces with electrical ground support equipment, pad electrical systems,
ground batteries, telemetry, grounding, and power).

Functional interfaces (e.g., structures, structural loads, and vibration).
Avionics systems and interfaces (e.g., payload avionics interfaces with launch

vehicle, separation systems, telemetry interfaces, payload command and
telemetry, and RF).

(vii) Mass properties.

(viii) Environmental requirements (e.g., thermal, contamination, vibration, pressure,

(ix)

(x)

Electromagnetic Compatibility (EMC), shock, launch complex RF, and
lightning).

Orbital requirements, launch vehicle performance, launch window injection
accuracy, and deployment attitudes and rates.

Payload/Launch Vehicle separation requirements (e.g., separation conditions,
launch vehicle post-separation maneuver requirements, and telemetry).

D1B-11


Section D NASA Launch Services II (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: S6-1
TELEMETRY TEST DATA

DESCRIPTION/PURPOSE:

To provide raw telemetry signals, on electronic medium, that are representative of the launch
vehicle and GSE telemetry allowing NASA to process, display and verify launch vehicle and
GSE telemetry prior to launch vehicle testing.

DATA REQUIREMENTS:

Provide as a minimum:

(A) An electronic copy representative of the telemetry signals of the launch
vehicle and GSE.

(B) Data on the electronic copy shall be time correlated in a manner that

enables time synchronization of all telemetry data and must conform to
IRIG Standard 106-07.

D3-12


Section C NASA Launch Services II (NLS Il)
Contract Terms and Conditions Contract NNK10LB01B

20.0

PLACE OF PERFORMANCE

The place of performance and launch site will be identified in each launch service or task
order. The delivery schedule and/or period of performance of this contract are based upon the
launch dates specified in the schedule or each individual task order.

21.0

22.0

23.0

23.1

23.2

23.3

24.0

24.1

RESERVED

Table C-7: Reserved
RESERVED
USE OF GOVERNMENT PROPERTY, FACILITIES, AND ASSETS
The Contractor shall obtain and maintain any necessary agreements between the
Contractor and any Government Agency authorizing the use of Government property,
facilities, assets or services required in performance of this contract
The Government makes no warranty whatsoever as to the suitability for use of
Government property, facilities and other assets made available under the terms and
conditions of any Government use agreements or contracts. Any costs necessary to
maintain, restore, refurbish, and/or replace any assets, for use under this contract, shall
result in no increase in the price of this contract.
The Contractor is responsible for determining the suitability for use of all materials,
property, and facilities acquired or made available to the Contractor by the Government
under any contract agreement. Any use of Government-Furnished Property (GFP),
materials, or facilities and services shall not relieve the Contractor of full launch service
performance responsibility.

MISSION SUCCESS DETERMINATION, INVESTIGATION, AND CORRECTIVE
ACTIONS

Mission Success Criteria
(A) Amission will be determined a Mission Success, if.
(i) The payload is placed into the required orbit by the launch vehicle, and

(ii) Received telemetry data shows the Interface Control! Document (ICD)
environments and parameters were not exceeded, and

(iii) The launch vehicle causes no damage to the payload during deployment or
thereafter from collision or contamination products, or

C-36


Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

Provide risk mitigation while utilizing commercial practices

Provide flexible manifesting policy that recognizes the national priorities of NASA
missions.

Provide a capability to optimize cost, schedule, and performance to satisfy mission
objectives.

Provide for clear Government visibility into program schedule, technical
performance, and risk

Foster competition and create opportunities for new, emerging launch service
providers.

Promote partnering among customers, launch service providers, and the LSP to
maximize flexibility and responsiveness to customers’ needs

1.3. Compliance Documents
The Contractor shall comply with the requirements contained in the following
documents.
Document No. Revision Document Title
Applicable Range Safety (e.g., EWR-127-1, AFSPCMAN 91-710, RSM-2002)
Requirements
ISO 9001/2000" 2000 International Organization of Standardization
AS9100 2009 Aerospace Quality Management System
KNPR 8715.3? KSC Safety Practices Procedural Requirements
LSP-PD-120.05 BASIC Launch Telemetry Requirements
NPR 8715.6" A NASA Procedural Requirements for Limiting Orbital
Debris
NASA-STD-8719.97 NASA Safety Standard for Lifting Devices and Equipment
*  1SO 9001/2008 is required after November 2010
2 The Contractor shall comply with the latest revisions of these documents. These documents apply to
NASA property, personnel, software, and processes performed in NASA-owned facilities.
3 NASA has the obligation to comply with this policy. The Contractor shall support NASA's compliance with
this document.
1.4 Reserved

D1A-6


Section B NASA Launch Services II (NLS II)
SF 1449 Continuation Contract NNK10LB01B

2.0 TOTAL AWARD AMOUNT

The guaranteed minimum value of this contract is $20,000. The maximum potential value of
contract number NNK10LB01B is $15,000,000,000. The total maximum potential value of all
NLS contracts combined is $15,000,000,000.

3.0 RESERVED
3.1 Reserved
3.2, Reserved

Table B-11: Reserved
3.3. Reserved

Table B-12: Reserved
4.0 MOST FAVORED CUSTOMER

The Contractor hereby certifies the CLIN prices for standard launch services (including
standard mission integration) under this contract are no higher than the lowest price charged to
any other commercial or U.S. Government customer for an equivalent launch service during
the twelve (12) months both preceding and following contract award, or placement of a launch
service task order. The Government shall be entitled to a one-time reduction in contract price
for each standard launch service failing to meet this certification. The price credit will be equal
to the difference between the standard launch service price under this contract and the lower
price awarded for an equivalent launch service.

5.0 IDIQLAUNCH SERVICE AND PRICE UPDATES

Successful Offerors who receive NLS IDIQ contract awards may propose additional IDIQ NTE
launch services and prices via the On-Ramp and Technology Insertion clause, Section C,
Clause 2.0. IDIQ contract holders will not be entitled to unilaterally adjust NTE prices or delete
launch services already in the contract. Contractor initiated changes to the launch vehicle
configuration, vendor, or design shall be subject to the launch vehicle certification
requirements of Section C, Clause 3.0. Contractor initiated changes to the launch vehicle
configuration, vendor, or design, after mission ATP, shall be at no increase to the contract
price and subject to the written approval of the Contracting Officer. New launch vehicle
certification plans and revisions to existing certification plans may be proposed for inclusion
into the contract when submitting Launch Service proposals pursuant to Section C, Clause
14.0, and shall be subject to the written approval of the Contracting Officer.

B-19


Section B NASA Launch Services II (NLS II)
SF 1449 Continuation Contract NNK10L801B

This page left intentionally blank.


Section D NASA Launch Services II (NLS II)
Attachment D4: SB and SDB Subcontracting Plan Contract NNK10LB01B

The following efforts will be taken to ensure that SBs, VOSBs, SDVOSBs, HUBZone SBs,
SDBs, WOSBs, including HBCU's and M's, have an equitable opportunity to compete for
subcontracts:

(a) Outreach efforts will be made as follows:

¢ Contacts with Dynamic Small Business Search through the CCR and
SUB-Net, the U.S. Small Business Administration Subcontracting Network

¢ Contacts with central Contractor Registration (CCR)

e Contacts with minority and small business trade association

e Contacts with business development organizations

e Attendance at small and minority business procurement conferences and
trade fairs .

(b) Source lists, guides and other data identifying SB, VOSBs, SDVOSB, HUBZone
SB, SDB and WOSB suppliers will be maintained and utilized by buyers soliciting
subcontracts

(c) Internal efforts to guide and encourage buyers will include workshops, seminars
and training programs and monitoring of activities to evaluate compliance with
this subcontracting plan.

LSG shall insert FAR clause 52.219-8, “Utilization of Small Business Concerns” in all
subcontracts that offer further subcontracting opportunities, are expected to exceed $550,000,
and are required to include this clause. All subcontractors, except small business concerns,
are required to adopt and comply with a subcontracting plan in accordance with FAR clause
52.219-9, “Small Business Subcontracting Plan”. Such will be reviewed assuring that all
minimum requirements of an acceptable subcontracting plan have been satisfied. The
acceptability of percentage goals shall be determined on a case-by-case basis depending on
the supplies/services involved, the availability of potential SB, VOSB, SDVOSB, HUBZone SB,
SDB, and WOSB subcontractors, and prior experience. Once approved and implemented,
plans will be monitored through the submission of periodic reports, and/or as time and
availability of funds permit, periodic visits to subcontractor's facilities to review applicable
records and subcontracting program progress.

LSG shall cooperate in any studies or surveys, submit periodic reports as may be required by
the contracting agency or the SBA, and will submit Individual Subcontracting Plans (ISRs-
formally SF 294s) and Summary Subcontract Report (SSRs- formally SF 295s) into the
Electronic Subcontracting Reporting System (eSRS) in accordance with FAC 2005-0025,
dated April 22, 2008, in accordance with FAR 19.704(10)(iii). LSG will require its
subcontractors to do the same

04-9


Section D NASA Launch Services II (NLS II)
Exhibit 1A: Pegasus Capabilities, Specifications and Environments Contract NNK10LB01B

EXHIBIT 1A

PEGASUS CAPABILITIES, SPECIFICATIONS AND ENVIRONMENTS

E1A-1


Section D
Attachment 010: Acronyms and Abbreviations

NASA Launch Services II (NLS II)
Contract NNK10LB01B

TM Technical Manual

TM Telemetry

TML Total Mass Loss

TO Take Off

TPA Test Payload Adapter

TPAF Test Payload Attach Fitting

TX Transmit

UDS Universal Documentation System
UPN Unique Project Number

USAF United States Air Force

US. United States

U.S.C. United States Code

VAB Vehicle Assembly Building
VAFB Vandenberg Air Force Base
VC-HS Visibly Clean - Highly Sensitive
VDC Voltage Direct Current

VETS Veterans

Vert Vertical

VOC Volatile Organic Compounds
VOSB Veteran-Owned Small Business
Ww Week

WFF Wallops Flight Facility

WOB Woman-Owned Business

WR Western Range

WTO World Trade Organization

x Number reference, such as CLIN
“x” Unknown L-period typically in months
YY Year

D10-7


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

19.3

19.4

19.5

lf the Contractor requests a postponement of the launch date and NASA agrees to the
postponement, the Parties agree that, in lieu of Termination for Cause and in place of
actual damages, and as fixed, agreed, and liquidated damages, the price of each
applicable launch service shall be reduced, dependent upon when receipt of the
Notification is received, for each calendar day of delay in excess of the grace period by
the amount as shown in Table C-5. In this event, NASA shall have the right of approval
of the revised launch date prior to its implementation. NASA shall also have the right of
approval of the reallocation of launch vehicles if milestone payments have already been
made towards a designated launch vehicle. Finally, NASA shall have the right of
approval prior to any revision in its position (i.e., the order in the Contractor's launch
manifest queue sequence, if it results in the postponement of the NASA launch date).

If the Contractor fails to request a postponement and the major program milestone
event designated as the launch is delayed (i.e., the launch service is not completed by
the contractual launch date), for reasons other than those excusable delays described
in paragraph 19.9, then the Contractor shall pay NASA for each day of delay in
accordance with Table C-5. Alternatively, if delivery or performance is so delayed by
the Contractor, NASA may terminate this contract in whole or in part under contract
Section C, Clause 1.0(m), Termination for Cause, of this contract and in that event, the
Contractor shall be liable for fixed, agreed, and liquidated damages accruing until the
time NASA may reasonably obtain delivery or performance of similar supplies or
services, up to the maximum specified in Clause 19.7. The liquidated damages shall be
in addition to any other costs under contract Section C, Clause 1.0(m), Termination for
Cause.

Each postponement request by the Contractor that is not the result of paragraph 19.9
herein is subject to the liquidated damages shown in Table C-5. The delay damages
are calculated on a per mission basis.

Contractor Liquidated Damages and Grace Periods

During Months Prior to Launch a . Grace
. Liquidated Damages Paid to NASA for .
Date - First Day to Last Day Period
(Months) Each Day of Launch Delay (Days)
(8)

Table C-5: Contractor Liquidated Damages and Grace Periods

C-33


Section D NASA Launch Services II (NLS II)
Exhibit 2B: Taurus Standard Services Contract NNK10LB01B

EXHIBIT 2B

TAURUS STANDARD SERVICES

E2B-1


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

and the terms of insurance policies, contracts, or other proof of financial
protection.

Notification and litigation of claims. The contractor shall give immediate written
notice to DOE of any known action or claim filed or made against the contractor
or other person indemnified for public liability as defined in paragraph (d)(2).
Except as otherwise directed by DOE, the contractor shall furnish promptly to
DOE, copies of all pertinent papers received by the contractor or filed with
respect to such actions or claims. DOE shall have the right to, and may
collaborate with, the contractor and any other person indemnified in the
settlement or defense of any action or claim and shall have the right to (1) require
the prior approval of DOE for the payment of any claim that DOE may be
required to indemnify hereunder; and (2) appear through the Attorney General on
behalf of the contractor or other person indemnified in any action brought upon
any claim that DOE may be required to indemnify hereunder, take charge of such
action, and settle or defend any such action. If the settlement or defense of any
such action or claim is undertaken by DOE, the contractor or other person
indemnified shall furnish all reasonable assistance in effecting a settlement or
asserting a defense.

Continuity of DOE obligations. The obligations of DOE under this clause shall not
be affected by any failure on the part of the contractor to fulfill its obligation under
this contract and shall be unaffected by the death, disability, or termination of
existence of the contractor, or by the completion, termination or expiration of this
contract

Effect of other clauses. The provisions of this clause shall not be limited in any
way by, and shall be interpreted without reference to, any other clause of this
contract, including the clause entitled Contract Disputes, provided, however, that
this clause shall be subject to the clauses entitled Covenant Against Contingent
Fees, and Accounts, records, and inspection, and any provisions that are later
added to this contract as required by applicable Federal law, including statutes,
executive orders and regulations, to be included in Nuclear Hazards Indemnity
Agreements.

Civil penalties. The contractor and its subcontractors and suppliers who are
indemnified under the provisions of this clause are subject to civil penalties,
pursuant to 234A of the Act, for violations of applicable DOE nuclear-safety
related rules, regulations, or orders.

C-64


Section D NASA Launch Services II (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

ATTACHMENT D1A

PEGASUS STATEMENT OF WORK

D1A-1


SOLICITATION/CONTRACTI/ORDER FOR COMMERCIAL ITEMS
OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24 & 30

1 REQUISITION NOMBER pace TOF 1

Attn: Steven B. Peterson, Room 3144C

Kennedy Space Center, Florida 32899

7 CEN HAGE NG 3 AWARDIFFFEGTIVE @ ORDER NUMER ¥ 20uK 1OR RAP “VE SODMITATION SSF
DATE CATE
NNK10LB01B __| RFP 10-99-0021 Rev D | October 18,1999
7 FOR SGLCITATION AME TOCPNGHiE tl aAF Na coat cal) [A OFT POLE oATEILOCAL (Mr
MEFCIRRATION CALL: Steven B. Peterson 321-867-5632 10/19/2009
a ISSULDEY OP LS SQUIE TIONS: TT ORTWERY GR FOR FES TINA LON
2MLESS
NASA John F. Kennedy Space Center Jit SVC TED stock istarkeo [_} see
SCHEDULE _
Procurement Office, Mail Code: OP-LS ST ASIDE a FGM 12 OFFER ACCFPTANGE Pi. RIOD)

180 Days from Date in Block 8

SMALL BUGLE SS.

SMALL DASADVANIAGLD.
Sus.

Ed)ian ris CONTRACT IS A RATED

ONDER
PUR} UNDER OPAS (15 CFF /00)
Ta, METHOD OF SOLICITATION sic: 3761 Pian nara :
Caro Cire SIZE STANDAHD 1000 DO-c9
DELIVER TO. [_OP-LS 16 ADMINIS IEAED DY
Same as Block 9. Same as Block 9.
17s CONTRACTOR? PPCISTATE 27555 | 1s PAYMENT WILL BE MADE BY al
OFFEROR Cove

Orbital Sciences Corporation

21839 Atlantic Boulevard (Bldg 1)

Attn: Jeffrey D. Campbell

Dulles, Virginia 20166

TELEPHONE NO. 703-406-5290 DUNS 80-320:9782

NASA Shared Services Center (NSSC)

Financial Manayemont Division (FMD) - Accounts Payable
Bidg 1111, C. Road

Stennis Space Center, MS 39529

Emait: NSSC-AccountsPaynble @nasa yov

Fax: 866-209-5415

17, CHECK IF REMITTANCE IS DIFFERENT AND PUT SUCH
ADDRESS IN OFFER.

15b SUBMIT INVGICES TO ADDRESS SIIOWN IN BLOCK 18a, UNLESS
BLOCK BELOW IS CHFCKED SEE ADDENDUM

I

20,

SCHEDULE OF SUPPLIES/SEAVICES

7a,
HEM NO.

21 ?
QUANSITY UNIT

Pa

23
UNIT PRICE AMOUNT

NASA LAUNCH SERVICES IN ACCORDANCE
WITH SECTION B, C AND D.

(Attach Additional Sheets as Necessary)

5, ACCOUNTING AND APPROPRIATION DATA

FB TOTAL AWARD AMOUNT (Fur Gov! (se

Wy)

Xe 7a. SOLICITATION INCORPOSATES IN FULL IUXT TAB 52.212-1, 52.2124, FAN 52 719-9 8 82 21)

SANE ATTACHED acorn Lane LJABE. NOT ATIACHED

27. CONTRACT/PUNCHASE ORDEN INCOMMONA ITS IN FULL TEX” FAR 52 210-4 FAN 92 2

bests artacheo —_apvenoa Y/Jan | Jane nor artacnno.

j28 CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN 3.COPIES [0

HSSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND DFLIVER ALL ITEMS SET FORTH.
DA OTHERWISE IDENTIFIED ABOVE AND ON ANY ADDITIONAL SHEETS SUBJECT TO THE
IFERIZS AND CONDITIONS SPECIFIED HEREIN.

[Jz AWARD OF ONINAC!: REFINENCE OFFER DAM D.

Tit GFF LR ON SULIC TATION (BLOCK 47 INCLUDING ARY ALIITIGNES Gti
HANGLS WHICH ANIL SEE FORT INEREIN, IS ACCEPTED AS TO ITT MS:

ORICONTAA lata uNttet SQ) AMLAICA (Samanure Gt Gon
f na YNHTEU ALL HICA (SSartane Gt Contracting Utter)
; \u ) ‘
0b, AMT AMO TITLE OF SIGNER (Type orpnnl) ‘30c DATE SIGNED [31b. NAME ORCONTAAGTING OF FICER (Tye ur print) [aie DATE
Camille T Cisek 9-17-2010 Michael S. McCart S.GNEO.
Vice President , Business Operations ° y D3; fa)
32a, GUANTITY IN GOLUPAN 71 TTAS BEEN [a SFP NUMAEA "34. VOUCHER 35 AMOUN
OB tectwveo  Ginsetcrip ( ACcLPTLD. AND CONFORMS 10 THE QGpaatial LJ Fivar NUMBER VEHILO
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ie DATE RFC D hd OF CONTAINEAS
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a
Provceted


Section D NASA Launch Services II (NLS I!)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

25

2.5.1

Launch vehicles provided under this contract shall include all hardware, software,
analysis and support necessary to meet the applicable Range Safety Requirements
(e.g., EWR-127-1, AFSPCMAN 91-710, or RSM-2002).

As part of the launch service, the Contractor shall make all launch Range support
arrangements for: scheduling Range for launch and integrated testing, Range Safety
functions, communications and timing, metric C-band beacon (radar) coverage,
telemetry coverage, camera coverage of launch, and tracking and telemetry station
acquisition predictions. If required, NASA will provide down range telemetry aircraft,
Tracking and Data Relay Satellite System (TDRSS) and/or NASA owned ground station
support for tracking and data recovery. The Contractor shall be responsible for
coordinating and ensuring all tracking and data recovery support meets mission
requirements (CDRL C2-3).

The Contractor shall make arrangements for Range provided services necessary to
support the launch service. As a minimum, the following services are to be provided:
fluids, gases, propellants, ordnance storage, facility usage, equipment support, shop
and laboratory services, meteorology, base security, fire protection and environmental
health. Payload-unique Range services will be provided as a mission-unique service.

The mission specific Program Requirements Document/Operational Requirements
(PRD/OR)(CDRL C2-2), or equivalent mission specific Range support documentation,
shall be submitted to obtain Range support. The Contractor, with support from NASA,
shall complete all forms pertinent to the mission and submit them to the appropriate
Range for formal acceptance

Safety, Reliability, and Quality Assurance

During the period of performance the Contractor shall establish, implement, and
maintain comprehensive safety and health, reliability and quality assurance programs
covering program management, mission integration management, and the design,
development, production, test, integration and launch of the LVS.

Safety and Health Program

The Contractor shall provide a Safety and Health Plan that will implement safety and
health requirements consistent with federal, state, and local government regulations and
applicable launch processing site Safety and Health requirements. This Plan shall
describe the Safety organization including structure of management interfaces and also
system safety methods employed to ensure compliance with applicable launch
processing site safety requirements.

The Contractor shall implement a system safety program to identify hazards of
systems/subsystems and impose applicable design requirements and management
controls to prevent mishaps. The Contractor shall develop system safety
documentation, plans, procedures, technical analyses, etc., IAW safety requirements of

D1A-27


Section D NASA Launch Services II (NLS II)
Exhibit 8: Mission Interface Control Documents (ICD) Contract NNK10LB01B

EXHIBIT 8
MISSION INTERFACE CONTROL DOCUMENTS (ICD)
Thirty (30) days prior to launch, the approved ICD shail be incorporated into the contract via

contract modification as Exhibit 8 to Attachment D1. Any approved changes after its inclusion
into the contract will be incorporated prior to mission success determination.

E8-1


Section D NASA Launch Services II (NLS I!)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.2.2

2.2.3

2.2.4

2.2.5

(iii) Open corrective actions/problems reports
(iv) Mission Unique and First flight items
(E) Launch Readiness Review (LRR)

NASA will conduct/chair, and the Contractor shall participate in an LRR one day
prior to launch to verify all actions from the FRR are complete and final processing
has been successfully completed. NASA will appoint the chairperson for this
review. At the conclusion of this review, an “approval to proceed with launch
countdown’ is given. Representatives from the Contractor, Range, and NNC
agencies sign the Certificate of Flight Readiness. The Contractor shall prepare the
Certificate of Flight Readiness. A sample Certificate of Flight Readiness is provided
in Exhibit 4.

Risk Management

The Contractor shall implement risk management techniques that address the
identification, analysis, mitigation, and tracking of potential impacts to mission success
The Contractor shall develop the criteria, methods, and procedures used for identifying
critical items in the Risk Management Plan (CDRL C3-6).

Configuration Management

The Contractor shall perform configuration management of the launch vehicle design
and production for all launch vehicle components/subsystems, hardware, and software

Manifest Policy

The Contractor shall develop and provide a Manifest Policy as described in CDRL C1-4
that addresses the Contractor's overall approach to ensuring timely launch of payloads.
The Contractor shall provide a Program Master Schedule and Launch Vehicle Planning
Manifest (SDRL S1-3) to support Government mission scheduling.

New Launch Vehicle Orientation

The Contractor shall conduct an orientation briefing at KSC. This briefing shall
introduce Contractor personnel and establish project interfaces with NASA personnel
and describe the Contractor's organization and infrastructure. The briefing shall contain
information summarizing the design, performance, fabrication, integration, testing,
qualification and operational features of the launch vehicle systems and supporting
facilities required to provide the launch service in the form of diagrams, schematics,
pictures, drawings, videos, etc.

D1B-16


Section D NASA Launch Services II (NLS II)
Exhibit 3A:_ Pegasus Non-Standard Services List Contract NNK10LB01B

This page left intentionally blank.

E3A-2


Section B NASA Launch Services II (NLS II)
SF 1449 Continuation Contract NNK10LB01B

Sree ae eso
ANOOKRWN=

2.0

Table B-1:_ Reserved..
Table B-2: Reserved..
Table B-3: Reserved..
Table B-4: _Reserved..
Table B-5: Special Task Assignments (Studies and Analyses) .
Table B-6: Hourly Labor Rate - FFP List.....
Table B-7: Reserved..
Table B-8: IDIQ Launch Service Task Order . a
Table B-9: NTE Price List - Standard Launch Services for IDIQ Missions

. Reserved ....
. Reserved ow...

TABLE OF CONTENTS

SCHEDULE OF SUPPLIES AND/OR SERVICES TO BE PROVIDED.............
Reserved .......
Reserved
Reserved ..
Reserved
Special Task Assignments (Studies ‘and Analyses) .
IDIQ Launch Service Task Order (LSTO) cieeteeeesseseaees
NTE Prices - Standard Launch Services for IDIQ Missions ..................

NTE Prices — Non-Standard Services for IDIQ Missions ..........

DODD DDOD
DANDAAAaAAA

TOTAL AWARD AMOUNT o.oo cece eee cette teeters creenteettreeittrtetteeteeeeeeers BETQ

RESERVED.
Reserved ..

MOST FAVORED CUSTOMER ......0..cccccccicc tenet reeset tte etter BAAD

IDIQ LAUNCH SERVICE AND PRICE UPDATES ..........scccecccecececeteteeteecteeceenes B-19

LIST OF TABLES

Table B-9A: Quantity Discount Schedule o.oo... cece cece eee eetsesereseeeseeeessienereee

Table B-10: Pegasus NTE Price List - Non-Standard Services for IDIQ Missions...
Table B-10: Taurus NTE Price List - Non-Standard Services for IDIQ Missions
Table B-11: Reserved..
Table B-12: Reserved..

B-3


Section D NASA Launch Services II (NLS II)

Attachment D2: Contract Data Requirements List Contract NNK10LB01B
Item Document Approval/ Initial Submittal Subsequent No. of
Review Date Submittal Date | Copies

C5: Engineering

IC5-1* |Vehicle Data Package Review NLT L-9M (if As Changed 4
Required)
|C5-2* —_|Mission Unique Hardware Test Plan |Approval MSCDR As Changed 4
IC5-3* —_|Mission Unique Hardware Test Review Test Completion + As Changed 4
Report 2M
IC5-4* {Mission Unique Drawings Review As Generated per As Changed 4

design review
criteria, but no later
than 30D prior to

fabrication,
installation,
assembly
IC5-5* —_|Integrated Procedures Approval Review and AIR 5
comment, 45D Prior
to Use;
Approval, 1W Prior
to Use
* Required per mission
Item Document Approval/ tnitial Submittal Subsequent No. of
Review Date Submittal Date | Copies
C6: Telemetry and
[Communications
IC6-1*  |Vehicle and GSE Telemetry Formats |Review L-3M As Changed with 2
Configuration
IC6-2* _|Vehicle and GSE Telemetry (Test, |Review Test + 1D; NIA 1
Pre-Launch, and Launch) Pre-Launch + 1D;
Launch + 1W

* Required per mission
TABLE D2-A: CDRL INDEX (Cont.)

D2-6


Section D

NASA Launch Services II (NLS I)

Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C3-2 (cont)

4.2 Mishap Investigation and Corrective Action for Mishaps on Contractor Property, Third
Party Property, or Other Non-NASA Government Property.

a)

b)

An initial investigation by the Contractor is required for all mishaps which have been
teported to NASA. NASA reserves discretionary authority to investigate mishaps
which involve NASA personnel or resources regardless of location. The Contractor
has the discretion to perform any collateral investigations. However, investigations
implemented by NASA will take priority with regard to access to evidence, data, and
witnesses. The proceedings of NASA investigations will remain confidential. The
Contractor will have an opportunity to comment on the investigation report in
accordance with NASA protocols.

Contractor Final Report. After the Contractor completes its investigation of the
mishap and, when appropriate, has developed a plan of corrective action, the
Contractor shall deliver this completed report to NASA within fifteen (15) days of
completion. This plan will include any verification activities identified by the
Contractor to ensure that corrective actions have been implemented or, if applicable,
accomplished.

D2-26


Section D NASA Launch Services |! (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

2.5.2

2.5.3

the applicable launch processing site. For launches at the Eastern Range or Western
Range, any previously approved agreements between the contractor and the Range for
a tailored EWR 127-1 are acceptable to NASA. Likewise, any previous Range Safety
Agreements between the Contractor and WFF or RTS are acceptable to NASA. In
accordance with Section C, Clause 25.0 of the contract, the Contractor shall provide
NASA with insight and approval into future tailoring of Range Safety Requirements for
launch vehicle systems and operations. Launch processing site safety required
documentation shall be made available to NASA (SDRL S3-4) upon request. The
Contractor shall participate in all safety working groups (i.e. payload safety working
group (PSWG), etc.) as the launch vehicle safety representative for each NASA mission
under this contract.

When the contractor is performing work in any NASA owned facility (e.g., buildings 836
and SLC-2W at VAFB and PHSF at KSC), all NASA requirements and safety
documentation as contained in the SOW, paragraph 1.3, Compliance Documents, shall
be adhered to. The Contractor shall submit system safety documentation (baseline and
any changes) to NASA for review/approval IAW CDRL C3-7 for processing at all NASA
provided facilities. NASA will review the safety documentation to ensure designs,
processing and operations do not pose an unacceptable safety risk to NASA
personnel/contractors, resources or risk to Mission Success.

The Contractor shall report Close Calls/Mishaps to NASA IAW CDRL C3-2. The
Contractor shall make provisions for NASA safety representative insight into integrated
Payload/launch vehicle processing.

Reliability Program

The Contractor shall implement and maintain a Reliability Program with an overall
vehicle design reliability of no less than 95% at an 80% confidence factor. The
Contractor's program shall facilitate evaluation of the Contractor and subcontractor's
programs to determine if the product meets the overall design reliability requirements.
Overall vehicle reliability predictions shall be incrementally revised to reflect design
modifications.

Quality Assurance Program

The Contractor shall maintain a quality management system that is ISO 9001/2000 third
party certified (ISO 9001/2008 third party certification is required after November 2010).
The Registrar shall be accredited by either the International Registrar of Certified
Auditors (IRCA) or the Registrar Accreditation Board (RAB). In the event the Contractor
certification is revoked, NASA shall be notified within five (5) business days (CDRL
C3-3).

The Contractor shall maintain a Software Assurance Program using ISO 90003 as a
guideline.

D1A-28


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

(d)

funds required to continue performance to the date specified in paragraph
(c)(1) of this clause, or an agreed date substituted for it.

(ii) The Contractor shall, sixty (60) days in advance of the date specified in
paragraph (c)(1) of this clause, or an agreed date substituted for it, advise
the Contracting Officer in writing as to the estimated amount of additional
funds required for the timely performance of the contract for a further
period as may be specified in the contract or otherwise agreed to by the
parties.

(4) If, after the notification referred to in paragraph (c)(3)(ii) of this clause,
additional funds are not allotted by the date specified in paragraph (c)(1) of this
clause, or an agreed date substituted for it, the Contracting Officer shall, upon
the Contractor's written request, terminate this contract on that date or on the
date set forth in the request, whichever is later, pursuant to contract Section C,
Clause 1.0(I) “Termination for the Government's convenience’.

When additional funds are allotted from time to time for continued performance of
the work under this contract, the parties shall agree on the applicable period of
contract performance to be covered by these funds. The provisions of paragraphs
(b) and (c) of this clause shall apply to these additional allotted funds and the
substituted date pertaining to them, and the contract shall be modified accordingly.

If, solely by reason of the Government's failure to allot additional funds in amounts
sufficient for the timely performance of this contract, the Contractor incurs additional
costs or is delayed in the performance of the work under this contract, and if
additional funds are allotted, an equitable adjustment shall be made in the price(s)
(including appropriate target, billing, and ceiling prices where applicable) of the
items to be delivered, or in the time of delivery, or both.

The Government may at any time before termination, and, with the consent of the
Contractor, after notice of termination, allot additional funds for this contract.

The provisions of this clause with respect to termination shall in no way be deemed
to limit the rights of the Government under the Termination for Cause clause of this
contract. The provisions of this Limitation of Funds clause are limited to the work on
and allotment of funds for the items set forth in paragraph (a) of this clause. This
clause shall become inoperative upon the allotment of funds for the total price of
said work except for rights and obligations then existing under this clause.

Nothing in this clause shall affect the right of the Government to terminate this

contract pursuant to contract Section C, Clause 1.0(I) “Termination for the
Government's convenience” of this contract.

C-21


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C3-4

QUALITY MANAGEMENT SYSTEM (QMS) AND SUPPLIER/VENDOR
AUDIT/ASSESSMENT SCHEDULES

DESCRIPTION/PURPOSE:

A QMS and Supplier/Vendor schedule that lists all planned audits/assessments and visits to
subcontractors, suppliers, vendors, and internal sites.

DATA REQUIREMENTS:

The list shall include the subject of the audit/assessment, a tracking number or identifier,
assigned assessor, and a schedule by month indicating the planned event

D2-28


Section D
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

NASA Launch Services II (NLS II)

21

All Contract Data Requirements List (CDRL) and Supplemental Data Requirements List
(SDRL) items, identified in Attachment D2 and D3 respectively, shall be included in the
standard launch service

Launch Vehicle

The standard launch service shall include, as a minimum, the following:

(A) Launch timing capabilities with

(i)
(ii)

(iii

Reserved

Multiple approximately twenty-four (24) hour re-launch attempts in the event of
a launch scrub (with exception of abort inside 45 seconds)

Launch window as short as 5 minutes

(B) A launch vehicle and Payload Adapter (PA) with appropriate electrical and
mechanical interfaces (as described in Exhibit 1) required for payload integration
and testing.

(C) A payload separation system with the following characteristics:

(i)

(ii)

(iii)

The payload shall be protected from debris generated by the separation
system

The separation system shall function in a manner that prevents any re-contact
with the payload, including Contractor-provided attach hardware on the
payload, by the upper stage or any element of the separation system once
separation has been initiated.

Redundant payload separation indications.

(D) A Payload Fairing (PLF) with the following items, as a minimum

(i)

Two payload access doors of size 33 cm x 21.6 cm (13 in x 8.5 in) whose
locations shall be mission unique within the stated structural limitations of the
fairing (defined in Exhibit 1). Additional or different size doors shall be provided
as a non-standard service. The Contractor shall provide payload personnel
access through all standard and non-standard access doors from fairing mate
through final vehicle closeout.

D1A-8


Section D NASA Launch Services II (NLS I!)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

3.1.1. Structural interfaces
3.1.1.1 Static Payload Envelope
3.1.1.2 PLF Clearance Requirements
3.1.1.3 SC Clearance Requirements
3.1.1.4 Separation Clearance Requirements
3.1.1.5 SC Access Requirements
3.1.2 Structural Loads
3.1.2.1 SC Stiffness
3.1.2.2 SC Interface Loads
3.1.2.3. Strength
3.1.2.4 SC Load Factors
3.1.3 Mass Properties
3.1.3.1 SC Mass Properties
3.1.3.2 SC Propellant Data
3.2 Electrical Interfaces
3.2.1 Airborne Interfaces
3.2.1.1 Standard Electrical Interfaces
3.2.1.2 Separation Indication
3.2.1.3. Interface Electrical Constraints
3.2.1.4 SC Separation System Electrical Interface
3.2.1.5 SC to LV Interleaved Telemetry
3.2.2 SC Umbilical Interface
3.2.2.1 T-0 Umbilical Interface
3.2.2.2 EGSE Interface Electrical Constraints
3.2.3 EGSE Telemetry/Command/Data Link
3.2.3.1. EGSE Hardline Links
3.2.3.2 SC Interleaved Data
3.2.4 Electrical Grounding
3.2.4.1 Spacecraft Grounding
3.2.4.2 Support Equipment Grounding
3.2.4.3. Personnel Grounding
3.2.4.4 Ground Continuity
3.3. Environmental Interfaces
3.3.1. Thermal

02-14


Section D
Attachment D1A: Pegasus Statement of Work (SOW)

NASA Launch Services II (NLS II)
Contract NNK10LB01B

TABLE OF CONTENTS

1.0 INTRODUCTION

1.1 Scope...

1.2 Objectives... .

1.3 compliance D Documents

1.4 Reserved ..

2.0 STANDARD LAUNCH SERVICE..
2.1 Launch Vehicle .

2.2 Program Management bee eee eens
2.2.1 Formal Reviews.....

2.2.1.1 Program Reviews... .

2.2.1.2 Design Reviews - Mission Specific ........
2.2.1.3 Readiness Reviews....

2.2.2 Risk Management
2.2.3 Configuration Management
2.2.4 Manifest Policy...

2.2.5 New Launch Vehicle Orientation...
2.3 Mission Integration Services....

2.3.1 Mission Integration Management...

2.3.2 Mission Analyses

2.3.3 Mission Success Determination.

2.4 Launch Site Support Le cece
2.4.1 Pre-Launch Checkout and Launch Support...
2.4.1.1 Launch Vehicle Preparation and Launch........

2.4.1.2 Telemetry Data and Launch Countdown Support........

2.4.1.2.1 Vehicle Telemetry
2.4.1.2.2 Baseline and Integrated Support.
2.4.1.2.3. Launch Countdown and Flight Support
2.4.1.3 Launch Dress Rehearsal

2.4.2 Launch Site Payload Suppo
2.4.2.1 Payload Processing Facility... bee
2.4.2.2 Launch Site Payload Integration ‘Support
2.4.2.3 Contamination and Environmental Control
2.4.2.4 Operational Support Services..

2.4.3 Range Support and Services... beceeees
2.5 Safety, Reliability, and Quality Assurance........
2.5.1 Safety and Health Program.. a

2.5.2 Reliability Program...

2.5.3 Quality Assurance Program...
26 NASA Insight and Approval...

D1A-3



Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B8

1.0

2.0
3.0
40
5.0

6.0

7.0
8.0

9.0

10.0
11.0

12.0

13.0

14.0

15.0

16.0

17.0
18.0
19.0
20.0
21.0

SECTION C
CONTRACT TERMS AND CONDITIONS
TABLE OF CONTENTS

FAR 52.212-4 CONTRACT TERMS AND CONDITIONS--COMMERCIAL ITEMS

(MAR 2009) (TAILORED) o......cccccssscccssssssssssesssevessesessvsssssvvesenssssessesnsivisestesssseveveseee 6
ON-RAMP AND TECHNOLOGY INSERTION co estttttetttttteeeee 13
LAUNCH VEHICLE CERTIFICATION . 15
OFF-RAMP CLAUSE... 16

LAUNCH SERVICE PAYMENTS, MILESTONE EVENTS AND COMPLETION
CRITERIA ooo cee cece eee ceeiececenece census tenserersesinssisitisssieiessisiessseisesiserseseeererersees 17

NFS 1852.232-77 LIMITATION OF FUNDS (FIXED-PRICE conrracn
(MAR 1989) .. wens

SECURITY FOR LAUNCH SERVICE PAYMENT FINANCING

SCOPE OF WORK - SPECIAL TASK ASSIGNMENTS (STUDIES AND
ANALYSES) (CLIN 10) .....cccccceceeeeeeee

ORDERING PROCEDURE AND PAYMENT FOR SPECIAL TASK ASSIGNMENTS
(STUDIES AND ANALYSES) (CLIN 10)...

RESERVED
FAR 52.216-18 ORDERING (OCT 1995) [Note: Applicable to IDIQ

23

contract portion OMly)............. cece cece cece reeseseereseeeseneeeteeenenees sectereereetenene 20
FAR 52.216-19 ORDER LIMITATIONS (OCT 1995) [Note: Aplabe to

IDIQ contract portion OMly] 2... cece ee eceeeseerscretseseeereeesicsersasseveieeeerseseeereeneeee 25
52.216-22 INDEFINITE QUANTITY (OCT 1995) [Note: Applicable to

IDIQ contract portion OMY] oo... ccc cece ee eeee ese cee settee tecesstsstecessesetsstsseseeeseateneeseeseees 26

LAUNCH SERVICE TASK ORDERING PROCEDURES > Note: Applicable to
IDIQ contract portion only]...

PRESERVATION, PACKING, PACKAGING, AND MARKING FOR
DOCUMENTATION ..

FAR 52.246-11 HIGHER LEVEL CONTRACT QUALITY
REQUIREMENT (FEB 1999)

INSPECTION SYSTEM RECORDS . .
REQUIRED TIME OF DELIVERY FOR LAUNCH SERVICES . 0.00.0... ccc 31

ADJUSTMENTS TO LAUNCH SCHEDULE 000.0... ccc ccc eeeete erste teeseeeeeseeeeeeeee 32
PLACE OF PERFORMANCE ...00.......cccccccccccceccsccesscecteeeecseseeeeeseeeseseesseseseieseeteesescnesnts 36
RESERVED o.oo. bo ceeeeceeeceseeseseeeeecansesseessseatseseeesstcasieerentiateeenes 36

C-3


Section D NASA Launch Services II (NLS I!)

Attachment D2: Contract Data Requirements List Contract NNK10LB01B
CDRL DESCRIPTION Number: C2-4
RESERVED

02-20


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

the primary payload customer prior to manifesting. If the secondary payload is not
ready to support scheduled launch day, the secondary payload will be
demanifested and replaced with a mass simulator.

29.2 NASA Secondary Payload with NASA Primary Payload

(A) Procedures

(B)

NASA may request to manifest a NASA secondary payload on a NASA primary
mission. The preferred method of ordering this secondary payload service will be
via non-standard service task order. If the non-standard service is not provided in
the catalog for the particular launch service, the Government will submit a task
order requesting a proposal for a non-standard service to accommodate a
secondary payload. The Contracting Officer will provide a description of the
proposed secondary payload including, as a minimum: volume, mass, attachment
requirements, and data requested by the Contractor. The task order will identify
any additional non-standard services or mission unique requirements.

Upon receipt of the task order, the Contractor shall develop a proposal to
accommodate the secondary payload or provide a response that the Contractor
cannot accommodate the secondary payload on any existing planned missions.
The Contractor's proposal shall include a firm fixed-price for the secondary payload
(if not ordered under a non-standard service), any additional non-standard services
required, any mission unique services, and a proposed payment schedule with
accomplishment criteria.

If the Government is unable to provide the secondary payload for launch vehicle
integration or there is insufficient time to complete a new mission analysis before
the launch date, the Government will bear the cost and the Contractor shall be
responsible for designing, fabricating, and installing a secondary payload mass
simulator.

In the event of termination for convenience of the NASA secondary payload
services, all costs associated with terminating such service shall be determined in
accordance with contract Section C, Clause 1.0(I), “Termination for the
Government's convenience.”

Delays

Any delays shall be subject to contract Section C, Clause 19.0, Adjustments to
Launch Schedule

Mission Success

Mission success determination for the NASA primary and secondary payload shall

be made in accordance with contract Section C, Clause 24.0, Mission Success
Determination, Investigation, and Corrective Actions with the following exception:

C-45



Section D

NASA Launch Services II (NLS I!)

Exhibit 2B: Taurus Standard Services Contract NNK10LB01B
sow Standard Service Description

RT

NIT

nT

E2B-7



Section D NASA Launch Services II (NLS tI)
Attachment D11: Definitions Contract NNK10LB01B

First Flight Item: A first flight item is the planned use of a component for which NASA will be
one of the first three flights or uses, and/or which affects qualification margins or subsystem
performance and interfaces. The term “flight” is used generically to include all airborne
systems and ground systems used to meet payload requirements and ground systems with
direct interfaces to the vehicle. Additionally, any change of component vendor or
manufacturing site relocation will be considered a first flight item if a NASA LSP-managed
mission is planned to be one of the first three uses of the new component.

Integrated Procedures: Launch vehicle procedures used for various operations that involve
the payload and/or the Launch Vehicle/payload interfaces.

Launch: The intentional ignition of the first-stage motor(s) of the launch vehicle that has been
integrated with the payload.

Limited Launch Period: Daily launch opportunities constrained by blackout periods associated
with scientific requirements (e.g., planetary, lunar, seasonal, and/or lunar exclusions)

Mission Specific: All standard, non-standard, mission unique and first flight services provided
to meet the requirements of the payload and mission.

Mission Integration Start: L-30M plus or minus 3M signifies the starting point of Mission
Integration Start. All integration work prior to or greater than L-30M plus or minus 3M is
considered Early/Extended Integration

Mission Unique: Services provided that are newly performed or developed specifically to meet
the requirements of the payload and mission. Mission unique items are considered first flight
items

NASA LSP Data Center: NASA's voice, video, communication and data facility located at
either CCAFS or VAFB.

NASA Provided Facility: Includes NASA owned facilities as well as NASA procured
commercially available facilities for payload processing

Party or Parties: The Contractor or NASA, or both

Payload or Spacecraft: All NASA or NASA-sponsored equipment that has been or will be
integrated with the launch vehicle for transportation into earth orbit or escape trajectories.
Payload and spacecraft are used synonymously throughout the document.

Payload Program Level Requirements: The basis for mission assessments conducted by
NASA Headquarters during the development period and provides the baseline for the
determination of the science mission success during the operational phase of the payload.

011-2


Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

develop and present a decision matrix for its launch team which defines who has
authority to issue a GO, NO GO, and HOLD during launch countdown. The
Contractor shall describe its launch day management activities, identify key team
members, and define responsibilities and communications between the launch
vehicle, NASA, and payload teams

Flight Readiness Review (FRR)

NASA will conduct/chair, and the Contractor shall participate in an FRR for each
mission to ensure the specific launch vehicle is acceptable for flight and all Range
and other mission requirements have been met, or will be satisfied prior to launch.
The FRR is held approximately three (3) days before launch. As a minimum, the
Contractor shall provide verification that:

(i) All critical items required to proceed into final launch countdown are ready

(ii) Vehicle configuration is defined and all vehicle systems have been verified
IAW launch site test plans

(iii) All previously recorded action items have been closed or are reflected on the
schedule

(iv) All previously held Contractor's readiness review actions have been closed or
resolved

(v) Launch site/Range support organizations have committed to launch
(vi) Tracking and data support resources are committed to launch

(vii) Any open work is identified and closeout plans and schedules are in place and
supportable

(viii) Any constraints to launch are identified and resolution plans developed
(ix) Mission risks are known and documented

(x) Launch commit criteria for payload and launch vehicle is approved and
released

The Contractor shall also discuss:
(i) Anomalies from previous missions, including non-NASA missions

(ii) _Hardware/software failures in the field either on the NASA assigned launch
vehicle or in the fleet

D1A-15


Section D NASA Launch Services II (NLS II)
Exhibit 9: LSTO Mission Solutions Contract NNK10LB01B

This page left intentionally blank.

E9-2


Section D NASA Launch Services II (NLS I!)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

This page left intentionally blank

D3-16


Section D NASA Launch Services II (NLS II)
Attachment D4: SB and SDB Subcontracting Plan Contract NNK10LB01B

Table || attached to the Master Plan shows examples of principal types of supplies and
services to be subcontracted to Small Business, Veteran-Owned Small Business, HUBZone
Small Business, Small Disadvantaged Business and Women Owned Small Business

The figures contained in Table | and Table I! are based on past history and/or actual
quotations obtained in support of an individual proposal

LSG continues to develop sources and locate additional companies to support government
contracts consistent with our guidelines of maintaining a fair market price and high quality
products and services. In this proposal, Orbital’s small business goals were established
based on its source lists, contacts with Procurement Marketing and Access Network (PRO-
Net) and use of SUB-Nef, the U.S. Small Business Administration Subcontracting Network.

Additional market research, including internet searches, utilizing the Small Business
Administration search tools and publicizing Orbital’s needs for small business subcontractors
has resulted in an awareness of more potential small businesses to contract with. However,
even after completion of market research Orbital still finds that SDBs, including ANCs and
Indian Tribes, HUBZone, WOSBs and SDVOSBs are still under represented in performing
work related to highly technical and proprietary specialization of Orbital Sciences Corporation,
Launch Systems Group (LSG). LSG has found itself limited in some areas where it can
contract with Small Businesses due to our quality requirements and our qualification process.
The nature of the technical and specialized business we support and the high standard which
Orbital LSG holds it Suppliers left us with little to no support from certain groups such as
SDVOSBs, WOSBs, and SDBs. Other than fulfilling basic product and material needs, it is
difficult to find experienced qualified small businesses to provide specialized items and perform
services relative to our core competency because of the proprietary nature of our designs,
drawings and processes. As Orbital grows, it continues to look for qualified small businesses
and institutions which can support our capabilities while also meeting the proper safety and
quality standards required in the rocket industry.

The name of an individual employed by LSG who administers the subcontracting program, and
a description of the duties of the individual;

Name: Taragh Mulvihill
Address: Orbital Sciences Corporation
Launch Systems Group
3380 South Price Road
Chandler, AZ 85248
Telephone: (480) 722-3933
Title: Sr. Manager of Procurement Compliance

D4-7


Section D

Exhibit 2B: Taurus Standard Services

NASA Launch Services II (NLS II)

Contract NNK10LB01B

SOW
Para.

Standard Service

Description

E2B-10



Section D NASA Launch Services II (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: S1-1
LAUNCH SERVICE USER’S GUIDE AND FACILITY INFORMATION
DESCRIPTION/PURPOSE:

The Launch Service User's Guide and facility information to provide customers with information
and capabilities regarding launch services and facilities.

DATA REQUIREMENTS:

Provide the commercially available Launch Service User's Guide and information on the LSC
provided facilities, including

(A) | Payload GSE Space and Capabilities

(B) | Crane Size and Hook Height

(C) — Electrical Service

(D) Environment, i.e., cleanliness level, relative humidity
(E) Environment Monitoring Equipment

(F) | Temperature

(G) Hazardous Capability

(H) Power

(I) Processing Space Floor Capability

(J) Processing Space Size

K) | Support Space

L) Grounding Provisions

M) Communications Capabilities

N) Security Systems
O)

(
(
(
(
( Mechanical Support Equipment (Lifts, etc)

03-2


Section C NASA Launch Services II (NLS I!)
Contract Terms and Conditions Contract NNK10LB01B

(3) “Launch Vehicle” means an object, or any part thereof, intended for launch,
launched from Earth, or returning to Earth which carries Payloads or persons, or
both.

(4) "Party" means a party to a NASA Space Act agreement for Science or Space
Exploration activities, unrelated to the ISS, but which involve a launch and a party
that is neither the prime contractor under this contract nor a subcontractor at any tier
hereto.

(5) "Payload" means all property to be flown or used on or in a Launch Vehicle

(6) “Protected Space Operations" means all Launch or Transfer Vehicle activities
and Payload activities on Earth, in outer space, or in transit between Earth and outer
space in implementation of an Agreement for Science or Space Exploration
activities, unrelated to the ISS, but which involve a launch. Protected Space
Operations begins at the signature of the Agreement and ends when all activities
done in implementation of the agreement are completed. It includes, but is not
limited to:

(i) Research, design, development, test, manufacture, assembly, integration,
operation, or use of Launch or Transfer Vehicles, Payloads, or instruments, as
well as related support equipment and facilities and services; and

(ii) All activities related to ground support, test, training, simulation, or guidance
and control equipment, and related facilities or services. Protected Space
Operations excludes activities on Earth which are conducted on return from
space to develop further a Payload’s product or process other than for the
activities within the scope of an Agreement.

(7) "Related entity" means:
(i) A contractor or subcontractor of a Party at any tier;
(ii) A user or customer of a party at any tier; or

(iii) A contractor or subcontractor of a user or customer of a Party at any tier. The
terms “contractors” and “subcontractors” include suppliers of any kind.

(c) Cross-waiver of liability:

(1) The contractor agrees to a waiver of liability pursuant to which it waives all claims
against any of the entities or persons listed in paragraphs (c)(1)(i) through (c)(1)(iv)
of this clause based on Damage arising out of Protected Space Operations. This
cross-waiver shall apply only if the person, entity, or property causing the Damage is
involved in Protected Space Operations and the person, entity, or property damaged
is damaged by virtue of its involvement in Protected Space Operations. The waiver

C-66


Section D

NASA Launch Services II (NLS II)

Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C6-1 (cont)

(D)

(E)

(F)

(G)

(viii) Initial minor frame number where measurement is found
(ix) | Frame step rate of measurement if found in more than 1 minor frame

(x) Special conversion algorithm from raw to engineering units if not standard
polynomial

(xi) Calibration coefficients for conversion from raw to engineering units

(xii) Bit number in word if measurement is a discrete

(xiit) List of guidance modes that measurement is valid

(xiv) Method of determining guidance modes

(xv) Measurement mask if required

Description of rules used to format measurement description file including:

(i) Description of each field in file

(ii) Description of all codes or abbreviations

(iii) | Method of determining revision level or revision date

Non-PCM Data Stream Description: This file will describe the format of the data
stream location and description of all measurements, and the calibration data
required to convert from raw to engineering units.

A list of flight events which will occur for each mission and the nominal time for
event occurrence. If event can occur at variable times, this must include a
description for determining event time during flight. This list must be delivered for
every mission.

A list of predicted position and velocity state vectors for significant events during
flight. This list must include, at a minimum, the end of all powered flight phases
and payload separation. A description of the coordinate system used to provide
the state vectors must also be included. This list must be delivered for every

mission.

A list of vehicle attitude measurements and description of format used.

All files must be delivered using an electronic medium.

D2-52


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-2
FINAL MISSION ANALYSIS (FMA)
DESCRIPTION/PURPOSE:
This analysis is prepared based on payload requirements resulting from NASA review of the
PGAA and contains information similar to that in the PGAA. This analysis supports pre-flight
verification of compliance with mission requirements
DATA REQUIREMENTS:
The FMA shall include, as a minimum

(A) The nominal 5 or 6 Degree of Freedom (DOF) trajectory simulation for each

targeted insertion condition utilizing actual weights and propulsion models

(electronic format is preferred)

(B) All Data Requirements identified in PGAA Data Requirement Description

D2-33


Section C NASA Launch Services I! (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

14.0

14.1

14.2

14.3

the order. The contract shall govern the Contractor's and Government's rights and
obligations with respect to that order to the same extent as if the order were
completed during the contract's effective period; provided, the Contractor shall not
be required to make any deliveries under this contract after December 31, 2022

LAUNCH SERVICE TASK ORDERING PROCEDURES [Note: Applicable to IDIQ
contract portion only]

Requirements for Competition. The intent of IDIQ is to support missions in addition to
the awarded missions. The Government will provide all multiple award Contractors a
fair opportunity to be considered for task orders issued under this contract based upon
the specific task order requirements, unless the Contracting Officer determines that one
of the following apply:

(A) The Agency need is of such urgency that competing the requirements among
Contractors would result in unacceptable delays

(B) Only one Contractor is capable of providing the service requested at the level of
quality required because the service ordered is unique or highly specialized

(C) The order should be issued on a sole-source basis in the interest of economy and
efficiency as a logical follow-on to an order issued under the contract, provided that
all Contractors were given a fair opportunity to be considered for the original order;
or

(D) It is necessary to place an order to satisfy the minimum guarantee.
Types of Task Orders

There are two types of task orders that may be issued under this contract. The first type
is an LSTO. Any required services related to a specific launch service will be included
in the LSTO. All items other than launch services and items not related to a specific
launch service will be obtained by task orders referred to herein as Special Task
Assignments (Studies and Analyses).

Launch Service Task Orders

(A) Requests for Launch Service Proposals (RLSPs). Prior to the issuance of an
RLSP, exchanges and fact-finding may take place with multiple award Contractors.
The RLSP will include specific information unique to the mission such as Mission
Success risk posture (Section C, Clause 24.4, Table C-8); payload mass and
volume; orbital requirements (such as altitude and/or inclination); target launch date
and science window, if appropriate; and any unique payload design considerations.

The RLSP will provide any special instructions regarding the level of detail required
in the proposal. The RLSP will include a date and time for submission of the

C-27


Section D NASA Launch Services tI (NLS II)
Exhibit 7; Launch Vehicle Certification Data Contract NNK10LB01B

This page left intentionally blank.

E7-2


Section D NASA Launch Services I! (NLS I!)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-4
PAYLOAD FAIRING VENTING ANALYSIS
DESCRIPTION/PURPOSE:

This analysis shall evaluate and verify that the payload depressurization rate requirements are
satisfied.

DATA REQUIREMENTS:

The Payload Fairing Venting Analysis shall be based on the mission trajectory and payload
geometry and volume.

D2-35


Section C

NASA Launch Services I! (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

24.5 Investigation and Corrective Action

(A)

(D)

In the event of an anomaly or failed mission, a NASA review board(s) will
determine the cause of anomaly or failure, if activated. The review board(s) will
evaluate all available data from the launch vehicle, payload, Range, and other
sources in order to determine if the mission failure was attributable to the launch
vehicle or conditions for which the Contractor would normally be expected to
control or avoid. Based on all available pertinent data, including the findings and
recommendations of the review board(s) the Contracting Officer shall make the
final determination as to partial mission success or failed mission. If the Contractor
disagrees with the determination, the decision shall be subject to the Disputes
clause of this contract.

lf one or more of the environmental requirements are exceeded or orbit
requirements are not achieved, as documented in CDRL C2-5 and reported in
CDRL C4-13 on a particular mission, the Contractor shall investigate the anomaly
or failure at its own expense. The Contractor shall determine the scope of the
investigation and shall conduct and control the investigation. The Government may
designate representatives to observe and participate in the Contractor's failure
investigation board. If the Contractor changes the launch vehicle design, the
Contractor shall provide NASA insight into the change. The Government may
establish an independent assessment team to assess the Contractor's
investigative and corrective actions.

The Contractor shall present to the Government its findings resulting from the
investigation and the proposed corrective actions (return to flight activities), if any.
The Contractor shall be responsible for proving the corrective action is sufficient to
return to flight. The Contracting Officer may either accept or reject any finding, root
cause, or corrective action. If the Contracting Officer accepts a finding and the
telated corrective action, the Contractor shall be responsible for the cost of the
corrective action including Contractor's cost for re-acceptance for NASA missions.

The Government may, at its option and its expense, conduct its own investigation
of the anomaly or failure. The Contractor shall cooperate with and fully support the
Government investigation, at the Contractor's expense. In the event the
Government requires additional analyses or tests beyond those planned by the
Contractor, the Contractor shall implement the Contracting Officer’s written
direction to perform the additional tests or analyses. The costs of implementing
these additional tests or analyses may be the basis for an adjustment to this
contract.

The Contractor shall report to NASA any flight anomalies from non-NASA
missions. For non-NASA missions, the requirements of paragraphs 24.5(B) and
(C) apply to these anomalies as the Contracting Officer finds them to be related to
NASA missions. Rights under the Default clause and the right to require corrective
action before return to flight shall also apply.

C-39


Section D NASA Launch Services I! (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

This page left intentionally blank.

D1B-2


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

are included in the standard launch service price. Approvals required by the payload are the
responsibility of NASA

28.0

28.1

28.2

28.3

28.4

29.0

29.1

ADVANCE UNDERSTANDING REGARDING TERMINATION SETTLEMENT UNDER
FAR 52.212-4(I)

In the event the Government decides to exercise its right to terminate all or part of this
contract under Section C, Clause 1.0(I), Termination for the Government's convenience,
it is agreed in advance that the Contractor, after receipt of a written notice of
termination, will have satisfied all obligations and discharged all duties required by
Section C, Clause 1.0(I), Termination for the Government's convenience, when the
Contractor has refunded that portion of the milestone-based payment(s) for each launch
service affected by the termination, in accordance with Table C-1

The parties agree that by virtue of the refund specified in Table C-1, any and all claims
for equitable adjustment as a result of the termination are fully satisfied and discharged.
The parties agree that this settlement represents fair compensation for Contractor effort
accomplished for the terminated portions of the contract and that the terms as stated
herein represent full and final settlement between the parties. The parties agree that
the Contractor shall retain title to all hardware associated with the terminated launch
service. The parties agree that the above settlement shall represent the total amount to
be paid to the Contractor without agreeing on or segregating the particular elements of
costs or profits comprising this amount

The refund amount shall be payable in full no later than thirty (30) days after receipt of
the written notice of termination. Delinquent payment(s) shall be subject to interest at
the applicable rate as determined by the Secretary of the Treasury.

Table C-9: Reserved

The provisions of this Contract clause shall only apply from Award until the point of
intentional ignition of the launch vehicle. The provision of this Contract clause shall in
no way be deemed to limit the rights of the Government under Section C, Clause
1.0(m), Termination for Cause. In the event the Government exercises its rights under
Section C, Clause 1.0(m), Termination for Cause, the provisions of this contract clause
will not apply

CO-MANIFESTED PAYLOADS
Definitions

(A) Primary Payload: the payload which serves to determine the launch day and time,
and without which the vehicle would not launch.

(B) Secondary Payload: Any payload carried by the launch vehicle in space not
required by the primary payload. The secondary payload requires the approval of

c-44



Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C2-3
LAUNCH VEHICLE DETAILED MISSION REQUIREMENTS (DMR)
DESCRIPTION/PURPOSE:

The Launch Vehicle DMR documents formal requests for tracking, communications, and data
system services that are either managed by or negotiated through the Exploration, Operations,
Communication and Navigation Systems Division (Code 450) at Goddard Space Flight Center
(GSFC).

DATA REQUIREMENTS:

The DMR, consisting of sets of Universal Documentation System (UDS) standard forms (with
associated instructions), shall be completed to obtain network support from NASA for the
baseline launch vehicle. The Contractor, with the support of NASA/KSC, completes all forms
appropriate to the vehicle and submits them to NASA/KSC for review and GSFC Code 450 for
formal acceptance. The DMR shall follow the format provided in the NASA/GSFC Instruction
Manual for the NASA DMR document.

D2-19


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

The Contractor shall be responsible for coordinating and ensuring all tracking and data
recovery support meets mission requirements (CDRL C2-3).

The Contractor shall arrange for the shipping of the recorded telemetry media(s) from
the downrange assets to the NASA designated NASA LSP Data Center no later than
five (5) calendar days following launch

2.4.1.3. Launch Dress Rehearsal

The Contractor shall conduct a minimum of one Dress Rehearsal prior to launch. The
rehearsal shall exercise the launch countdown procedure, and will have the participation
of the NNC and launch vehicle Contractor launch teams. The rehearsal may use an

\ abbreviated countdown script with simulated payload/vehicle conditions, including
anomalies.

2.4.2. Launch Site Payload Support
2.4.2.1 Payload Processing Facility

For launches conducted from CCAFS, VAFB, and WFF, NASA will provide the Payload
Processing Facility (PPF) unless processing services are purchased as a non-standard
service. In the event the Contractor proposes and NASA approves an alternate launch
site, the Contractor shall be responsible for providing a PPF, subject to NASA approval,
meeting the payload requirements.

Taurus’ encapsulation processing activities require facility physical characteristics and
capabilities typical for most payload processing facilities. These features include items
such as: certified grounding system, work lighting levels, telephone and communication
services, Suitability for hazardous operations, etc. Some of the more critical items
required specifically for Taurus launch vehicle processing include:

e Facility Door Opening Size: 14 ft wide x 30 ft tall (minimum)
e Crane Requirements: airlock/cleanroom — hook height of 35 ft minimum; 5000 Ib
working load; micro control preferred
e Power: 480V/3ph/60Hz, 4 wire; and 120V/1ph/60Hz
e Flight hardware floor space:
o Fairing Half (2 each): 22 ft x 10 ft (Airlock only)
o Fairing Half (2 each): 12 ft x 8 ft
o Payload Cone: 6 ft x 6 ft
o Separation System: 5 ftx5 ft

It is common for all facility requirements to be captured in NASA’s LSSP documentation

D1B-23


Section C NASA Launch Services {I (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

24.6

24.7

Finality of Contracting Officer's Determination

(A) Each of the Contracting Officer's Determinations, under paragraph 24.2, are subject
to FAR 52.233-1, Disputes

(B) Reserved

(C) In the event the Contractor appeals the Contracting Officer's determination under
the Disputes clause in accordance with FAR subpart 33.2 and submits a claim
under the Contract Disputes Act, the parties hereby agree the burden of proof shall
rest on the Contractor to prove the failure was not due to the LV. The Contractor
assumes the responsibility for providing confirming data. The Government will be
responsible for providing proof of payload degradation or reduction in operational
capacity or longevity

Acceptance

Final acceptance of the launch service will be accomplished following the Contracting Officer's
mission success determination

25.0

25.1

25.2

25.3

GOVERNMENT INSIGHT AND APPROVAL

The Contractor shall provide NASA an adequate level of insight into and/or approval of
certain Contractor tasks and milestones in order to ensure all reasonable steps have
been taken that result in the highest probability of mission success. This includes
insight into any corporation, corporate divisions, subsidiaries, joint ventures, partner(s),
and/or any other business entity actually performing launch vehicle manufacturing,
management, payload/launch vehicle integration, testing and launch. This also includes
insight into certain major sub-contractor tasks and milestones (i.e, those sub-
contractors that perform major portions of manufacturing or integration of the launch
vehicle system).

The Government's monitoring of launch services provided by the private sector has two
elements: approval and insight. Government approval is defined as providing authority
to proceed and/or formal acceptance of requirements, plans, tests, or success criteria in
specified areas. Where Government approval is required, the Contractor shall submit
the necessary documentation to the Contracting Officer and copies to the Contracting
Officer's Technical Representative (COTR).

Government insight is defined as gaining an understanding necessary to knowledgeably
concur/non-concur with the Contractor's actions through interaction, watchful
observation, documentation review, meeting attendance, reviews, tests and compliance
evaluations. Where Government insight is required, the Contractor shall notify the
Contracting Officer, the Government Resident Office or the appropriate Government

c-40


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C3-6

RISK MANAGEMENT PLAN

DESCRIPTION/PURPOSE:

In accordance with NPD 8610.23A, the contractor shall submit a Contractor's Risk
Management Plan to be provided to the COTR for subsequent distribution.

DATA REQUIREMENTS:

A

This Risk Management Plan shall describe how the contractor proposes to manage and
accept risk throughout the program and on all activities required to perform this contract.
It shall describe how the contractor will identify, assess, and mitigate/control risks as an
integral part of the Contractor's management and decision process.

Information that illustrates the functional relationships and lines of communication,
including the involvement of subcontractors and major vendors.

Descriptions of the risk management function within the organization including the
process through which management decisions will be made. This will include a
description of interfaces with NASA organizations and the NASA decision process for
areas such as critical and catastrophic hazards, corrective actions, mishaps, anomaly
resolution, safety and technical variances/waivers/exceptions, cost, schedule and
mission success.

Description of the management controls that will be used to ensure compliance with the
risk mitigation process.

Risk reports shall be delivered quarterly (at a minimum) to the COTR. The reports shall
include all identified risks, their likelihood, consequence and status of all activities
associated with the mitigation, avoidance or acceptance of each risk. The report shall
indicate the relative prioritization of all risks.

Access to the contractor's risk database shall be provided to NASA personnel to be
identified by the COTR or Contracting Officer.

02-30


Section D

Attachment D2: Contract Data Requirements List

NASA Launch Services II (NLS II)
Contract NNK10LB01B,

CDRL DESCRIPTION

2. NASA MISHAPS:

Number: C3-2 (cont)

Classification
Level &
Investigation
Type

Property Damage

Injury

Type A Mishap

Total direct cost of mission failure and

property damage is $1,000,000 or more,
or

Crewed aircraft hull loss has occurred,
or

Occurrence of an unexpected aircraft

departure from controlled flight (except

high performance jet/test aircraft such as

F-15, F-16, F/A-18, T-38, OV-10, and T-

34, when engaged in flight test activities).

Occupational injury and/or illness that resulted
in:

A fatality,
or
A permanent total disability,
or
The hospitalization for inpatient care of 3 or
more people within 30 workdays of the mishap.

Type B Mishap

Total direct cost of mission failure and
property damage of at least $250,000 but
less than $1,000,000.

Occupational injury and/or illness has resulted
in permanent partial disability.

or
The hospitalization for inpatient care of 1-2
people within 30 workdays of the mishap.

Type C Mishap

Total direct cost of mission failure and
property damage of at least $25,000 but
less than $250,000

Nonfatal occupational injury or illness that
caused any workdays away from work,
restricted duty, or transfer to another job
beyond the workday or shift on which it
occurred.

Type D Mishap

Total direct cost of mission failure and
property damage of at least $1,000 but
less than $25,000.

Any nonfatal OSHA recordable occupational
injury and/or illness that does not meet the
definition of a Type C mishap.

Close Call

An event in which there is no
equipment/property damage or minor
equipment/property damage (less than
$1000), but which possesses a potential
to cause a mishap.

An event in which there is no injury or only
minor injury requiring first aid, but which
possesses a potential to cause a mishap.

3. ONSITE MISHAPS OCCURRING ON NASA PROPERTY:
Any unplanned occurrence, event, or anomaly involving NASA personnel, equipment, or
facilities that meet one of the mishap classifications as defined above shall follow the
Mishap and Close Call Reporting, Investigating, and Recordkeeping procedural

requirements as documented in NPR 8621.1.

For occurrences that meet one of the

mishap classifications as defined above and occurring on NASA KSC owned facilities,
launch sites or equipment, the Mishap and Close Call reporting, investigation and
recordkeeping procedural requirements as documented in KNPR 8715.3 shall be

followed.

D2-24


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C3-7
SAFETY DOCUMENTATON FOR PROCESSING IN NASA PROVIDED FACILITIES
DESCRIPTION/PURPOSE:

This item covers the submission of documentation to NASA when performing operations in a
NASA-provided facility in support of this contract. NASA will approve this documentation when
processing in NASA-owned facilities and NASA will review this documentation when
processing in NASA-procured facilities. This includes system safety documentation associated
with launch vehicle systems, flight hardware and any associated equipment and/or ground
support equipment.

DATA REQUIREMENTS:
Safety documentation related to processing in NASA-provided facilities:

* Safety Data Package (Missile System Prelaunch Safety Package - MSPSP)
o System Descriptions
Hazards Analyses/Hazard Reports
Single Failure Point (SFP) Analyses (where applicable)
Test Plans and Nondestructive Examination Plans
Material Compatibility
o Material Safety Data Sheets (MSDS’s)
* Tailored Range Safety Requirements
Any Waivers or Equivalent Level of Safety Requests
Mishap Preparedness and Contingency Plans
o Initial submittal date forty-five (45) days prior to shipment to the facility
« Radiation control and use authorization for all ionizing and non-ionizing (radio frequency
and high intensity light) sources
o Initial submittal date 4 months prior to use
e Hazardous launch vehicle standalone procedures
o Initial submittal date forty-five (45) days prior to use

oo0°0o

If the LV, hardware, equipment, and/or system is of a new design or is being
upgraded/modified, the Contractor shall provide draft and preliminary revision of the applicable
safety documentation. The applicable Safety Data Package, tailored Range Safety
requirements, and any waivers or Equivalent Level of Safety requests shall be delivered to
NASA thirty (30) days prior to each design review milestone (i.e. MSPDR, MSCDR). Final
revisions of safety documentation related to processing in NASA-owned facilities shall be
delivered to NASA for approval at least forty-five (45) calendar days prior to first use for
hazardous operations.

The Contractor shall update the safety data documentation and any technical analyses as
necessary to keep the data current and resubmit to NASA for review.

D2-31


Section C NASA Launch Services 11 (NLS II)
Contract Terms and Conditions Contract NNK 10LB01B

The estimated range and launch site direct costs currently included in the standard launch
services prices contained in Article B1.7 are as follows:

Order Year

PeaasusXL[ CYi0 | Cyii | cyiz | cyis [ Cyi4 | CYis [CY46-cy20
Order Year

TaurusXL_| CY10 | cY11 | CYi2 | CYi3 | cyYi4 | CyYi& | CYt6-cY20

C69


Section D NASA Launch Services II (NLS I!)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

2.0

STANDARD LAUNCH SERVICE

The Contractor shall perform all launch service tasks necessary to deliver payloads to
defined orbital parameters in compliance with mission requirements. The launch service
shall support missions to all orbital parameters, consistent with vehicle configuration
capabilities and launch Range restrictions. The Contractor shall provide launch
services, which are in compliance with all Range and responsible authority
requirements. The Contractor shall make all arrangements with the responsible
authorities for the required launch Range authorization and support for vehicle
processing; integrated payload/vehicle processing, launch; and launch site maintenance
and modifications. NASA reserves the right to approve the choice of launch site [e.g.
Cape Canaveral Air Force Station (CCAFS), Vandenberg Air Force Base (VAFB)}.

The Contractor shall furnish all services, maintain all equipment and infrastructure
including, but not limited to: program management, mission integration, launch site
support, ground and flight system safety, and performance assurance, necessary to
accomplish the safe and successful launch of payloads to the required orbit conditions
within required launch periods. The Contractor shall provide facilities and services at
Contractor facilities for NASA personnel performing insight and approval functions
during the performance of the contract. The Contractor shall provide access to launch
vehicle documentation in support of NASA insight and approval functions.

The Contractor shall provide all necessary services, test hardware and software, and
mission specific elements required to integrate the payload(s) to the launch vehicle
systems. The Contractor shall meet all launch service performance requirements
described in Exhibit 1, Capabilities, Specifications and Environments. All capabilities
and conditions stated in Exhibit 1 must be consistent and compatible with all other
capabilities and conditions stated in Exhibit 1 and in response to the requirements of the
SOW. Any exceptions to the stated capabilities or conditions must be specifically noted.

The Contractor shall coordinate with NASA Public Affairs Office all press releases
concerning launches under this contract. During vehicle build-up, payload integration,
and launch countdown, the Contractor shall allow NASA Public Affairs access to
facilities to photograph and videotape activities, including hazardous operations. The
Contractor shall assist NASA Public Affairs in developing the launch commentary for
NASA Television by furnishing launch countdown and operations background material
The Contractor may also be asked to provide information to support the development of
the press kit document and the NASA pre-launch and post-launch news conferences.
The Contractor shail coordinate with NASA Public Affairs Protocol and Guest Services a
minimum of sixty (60) days in advance of each launch to determine any special
requirements.

The Contractor shall provide standard launch services as delineated in Exhibit 2,
Standard Launch Services List which shall comply with the requirements of the SOW.
All hardware, software, analyses, and support required to provide each item listed in
Exhibit 2, shall be included in the standard launch service.

D1A-7


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

19.6

If NASA requests a postponement of the launch date, the Parties agree that, in place of
actual damages, and as fixed, agreed, and liquidated damages, the price of each
applicable launch service shall be increased, dependent upon when receipt of the
Notification by the Contracting Officer is received, for each calendar day of delay in
excess of the grace period by the amount as shown in Table C-6. Each postponement
request by NASA that is not the result of paragraph 19.9 is subject to the postponement
fees shown in Table C-6.

NASA Postponement Fees and Grace Periods

During Months Prior to Launch | Postponement Fees Paid to Contractor | Grace
Date - First Day to Last Day for Each Day of Launch Delay Period
(Months) ($)_ (Days)

19.7

19.8

Table C-6: NASA Postponement Fees and Grace Periods

The Liquidated Damages/Postponement Fees (Tables C-5 and C-6) cover all costs
related to the delay except vehicle de-stack/re-stack (de-mate/re-mate) costs,
necessary repeated performance of studies and analyses, and new scope. The party
causing the delay will be responsible for the aforementioned costs.

The maximum amount paid for delays (in excess of the grace period) by the
Contractor/NASA is and shall be the lesser amount of either 5% of the highest
priced launch vehicle configuration at year of contract award or a total of $9,400,000.
The maximum amount applies only to the Liquidated Damages/Postponement Fees
shown in Tables C-5 and C-6. Both parties are entitled to recover additional monies for
Equitable Adjustment as referenced in 19.2.

A grace period is defined as the number of days the Contractor/NASA may delay the
launch date, without incurring liquidated damages/postponement fees. The amount of
grace available for any period is the smaller of the number of days in the grace period
column in Table C-5 compared to the remaining available grace days from the previous
period.

For example, if 100 days are used during the period L-X through L-24, there would be
50 days available during the period L-24 through L-12. If no further days are used
through the period L-6 through L-3, there would be 30 days available during the period
L-3 through L-11 days; with 20 days having expired.

In the event that NASA/Contractor postpones the launch date, the payment schedule
shall be suspended for the length of the delay and then resumed with all remaining

C-34


Section D

NASA Launch Services II (NLS Il)

Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.2.1.3 Readiness Reviews

The Launch Vehicle Systems Readiness Review, Pre-Mate Readiness Review, Launch
Management Coordination Meeting (LMCM), Flight Readiness Review (FRR) and
Launch Readiness Review (LRR) described herein will be conducted for each NASA
mission

(A)

(C)

Launch Vehicle Systems Readiness Review

The Contractor shall conduct a Launch Vehicle Systems Readiness Review to
demonstrate that the launch site and launch vehicle are ready to proceed with
launch vehicle processing activities at the launch site. The Contractor shall present
as a minimum:

(i) Mission description including S/C and launch vehicle configuration; integration
status; summary of waivers; post launch data review of previous flights (NASA
and non-NASA); mission specific analyses results and status; vehicle hardware
assignments, assessments and status; and launch site status

(ii) A detailed schedule showing all activities (ground and flight) remaining to
achieve a successful, on-time launch

Pre-Mate Readiness Review

The Contractor shall conduct a Pre-Mate Readiness Review to demonstrate the
launch site and launch vehicle are ready for payload mechanical and electrical
integration. The Contractor shall conduct a launch vehicle/site walk-down
[reference SOW Section 2.4.1.1(D)] with NNC participation prior to or in conjunction
with the Pre-Mate Readiness Review. The Contractor shall present as a minimum

(i) Action item status, safety status, payload mating plan, closure plan, payload
integration/launch site documentation, interface verifications, checkout and
launch software status, nonconformance reports, launch site status, S/C
readiness, and review of flight profile.

(ii) A detailed schedule showing all activities remaining to achieve an on-time
launch.

Launch Management Coordination Meeting (LMCM)

The Contractor shall participate in an LMCM conducted by NASA before each
faunch dress rehearsal or launch. The LMCM is used to ensure the readiness of
the launch team to execute the procedures necessary to conduct the launch dress
rehearsal (reference SOW Section 2.4.1.3) or launch. At this meeting, participant
roles and responsibilities during countdown shall be identified. The Contractor shall
develop and present a decision matrix for its launch team which defines who has

D1B-14


Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

7.0 GUIDELINE DOCUMENTS

The following documents are to be used as guidelines to the extent specified in this SOW. Ifa
revision number or date is not specified, the latest revision of the documents shall be used as
guidelines to the extent specified in the SOW.

Document No Rev. Document Title

ISO 14644-1 Basic Clean rooms and associated controlled environments — Part 1:
classification of air cleanliness

ISO 14644-2 2000 Clean rooms and associated controlled environments — Part 2:
specifications for testing and monitoring to prove continued
compliance with ISO 14644-1-First Edition

IRIG-106-07 2007 Telemetry Standards

ISO 90003 2004 Software Engineering - Guidelines for the Application of ISO
9001:2000 to Computer Software

ISO 19011 2002 Guidelines for Quality And/Or Environmental Management

MIL-STD-1553' B
MIL-STD-1540 Borc

MIL-STD-176 A,
Notice 1

MIL-STD-1773 Notice 1

IEST-STD-CC1246 D

2002
MIL-PRF-27401 F

2008
ASTM E1216 2006
ASTM E1235 2008

NASA RP-1124 4
1997

NPR 2810.A 2006
NASA-STD-8729.1

NPD 8610.23

Systems Auditing
Digital Time Division Command/Response Multiplex Data Bus

Test Requirements for Launch, Upper-Stage, and Space
Vehicles

Weight and Balance Data Reporting Forms for Guided Missiles
and Space Launch Vehicles

Fiber Optics Mechanization of an Aircraft Internal Time Division
Command/Response Multiplex Data Bus

Product Cleanliness Levels and Contamination Control
Program

Propellant Pressurizing Agent, Nitrogen

Standard Practice for Sampling for Particulate Contamination
by Tapelift

Standard Test Method for Gravimetric Determination of
Nonvolatile Residue (NVR) in Environmentally Controlled Areas
for Spacecraft

Outgassing Data for Selecting Spacecraft Materials

Security of Information Technology

Planning, Developing and Managing an Effective Reliability and
Maintainability (R&M) Program

Launch Vehicle Technical Oversight Policy

D1A-32


Section D NASA Launch Services II (NLS II)
Attachment D6: Reliability Plan Contract NNK10LB01B

ATTACHMENT D6

RELIABILITY PLAN


Section D NASA Launch Services II (NLS II)

Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B
1.4 Reserved
2.0 STANDARD LAUNCH SERVICE

The Contractor shall perform all launch service tasks necessary to deliver payloads to
defined orbital parameters in compliance with mission requirements. The launch service
shall support missions to ail orbital parameters, consistent with vehicle configuration
capabilities and launch Range restrictions. The Contractor shall provide launch
services, which are in compliance with all Range and responsible authority
requirements. The Contractor shall make all arrangements with the responsible
authorities for the required launch Range authorization and support for vehicle
processing; integrated payload/vehicle processing, launch; and launch site maintenance
and modifications. NASA reserves the right to approve the choice of launch site [e.g.
Cape Canaveral Air Force Station (CCAFS), Vandenberg Air Force Base (VAFB)].

The Contractor shall furnish all services, maintain all equipment and infrastructure
including, but not limited to: program management, mission integration, launch site
support, ground and flight system safety, and performance assurance, necessary to
accomplish the safe and successful launch of payloads to the required orbit conditions
within required launch periods. The Contractor shall provide facilities and services at
Contractor facilities for NASA personnel performing insight and approval functions
during the performance of the contract. The Contractor shall provide access to launch
vehicle documentation in support of NASA insight and approval functions.

The Contractor shall provide all necessary services, test hardware and software, and
mission specific elements required to integrate the payload(s) to the launch vehicle
systems. The Contractor shall meet all launch service performance requirements
described in Exhibit 1, Capabilities, Specifications and Environments. All capabilities
and conditions stated in Exhibit 1 must be consistent and compatible with all other
capabilities and conditions stated in Exhibit 1 and.in response to the requirements of the
SOW. Any exceptions to the stated capabilities or conditions must be specifically noted.

The Contractor shall coordinate with NASA Public Affairs Office all press releases
concerning launches under this contract. During vehicle build-up, payload integration,
and launch countdown, the Contractor shall allow NASA Public Affairs access to
facilities to photograph and videotape activities, including hazardous operations. The
Contractor shall assist NASA Public Affairs in developing the launch commentary for
NASA Television by furnishing launch countdown and operations background material
The Contractor may also be asked to provide information to support the development of
the press kit document and the NASA pre-launch and post-launch news conferences.
The Contractor shall coordinate with NASA Public Affairs Protocol and Guest Services a
minimum of sixty (60) days in advance of each launch to determine any special
requirements.

The Contractor shall provide standard launch services as delineated in Exhibit 2,

D1B-7


Section D

NASA Launch Services II (NLS II)

Attachment D2: Contract Data Requirements List Contract NNK10LB01B
CDRL DESCRIPTION Number: C3-2 (cont)
4. MISHAPS OCCURRING ON CONTRACTOR PROPERTY, THIRD PARTY PROPERTY

4.1

OR OTHER NON-NASA GOVERNMENT PROPERTY:

Immediate Notification and Reporting of Mishaps Occurring on Contractor Property,
Third Party Property or Other Non-NASA Government Property

a.

b.

Cc.

Telephonic Report: The Contractor shall notify the NASA Launch Services Division
Safety Office within one hour of the occurrence of a Type A mishap, Type B mishap,
high-visibility mishap, or high-visibility close call that involves NASA personnel or
property while performing work in support of this SOW. For Type C or D Mishaps
and Close Calls involving NASA personnel or property, the contractor shall notify the
Launch Services Division Safety Office within four (4) hours of the occurrence

i. During this notification, the Contractor shall provide the following information: the
Facility name, location of incident, time of incident, number of fatalities (if known),
number of hospitalized employees (if known), type of injury (if Known), type of
damage (if known), contact person, contact person's phone number, and a brief
description of the mishap.

24-Hour Report: The Contractor shall provide an initial incident report to the Launch
Services Division Safety Office within twenty-four (24) hours of the incident for all
Mishaps, or Close Calls involving NASA personnel or property while performing work
in support of this SOW. The following information, as a minimum, shall be included:
author of report; author’s phone number and mail code; date report submitted; time
report submitted; incident date; incident time; incident general location; exact
location (if known); responsible organization; organization’s point of contact; point of
contact’s phone number and mail code; mission affected; program impact (if known);
number and type of injuries or fatalities (if known); type of damage to equipment,
flight hardware, flight software, or facilities; estimate of direct cost of damage; and a
brief description of the mishap or close call.

Notify OSHA: Within eight (8) hours of a work-related mishap involving death of a
Federal employee, or the hospitalization for inpatient care of three or more
employees (provided at least one is a Federal employee) the contractor shall notify
OSHA by calling the area office nearest the site of the mishap or OSHA's toll-free
number, 1.800.321.6742. OSHA notification is required for any fatality or three or
more hospitalizations that occur up to thirty (30) workdays after the respective
mishap. In notifying OSHA, the Contractor shall provide OSHA with the following
information: the establishment name, location of incident, time of incident, number of
fatalities (if known), number of hospitalized employees (if known), contact person,
contact person's phone number, and a brief description of the mishap.

02-25


Section D

NASA Launch Services I! (NLS II)

Attachment 01B: Taurus Statement of Work (SOW) Contract NNK10LB01B

(B) Mission Specific Preliminary Design Review (MSPDR)

The Contractor shall conduct a preliminary detailed design review prior to major
commitment to drawings and design. Mission unique trade studies shall be
completed prior to the MSPDR. The Contractor shall discuss analyses performed
and their results along with comparisons to any similar proven designs. The
Contractor shall evaluate the safety of the design and its ability to meet safety
requirements. The preliminary mission unique design shall be subject to NASA's
approval. NASA reserves the right to withhold approval until all action items have
been closed. As a minimum, the Contractor shall provide verification of the
following items at the MSPDR:

(i) All system requirements have been allocated to the subsystem and
component level and the flow down is adequate to verify system performance.

(ii) The design solutions being proposed are expected to meet the performance
and functional requirements

(iii) The design does not pose major problems that may cause schedule delays.

(iv) Overall system architecture has been established and all launch vehicle to
payload interfaces have been identified and are verifiable

(v) The design solution can be produced based on existing processes and
techniques; if not, risk areas, which require unique and unproven processes,
are identified and risk mitigation plans are established.

(vi) An acceptable operations concept has been developed.

(vii) Preliminary launch vehicle interfaces have been defined.

(viii) Preliminary plans are established for end-to-end testing methodologies.
(ix) 30% mission unique drawings released

Mission Specific Critical Design Review (MSCDR)

The Contractor shall conduct an MSCDR prior to design freeze and before
significant fabrication activity begins. The Contractor shall present a final detailed
design using drawings, analyses, and evaluation testing that shows the design
meets final performance and interface specifications, safety requirements, and
mission objectives. The Contractor shall provide selection criteria for the evaluation
tests performed to prove validity. The mission unique critical design shall be subject
to NASA's approval. NASA reserves the right to withhold approval until all action
items have been closed. As a minimum, the Contractor shall provide verification of
the following items at the MSCDR:

D1B-12


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C5-3
MISSION UNIQUE HARDWARE TEST REPORT

DESCRIPTION/PURPOSE:

This plan describes the qualification and acceptance test results for mission unique hardware.
DATA REQUIREMENTS:

The mission unique hardware test report shall include, as a minimum

(A) | Sequence, configuration, setup, and results for all tests described in the mission
unique hardware test plan (CDRL C5-2)

(B) | Acompliance matrix of test requirements versus tests successfully completed

(C) Reference to or description of any applicable industry standards used to support
testing

(D) Detailed description of any test failures, anomalies, open items, and closure plan

D2-48


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-6
PRE-FLIGHT CONTROLS AND STABILITY ANALYSIS
DESCRIPTION/PURPOSE:

This report describes analyses conducted to ensure an acceptable vehicle mission unique
autopilot design.

DATA REQUIREMENTS:

(A) List all flight conditions analyzed. Reference source for flight condition data (e.g.,
nominal mission trajectory).

(B) Provide tabular-format gain and filter histories for all times during the course of the
mission and provide detailed descriptions of all filters used (by reference, if previously
supplied). Mission unique software electronic-format files are acceptable.

(C) List all vehicle models used including, but not limited to: aerodynamics, mass
properties, structural frequencies, thrust profiles, and liquid slosh representations.
Reference the source for each vehicle model.

(D) List all dispersions used and describe (or reference) how they were defined.

(E) List all software tools used to develop the analyses documented in this report.

(F) Provide detailed descriptions of all linear analysis results, to include rigid body and
flexible mode gain and phase margins at all flight conditions analyzed.

(G) Provide vehicle structural mode frequency histories in graphical or tabular format.

(H) Describe the results of any and all time-domain controllability analyses either generally
applicable to the design or unique to design of the autopilot in the mission unique
software.

(I) Provide detailed flight control system consumables budget, including, but not limited to:

any reaction/attitude control system propellant usage, thrust vector control system
hydraulic fluid expelled, and vernier engine propellant consumed.

D2-37


Section D NASA Launch Services II (NLS I!)
Exhibit 1A: Pegasus Capabilities, Specifications and Environments. Contract NNK10LB01B

This page left intentionally blank.

E1A-2


Section D NASA Launch Services II (NLS II)
Exhibit 1B: Taurus Capabilities, Specifications and Environments Contract NNK10LB01B

This page left intentionally blank.

E1B-28


Section B NASA Launch Services II (NLS II)
SF 1449 Continuation Contract NNK10LB01B

This page left intentionally blank.

B-2


Section D NASA Launch Services II (NLS II)

Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B
SDRL DESCRIPTION Number: S4-2
RESERVED

D3-10


Section D NASA Launch Services II (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: S6-3
RECORDED LAUNCH VEHICLE AND GSE TELEMETRY (TEST, PRE-LAUNCH, LAUNCH)
DESCRIPTION/PURPOSE:

To provide a copy of all launch vehicle and GSE telemetry (RF and Hardwire) allowing NASA
to perform independent data processing and analysis.

DATA REQUIREMENTS:
To provide:

(A) A copy of all system and sub-system test telemetry (RF and hardwire)
data on a compatible media or in an electronic format and corresponding
processing software, if an electronic copy is provided. Telemetry data
must be time correlated in a manner enabling time synchronization of all
telemetry and conforming to the standards defined in IRIG Standard
106-07.

(B) Electronic copy of the raw telemetry (RF and hardwire) data recorded from
all phases of powered flight per SOW paragraph 2.4.1.2.3 shall also be
included.

(C) All RF signal strengths as a function of time from launch until completion
of vehicle safing.

D3-14


CDM RELEASED

Orbifal

NASA LAUNCH SYSTEMS (NLS)
QUALITY MANAGEMENT PLAN

WARNING: INFORMATION SUBJECT TO U.S. EXPORT CONTROL LAWS. The attached documents
contain technical data within the definition of the International Traffic in Arms Regulations, and are subject
to the export control laws of the U.S. Government.

PREPARED BY

Orbital Sciences Corporation
Launch Systems Group
CAGE Code 9X711

ORIGINAL ISSUE DATE TM-18472 REV C
11 JUNE 2004 28 SEPTEMBER 2009
CODE A1-0-A7



Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

26

3.0

The contractor shall provide NASA all anomaly resolutions that affect the integrated
payload/launch vehicle assembly, including both hardware and software. NASA will
approve all integrated payload/launch vehicle anomaly resolutions. The contractor shall
provide insight to Material Review Board (MRB) and failure reporting for all launch
vehicle nonconformances.

The Contractor shall participate in the Government/Industry Data Exchange Program
(GIDEP) and provide Alert System Documentation (CDRL C3-1)

NASA Insight and Approval

The Contractor shall comply with the Government's implementation of NPD 8610.23
and NPD 8610.24 as defined under Section C, Clause 25.0 and the SOW paragraph
2.2.1, Formal Reviews. As part of the standard launch service, the Contractor shall
provide the data, documentation, drawings, analytical models, and support services as
necessary to accommodate the requirements specified under contract Section C,
Clause 25.0, Government Insight and Approval.

The Contractor shall notify NASA of qualification or test anomalies involving similar
launch vehicles, systems, subassemblies and components. The Contractor shall make
available to NASA all problem reports or discrepancy reports on launch vehicle systems’
failures and anomalies. This shall include insight into fleet-wide problems, anomalies,
MRB actions, deviations or waivers to systems, subsystems, materials, processes, and
test equipment including those used on non-NASA missions.

In the event of an anomaly or launch failure, the Contractor shall support NASA's
Failure Review Board, if activated, or shall allow NASA to fully participate in the
Contractor's Failure Investigation Board including those for non-NASA missions.

NASA may elect to have representation as a resident office at the Contractor's major
manufacturing and engineering facilities for the life of the contract. The Contractor shall
provide accommodations and services, such as badging, furniture, telephones, and use
of easily accessible fax and copy machines from one to three residents and up to four
visitors at each location. A minimum of two voice and two data telephone lines shall be
provided. Electronic data transfer compatibility between the resident office and off-site
NASA institutions is required. A resident office will not be required at CCAFS or VAFB,
but NASA will require operational support accommodations (i.e. office space, power,
telephone, communication end instruments for monitoring vehicle testing, etc.) at the
launch complex during NASA launch operations.

NON-STANDARD SERVICES
The Contractor shall provide the non-standard services identified in Exhibit 3 as directed

by the Contracting Officer. Implementation of all non-standard services shall be fully
compliant with this SOW.

D1B-30


Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

the Class 8 clean room; therefore, the payload must be bagged or otherwise
protected during lifting operations. The Contractor shall provide contamination and
environmental monitoring when the payload is exposed. Following encapsulation of
the payload within the fairing but prior to the transportation of the Pegasus launch
vehicle to the Hot Pad, the fairing shall be purged with conditioned filtered air. The
air temperature and relative humidity as measured within the air supply duct at the
fairing inlet shall remain within a range of 18 to 29°C (64.4 to 84.2°F) and <55%
respectively. Air filtration shall be capable of removing 99.97% of all particles
greater than 0.3 microns and removing 95% of all hydrocarbons with a molecular
weight greater than 70. If required, Grade B, Type 1, GNo (or better) per MIL-PRF-
27401F, may be used to purge the fairing environment in place of filtered air. GN2
purge or conditioned air shall not impinge directly on the payload at any point.

Transportation Environment. Following payload encapsulation and during
transportation of the Pegasus launch vehicle to the Hot Pad, the fairing shall be
purged with filtered and dried ambient air. The air temperature and relative
humidity as measured within the air supply duct at the fairing inlet shall remain
within a range of 2 to 29°C (35.6 to 84.2°F) and < 60% respectively. Air filtration
shall be capable of removing 99.97% of all particles greater than 0.3 microns and
removing 95% of all hydrocarbons with a molecular weight greater than 70. If
required, Grade B, Type 1, GN2 (or better) per MIL-PRF-27401F, may be used to
purge the fairing environment in place of filtered air. GN2 purge or conditioned air
shall not impinge directly on the payload at any point.

Fairing Environment During Ground and Flight Operations. Following transportation
of the Pegasus LV to the Hot Pad, the payload fairing shall be purged with
conditioned filtered air. During ground operations, the temperature of the
conditioned air, as measured in the ground air conditioner supply duct at the fairing
inlet, shall be maintained within + 3°C (5.4°F) of a temperature setpoint, selectable
by the payload, from 13 to 29 °C (55.4 to 84.2°F). The humidity of the conditioned
air supply shall be maintained to < 55%. Following the transition to the L1011
Airborne Air Conditioning System (AACS) in preparation for launch operations, the
temperature of the conditioned air shall be measured in the AACS duct downstream
of the filters. During the period of time prior to L1011 takeoff, the AACS air
temperature shall be maintained within the range of 18 to 29 °C (64.4 to 84.2°F).
When the L1011 is in flight, the AACS air temperature shall be maintained within

+ 3°C (5.4°F) of a temperature setpoint, selectable by the payload, from 18 to 38 °C
(64.4 to 100.4°F). The humidity of the AACS air supply shall be maintained to

< 55%. Ground and airborne air filtration shall be capable of removing 99.97% of all
particles greater than 0.3 microns and removing 95% of all hydrocarbons with a
molecular weight greater than 70. If required, Grade B, Type 1, GNo (or better) per
MIL-PRF-27401F, may be used to purge the fairing environment in place of filtered
air. GNz purge or conditioned air shall not impinge directly on the payload at any
point.

D1A-25


Section D NASA Launch Services II (NLS II)
Attachment D11: Definitions Contract NNK10LB01B

ATTACHMENT D11
DEFINITIONS

Anomaly: An unexpected event that can reasonably be considered to pose immediate mission
success implications for subsequent NASA missions. An anomaly requires an engineering
evaluation and Engineering Review Board disposition prior to a NASA mission flight on an
affected launch vehicle configuration

Authority to Proceed: Notification from the Contracting Officer via task order award to proceed
with work on either a Launch Service Task Order (LSTO) or Special Task Assignment.

Baseline ICD: First approved and signed release of ICD.
Certified Common Launch Vehicle Configuration: A common launch vehicle configuration

which has met the requirements defined in NPD 8610.7 for a specific launch vehicle risk
category

Common Launch Vehicle Configuration: A distinct combination of core propulsive stages and
hardware used to deliver payloads to earth orbit or escape trajectories.

Core Propulsive Stages: All propulsive stages except strap-on motors, final stages
(exclusively used for orbit circularization or escape), and trim stages.

Common Launch Vehicle Configuration Upgrades or Modifications: Items that do not
substantially affect operating time, total impulse, and/or the thrust profile of one or more
propulsive stages are considered upgrades or modifications to the certified common vehicle
configuration. Examples of upgrades and modifications include changes in software, payload
fairing, payload electrical/mechanical interfaces, incorporation of mission-unique requirements,
and the addition or deletion of a final stage (exclusively used for orbit circularization or
escape), strap-on motors, and/or trim stage. Upgrades or modifications are not to be
interpreted as common vehicle configuration changes.

Common Launch Vehicle Configuration Changes: Items that substantially affect the airframe
integrity, operating time, total impulse and/or thrust profile of one or more core propulsive
stages are considered changes to the certified common vehicle configuration. Examples of
vehicle configuration changes include the replacement of engine types, core propulsive stages,
and/or major airframe structures.

Covered Launch Activities: Any and all activities involved in the preparation of a launch
vehicle and payload for launch, and conduct of the launch, when those activities take place at
a launch site in the United States.

D11-1


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

(d)

(e)

(7) 52.226-6, Promoting Excess Food Donation to Nonprofit Organizations.
(Mar 2009) (Pub. L. 110-247).

(8) 52.237-11, Accepting and Dispensing of $1 Coin (Sep 2008) (31 U.S.C
5112(p)(1))

Comptroller General Examination of Record. The Contractor shall comply with the
provisions of this paragraph (d) if this contract was awarded using other than
sealed bid, is in excess of the simplified acquisition threshold, and does not contain
the clause at 52.215-2, Audit and Records-Negotiation.

(1)

The Comptroller General of the United States, or an authorized representative
of the Comptroller General, shall have access to and right to examine any of
the Contractor's directly pertinent records involving transactions related to this
contract.

The Contractor shall make available at its offices at all reasonable times the
records, materials, and other evidence for examination, audit, or reproduction,
until three (3) years after final payment under this contract or for any shorter
period specified in FAR Subpart 4.7, Contractor Records Retention, of the
other clauses of this contract. If this contract is completely or partially
terminated, the records relating to the work terminated shall be made
available for three (3) years after any resulting final termination settlement.
Records relating to appeals under the disputes clause or to litigation or the
settlement of claims arising under or relating to this contract shall be made
available until such appeals, litigation, or claims are finally resolved

As used in this clause, records include books, documents, accounting
procedures and practices, and other data, regardless of type and regardless
of form. This does not require the Contractor to create or maintain any record
that the Contractor does not maintain in the ordinary course of business or
pursuant to a provision of law.

Notwithstanding the requirements of the clauses in paragraphs (a), (b), (c)
and (d) of this clause, the Contractor is not required to flow down any FAR
clause, other than those in paragraphs (e)(1) of this paragraph in a
subcontract for commercial items. Unless otherwise indicated below, the
extent of the flow down shall be as required by the clause --

(i) 52.203-13, Contractor Code of Business Ethics and Conduct
(Apr 2010) (Pub. L. 110-252, Title VI, Chapter 1 (41 U.S.C. 251 note)).

(ii) 52.219-8, Utilization of Small Business Concerns (May 2004)(15 U.S.C.
637(d)(2) and (3)), in all subcontracts that offer further subcontracting
opportunities. If the subcontract (except subcontracts to small business

C-57


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

25.9

26.0

26.1

26.2

26.3

27.0

(S) Conduct of Contractor-chaired Mission, Launch, and Flight Readiness Reviews
(T) Post-flight vehicle, tracking, and Range data
(U) Post-flight anomaly investigations/close-outs.

Notwithstanding the insight and approvals set forth in Clause 25.0 herein, the
Contractor assumes full performance responsibility as set forth in this contract, and
neither the Government's insight nor its approval under this paragraph 25 shall be
construed as a defense to any finding of mission success or final acceptance / rejection
of the launch service.

GOVERNMENT LAUNCH READINESS ASSESSMENT

The Contractor shall participate in a NASA-chaired Launch Readiness Review (LRR)
(reference 2.2.1.3(E) of the SOW). At the LRR, the Contractor shall summarize the
status of its launch vehicle and all supporting elements and attest to readiness to launch
the mission. If, after due consideration of the status of the launch vehicle, payload and
other launch support systems, NASA does not agree that the total mission is ready for
launch, NASA has the right to delay the launch.

The Contractor shall poll NASA in the final launch countdown and any re-cycle
procedure during status checks for their approval of the final launch readiness
assessment. NASA may declare a "HOLD" and delay the launch at any time during the
final launch countdown

In the event NASA delays the launch, as a result of exercising its rights under this
clause, and the causes of the delay were within the control of or due to the fault or
negligence of the Contractor or its Subcontractors at any tier, then the provisions of
Section C, Clause 19.0, Adjustments to Launch Schedule shall govern and the
Contractor shall be deemed to have caused the delay. For the purpose of this clause,
the burden of proof for showing that the causes of delay were within the control or fault
and/or negligence on the part of the Contractor or its Subcontractors at any tier rests
with NASA. If NASA delays the launch beyond the grace period established in Section
C, Clause 19.0 and the causes of the delay were not within the control or due to the
fault or negligence of the Contractor or its Subcontractors at any tier, then the provisions
of Section C, Clause 19.0, Adjustments to Launch Schedule shall apply

LICENSES AND PERMITS FOR A LAUNCH SERVICE OPERATOR

The Contractor shall obtain and maintain the necessary licenses, permits and clearances that
may be required by the Department of Transportation, Department of Commerce, Department
of Defense, NASA, or other Governmental agencies in order to provide launch services under
this contract. No Federal Aviation Administration commercial launch license is required under
this contract. All costs and fees associated with obtaining licenses, permits and clearances

C-43


Section D NASA Launch Services II (NLS II)
Attachment D7: Quality Management Plan Contract NNK10LB01B

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D7-2


Section D NASA Launch Services II (NLS II)
Exhibit 3B: Taurus Non-Standard Services List Contract NNK10LB01B

This page left intentionally blank.

E3B-2


Section D NASA Launch Services II (NLS Il)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

2.4.1.2.1 Vehicle Telemetry

Telemetry data shall be archived in an industry standard format compatible with NASA's
LSP Data Center. All recordings shall include direct receiver video-out data when
available, as well as reshaped data waveforms when applicable for each designated
telemetry link. Archived data should include, if available, receiver signal strengths,
tracking antenna azimuth/elevation and IRIG-B Timing. All media shall be clearly
documented and labeled with the mission, date, record length and any and all channel
assignments and associated digital sample rates or clock rates per channel recorded.

2.4.1.2.2 Baseline and Integrated Vehicle Support

The Contractor shall provide, in electronic form, all raw launch vehicle and GSE
telemetry (RF and hardwire) formats described in sufficient detail to allow NASA to
process and verify the data prior to initial launch vehicle power-up at the launch site
This shall include a detailed listing and description of all measurements and calibration
coefficients for all launch vehicle and GSE telemetry (TM) links including the guidance
system and any embedded data streams. The Contractor shall provide to the NASA
LSP Data Center, via electronic format, any changes to the launch vehicle and/or GSE
telemetry format as the change is implemented to the launch vehicle and/or GSE
telemetry streams (CDRL C6-1).

The Contractor shall provide NASA with a compatible data recording (CDRL C6-2)
representative of the telemetry (RF and hardwire) signals of the launch vehicle and GSE
prior to the initial launch vehicle power-up test on each mission. This will allow NASA to
verify its ability to process the Contractor's telemetry (SDRL S6-1).

The Contractor shall submit an initial end-to-end launch vehicle telemetry path test plan
(SDRL S6-2) NLT 6 months prior to launch. This plan shall describe the telemetry links
from the launch vehicle through down range and deployable telemetry assets specific to
that mission. The plan shall identify and/or suggest orbiting or ground locations and/or
mobile assets to meet LSP telemetry coverage requirements. The Contractor shall
submit a final end-to-end launch vehicle telemetry path test plan NLT sixty (60) calendar
days prior to launch. The final plan shall verify the adequacy of telemetry link margins
with down range assets, and shall include link margin analysis and shall present data
flow diagrams between the NASA designated NASA LSP Data Center and downrange
assets

The Contractor shall record all launch vehicle and GSE telemetry streams while the
vehicle is powered prior to launch. The Contractor shall provide real-time launch
vehicle and GSE telemetry (RF and/or hardline) data to the NASA designated LSP Data
Center for system level launch vehicle testing (system-level testing to include anytime
the vehicle or stage is powered and exercised, with data transmitted from the flight
telemetry system for the purpose of evaluating system health and function). Examples
include, but are not limited to, telemetry test data during initial vehicle power-up, flight

D1A-20


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D044


Section C NASA Launch Services II (NLS I!)

Contract Terms and Conditions Contract NNK10LB01B
43 Reserved
44 Reserved

5.0

5.1

5.2

5.3

5.4

5.5

(A) Reserved
(B) Reserved
(C) Reserved
(D) Reserved

LAUNCH SERVICE PAYMENTS, MILESTONE EVENTS AND COMPLETION
CRITERIA

The Contracting Officer will notify the Contractor of ATP of the launch service via award
of the task order.

Upon successful completion of a milestone event and submission of a properly certified
invoice, the Contractor may request commercial interim payments. The commercial
interim payments will be paid in accordance with the payment schedule shown in Table
C-1 and based on the milestone events identified in the contract Work Plan (Attachment
D8).

Commercial interim payments are contract financing payments that are not payment for
accepted items. Commercial interim payments are fully recoverable, in the same
manner as progress payments, in the event of default. Commercial interim payments
are contract financing payments and, therefore, are not subject to the interest-penalty
provisions of prompt payment. However, these payments shall be made in accordance
with the Agency's policy for prompt payment of contract financing payments. In
accordance with 42 U.S.C. 2465d, NASA shall not take title to launch vehicles under
contract for launch services

In the event an LSTO is issued at twenty-four (24) months or less prior to launch, the
initial payment for such launch service will be the cumulative total of all payments that
would have been paid if the LSTO had been issued at L-30 months. If a non-standard
service is ordered when an LSTO is issued, the initial payment shall include the catalog
price adjustment.

Scheduled dates in Table C-1 are tentative and represent invoice submission dates.
Payment schedules may be deferred or canceled by the Government if the Contractor
fails to make substantial progress in accomplishing the major launch service milestone
events in the attached contract Work Plan. Payments falling due in the first quarter of
each fiscal year (October - December) shall be paid promptly to the maximum extent
practicable, but shall not be considered late until January 31 of the following calendar


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-11
MISSION UNIQUE SOFTWARE
DESCRIPTION/PURPOSE:

Ensure the mission unique software is consistent with the analyses and data products
delivered under CDRLs C4-2, C4-3, C4-6, C4-7, and C4-9.

DATA REQUIREMENTS:

(A) Provide a report describing the methods used to check validity of the mission unique
software (by reference if previously supplied).

(B) | Provide a memorandum or report documenting the results of mission unique software
validation tests. At a minimum, this report shall include comparison of hardware-in-the-
loop flight simulation test results with all required event sequences and the target
insertion state.

(C) Copy, in electronic format (ASCII test), of all mission constants, data loads, or |-loads

for the mission. This data shall match the flight values used in the vehicle flight
program

02-43


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C6-1
VEHICLE AND GSE TELEMETRY FORMATS
DESCRIPTION/PURPOSE:

To provide all telemetry (RF and hardwire) formats for vehicle systems, GSE and sub-systems
testing, including detailed description of formats that will allow NASA to process, display and
verify all launch vehicle and GSE telemetry (RF and hardwire)

DATA REQUIREMENTS:
The raw vehicle and GSE telemetry (RF and hardwire) formats shall include as a minimum:

(A) PCM Data Stream Description: this file will describe the format of the Pulse Code
Modulation (PCM) telemetry data stream. A new file must be delivered if the
formatting of the PCM data stream is modified. It must include:

(i) Bit rate in bits per second

(ii) Location and description of sync word
(iii) | Number of minor frames in major frame
(iv) Size of minor frame

(v) Number of bits per word or syllable

(B) | Measurement Description File: this file must be standard ASCII text or another
format easily read with a personal computer using commercially available
software. A new file must be delivered if any measurement or calibration
changes are made to the launch vehicle and/or GSE telemetry stream. It must
include:

(i) Measurement ID

(ii) Measurement description

(iii) | Engineering units of measurement

(iv) Location of measurement in minor frame

(v) Word step rate of measurement if supercommutated
(vi) | Size of measurement in bits or bytes

(vii) Type of measurement

(viii) Initial minor frame number where measurement is found

(vii) Type of measurement

D2-51


Section C
Contract Terms and Conditions Contract NNK10LB01B

NASA Launch Services II (NLS II)

2.0

2.1

(2)

(3)

(4)

(i) If a Contractor has legally changed its business name, “doing business
as” name, or division name (whichever is shown on the contract), or has
transferred the assets used in performing the contract, but has not
completed the necessary requirements regarding novation and change-
of-name agreements in Subpart 42.12, the Contractor shall provide the
responsible Contracting Officer a minimum of one business day’s written
notification of its intention to:

(A) Change the name in the CCR database;
(B) Comply with the requirements of Subpart 42.12 of the FAR;

(C) Agree in writing to the timeline and procedures specified by the
responsible Contracting Officer. The Contractor must provide with
the notification sufficient documentation to support the legally
changed name.

(ii) If the Contractor fails to comply with the requirements of paragraph
(t)(2)(i) of this clause, or fails to perform the agreement at paragraph
(t)(2)(i)(C) of this clause, and, in the absence of a properly executed
novation or change-of-name agreement, the CCR information that shows
the Contractor to be other than the Contractor indicated in the contract
will be considered to be incorrect information within the meaning of the
“Suspension of Payment” paragraph of the electronic funds transfer
(EFT) clause of this contract.

The Contractor shall not change the name or address for EFT payments or
manual payments, as appropriate, in the CCR record to reflect an assignee
for the purpose of assignment of claims (see FAR Subpart 32.8, Assignment
of Claims). Assignees shall be separately registered in the CCR database.
Information provided to the Contractor’s CCR record that indicates payments,
including those made by EFT, to an ultimate recipient other than that
Contractor will be considered to be incorrect information within the meaning of
the “Suspension of payment’ paragraph of the EFT clause of this contract

Offerors and Contractors may obtain information on registration and annual
confirmation requirements via the Internet at http://www.ccr.gov or by calling
1-888-227-2423, or 269-961-5757.

ON-RAMP AND TECHNOLOGY INSERTION

The purpose of the IDIQ On-Ramp is to create an opportunity for qualified new,
emerging launch service providers and for incumbent launch service providers to
introduce launch vehicles not available at the time of the award of the initial contract and
to compete for additional requirements not identified as firm or option requirements

C-13


Section D NASA Launch Services II (NLS I!)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

(F) Provision for launch site services to meet payload requirements agreed to in the
Mission ICD such as: power, air conditioning, GN,/GHe purges, and contamination
control.

io)

Support of all activities required to de-mate and to return the payload from the Hot
Pad to the processing facility if necessary. The return of the payload to the
processing facility from a remote launch site or airfield will be performed as a
mission-unique service.

(H) Preparation of the procedures for integrated launch vehicle/payload operations for
NASA approval and incorporation of the payload procedures as appropriate (CDRL
C5-5).

(1) Coordination of payload and launch vehicle operations into an integrated
operational flow, preparation of the schedules, and provision of the schedules with
updates as needed to NNC.

(J) Provision of contamination control for payloads while they are in the possession of
the Contractor, or in a Contractor-provided PPF IAW the SOW, paragraph 2.4.2.3.

(K) Reserved.

(L) Certification of payload contamination control requirements for: fairing surface
cleanliness, cleanroom environments, and purge system cleanliness.

(M) Support for the installation of customer provided RF re-radiating equipment as
ground support equipment in the payload processing facility.

(N) Provision for the planning and execution of activities associated with the integrated
testing of the customer's payload with the launch vehicle on the hot pad

2.4.2.3. Contamination and Environmental Control

The Contractor shall provide and implement a generic payload contamination control
plan and, if required, provide and implement a contamination control implementation
plan for each payload. Using IEST-STD-CC1246D, MIL-PRF-27401, ISO 14644-1, ISO
14644-2,and NASA RP-1124 (Rev-4) as guidelines, the launch service shall meet the
following minimum requirements:

(A) Payload/Vehicle Integration Environment. For all Contractor-provided facilities
where the payload resides and is exposed (including payload processing facilities
and integration facilities), a 12'(W) x 24’(L) x 14'(H) Class 8 clean room
environment IAW ISO 14644-1 shall be provided. The environment within the clean
room shall be maintained within a temperature and humidity range of 18 to 29 °C
(64.4 to 84.2 °F) and < 55%, respectively. Overhead crane lifts must occur outside

D1A-24


Section D NASA Launch Services II (NLS II)
Exhibit 2B: Taurus Standard Services Contract NNK10LB01B

This page left intentionally blank.

E2B-2


Section D NASA Launch Services II (NLS I)

Exhibit 2B: Taurus Standard Services Contract NNK10LB01B
SOW . a.
$s Service
Para. tandard Description

E2B-5


wT

Section D

NASA Launch Services II (NLS II)
Exhibit 2B: Taurus Standard Services :

Contract NNK10LB01B

SOW . ae
Para. Standard Service Description

E2B-9


Section C NASA Launch Services I! (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

9.3

9.4

9.5

10.0
11.0

12.0

Executed Special Task Assignments shall be incorporated by reference into the contract
via contract modification to include the following: Special Task Assignment number,
title, number of labor hours, and firm fixed price. The contract modification will reflect
the firm fixed price of the Special Task Assignments with respect to the adjustment of
the contract value and any other terms deemed pertinent.

Costs and/or labor hours incurred in excess of those authorized by the Contracting
Officer shall be at the Contractor's own expense. Failure to agree to any adjustment
shall be handled IAW the Contract’s Disputes clause. However, nothing in this clause
shall excuse the Contractor from proceeding with the Special Task Assignment as
written.

The price for completion of special task assignments under CLIN 10 will be paid upon
satisfactory completion of each individual Special Task Assignment.

RESERVED

FAR 52.216-18 ORDERING (OCT 1995) [Note: Applicable to IDIQ contract portion
only]

(a) Any supplies and services to be furnished under this contract shall be ordered by
issuance of delivery orders or task orders by the individuals or activities designated
in the Schedule. Such orders may be issued from the effective date of the contract
through the second quarter of calendar year (June 30, 2020). Special task
assignment and non-standard service task orders may be issued from the effective
date of the contract through the completion of all LSTOs.

(b) All delivery orders or task orders are subject to the terms and conditions of this
contract. In the event of conflict between a delivery order or task order and this
contract, the contract shall control.

(c) If mailed, a delivery order or task order is considered “issued” when the
Government deposits the order in the mail. Orders may be issued orally, by
facsimile, or by electronic commerce methods only if authorized in the Schedule.

FAR 52.216-19 ORDER LIMITATIONS (OCT 1995) [Note: Applicable to IDIQ
contract portion only]

(a) Minimum order. When the Government requires supplies or services covered by
this contract in an amount of less than:

(1) One Launch Service, or
(2) One Special Task Assignment, or
(3) One Non-Standard Service

The Government is not obligated to purchase, nor is the Contractor obligated to
furnish, those supplies or services under the contract.

C-25


Section D NASA Launch Services II (NLS II)
Exhibit 4: Sample Certificate of Flight Readiness Contract NNK10LB01B

This page left intentionally blank.

E4-2


Section D NASA Launch Services I! (NLS II)
Attachment D7: Quality Management Plan Contract NNK10LB01B

ATTACHMENT D7

QUALITY MANAGEMENT PLAN


Section D NASA Launch Services II (NLS I!)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C5-1
VEHICLE DATA PACKAGE
DESCRIPTION/PURPOSE:

This item is a data package of vehicle hardware and software changes that are neither dictated
by payload requirements nor represent fleet-wide changes.

DATA REQUIREMENTS:
Package shall include, as a minimum:
(A) — Adescription of the item, the modification, and the purpose of the modification

(B) For all hardware changes, an indentured part list of the item, which shall define the
difference between the assigned configuration and the as-built configuration and
supporting rationale for differences. For purposes of this requirement, the as-built
configuration excludes standard usage hardware (e.g., nuts, bolts, washers, shims, and
pins). The as-built configuration list shall contain:

(i) Deliverable equipment part name, number, and serial number
(ii) Quantity

(iii) | Drawing number or traceability code

(

iv) | Drawing dash number, change letter and unincorporated Engineering Orders
(EOs)

(v) For EEE parts: circuit reference designators, part numbers, part manufacturers,
and part lot data codes/serial numbers

(C) For software changes, a copy of all change documentation shall be provided, along with
a laboratory and field testing plan

(D) Test Report/Data/Conclusions - A copy of the test procedures, a description of all
changes since item qualification, a description of major fabrication anomalies and their
disposition, a copy of the test data, a copy of any test failure reports and their
disposition, and final approval signatures. For ordnance, inspection data records and a
copy of the lot test data shall also be submitted.

(E) Operating Time/Cycle - Status at the time of delivery of accumulated operating time
and/or critical cycles history of parts designated as time/cycle critical

(F) Allowable (specification requirement) and remaining operating time and/or cycles from
point of delivery

D2-46


Section D NASA Launch Services II (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

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D1A-34


Section D NASA Launch Services II (NLS II)
Attachment 04: SB and SDB Subcontracting Plan Contract NNK10LB01B

LSG shall, at a minimum, maintain at least the following types of records to document
compliance with this subcontracting plan:

(a) SB, VOSB, SDVOSB, HUBZone SB, SDB, and WOSB Source lists, guides and other
data identifying SB, VOSB, SDVOSB, HUBZone SB, SDB and WOSB suppliers.

(b) Organizations contacted for SB, VOSB, SDVOSB, HUBZone SB, SDB, and WOSB
sources

(c) Records to support internal activities to guide and encourage buyers, workshops,
seminars, training programs, etc., monitoring activities to evaluate compliance.

(d) On a contract-by-contract basis, records on all subcontract solicitations, over $100,000
indicating on each solicitation (a) whether SB concerns were solicited, and if not, why
not; (b) whether VOSB, SDVOSB, HUBZone SB, SDB and WOSB concerns were
solicited, and if not, why not; and (c) reason(s) for the failure to solicit SB, VOSB,
SDVOSB, HUBZone SB, SDB, and WOSB concerns

(e) Contract by Contract Award Data - Data for contract by contract reporting will be
provided by a computer-generated report. The report identifies the purchase agreement
number, size status of subcontractor, dollar value of procurement, and supplier
identification code

(f) A database containing the classification of suppliers

D4-10


Section D NASA Launch Services I! (NLS !I)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B
CDRL DESCRIPTION Number: C1-2 (cont.)

(iii)
(iv)
(v)

Range requirements
Collision avoidance (COLA)
Tracking and telemetry

The document shall also identify critical measurements during the launch
countdown. Not to exceed values shall be identified for all critical
measurements.

Redline Document

A document that identifies monitored measurements, applicable in test
and countdown, used to verify that the Launch Vehicle and ground
systems are operating within normal limits. This document shall include
Operational and Redline limits which, if specified parameters minimum or
maximum values are exceeded, indicate: a condition that may be
hazardous to personnel, vehicle, or site; a condition which may
compromise the successful completion of the vehicle mission or, a
condition that is outside of the expected range based on previous
experience or analysis.

02-9


Section D

NASA Launch Services Ii (NLS II)

Attachment D4: SB and SDB Subcontracting Plan Contract NNK10LB01B

This individual's specific duties, as they relate to LSG's subcontracting program include
general overall responsibility for this company's Small Business Development (SBD) program,
the development, preparation and execution of individual subcontracting plan goals, and
monitoring performance relative to contractual subcontracting requirements contained in this
plan, including, but not limited to:

(a)

Obtaining SBs, VOSBs, SDVOSBs, HUBZone SBs, WOSBs, and SDBs
(inclusive of ANCs and Indian Tribes), including historically Black Colleges
and Universities (HBCUs) and Minority Institutions (MIs) sources from all
applicable agencies such as Small Business Administration (SBA).

Assuring inclusion of SBs, VOSBs, SDVOSBs, HUBZone SBs, WOSBs
and SDB (inclusive of ANCs and Indian Tribes) concerns including,
HBCUs and Mls in all solicitations where appropriate.

Attending or arranging for attendance at relevant business opportunity
workshops, seminars, trade fairs, etc. Planned attendance at the Offices
of Small and Disadvantaged Business Utilization conference and the 21st
Annual High-Tech Small Business Conference should help to increase our
small business participation. Orbital LSG has plans to increase its
visibility into the local (Phoenix, AZ) Small Business Administration
activities in an attempt to connect with more small businesses. In
addition, the idea of participation as a mentor in the Small Business
Administration's Mentor- Protégé Program has been recommended as a
course of action for greater small business relationship building.

Conducting or arranging for conduct of motivational training for purchasing
personnel pursuant to the intent of Public Law 95-507, and current FAR
requirements. This training is planned for the first quarter of 2009 and will
be taught by our new Procurement Compliance Manager who will also be
the Small Business Plan Administrator. The goal is that our procurement
and subcontracting professionals will help identify small business
opportunism for Orbital based on their new awareness and sensitivity to
this important issue.

Monitoring attainment of proposed goals.
Submission of Individual Subcontracting Plans (ISRs- formally SF 294s)

and Summary Subcontract Report (SSRs- formally SF 295s) into the
Electronic Subcontracting Reporting System (eSRS)

D4-8


Section D NASA Launch Services |I (NLS II)
Attachment D4: SB and SDB Subcontracting Plan Contract NNK10LB01B

This page left intentionally blank

D4-2


Section D NASA Launch Services II (NLS II)
Attachment D6: Reliability Plan Contract NNK10LB01B

This page left intentionally blank.

D6-2


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-9
RF LINK ANALYSIS
DESCRIPTION/PURPOSE:
This analysis is performed for each nominal mission trajectory and is required to ensure
sufficient RF Link margins exist for both the telemetry and flight termination systems during all
phases of powered flight through payload separation. This analysis also supports pre-flight
verification of compliance with mission requirements.
DATA REQUIREMENTS:
The document shall include the following data as a minimum:

(A) Definition and description of all coordinate systems used.

(B) Identification of the mission trajectory used.

(C) Nominal, maximum and minimum loss / gain factors for all elements in each
TX/RX signal propagation path

(D) A listing of all ground and mobile telemetry station locations and space based
telemetry assets.

(E) An electronic copy of respective antenna patterns (one submittal required per
vehicle configuration and as changed) with Theta, 8, having values from zero (0)
to one hundred eighty (180) degrees and Phi, ~, having values from zero (0) to
three hundred sixty (360) degrees for both magnitude and phase in a maximum
of five (5) degree increments.

(F) Analysis outputs (Contractor format acceptable), which must capture all
information presented in the sample figure below (see Figure D2-1)

D2-40


Section D NASA Launch Services II (NLS II)
Attachment D1B:_Taurus Statement of Work (SOW) Contract NNK10LB01B

simulation prior to payload mate, and flight simulation following payload mate (SDRL
S6-3).

The Contractor shall provide compatible data of all recorded launch vehicle and GSE
telemetry (CDRL C6-2)

The Contractor shall provide a mutually agreed upon transport interface or extend the
Spacecraft command and telemetry streams between the launch complex and the
NASA designated NASA LSP Data Center.

The Contractor shall provide voice and video communications from the launch complex
to the designated NASA LSP Data Center during integrated and stand-alone spacecraft
operations at the launch complex.

The Contractor shall implement the NASA provided console communications
configuration for those consoles occupied by the NASA team within the Contractor's
launch control center. The Contractor shall validate this configuration with the
designated NASA LSP Data Center prior to launch vehicle testing and mission
simulations.

The Contractor shall provide to NASA, upon request, launch vehicle processing test
procedures in a mutually agreed upon electronic format prior to the test (SDRL S5-1)

The Contractor shall submit to NASA a draft version of a preliminary Statement of Work
for each downrange asset no later than four (4) months prior to launch.

The Contractor shall coordinate the downrange assets and shall provide NASA the
latest documentation required by the downrange assets (e.g. PRD, Expedite OR, etc)
for receiving, recording, and relaying the data no later than sixty (60) days prior to
launch. The Contractor shall ensure proper operation of all launch vehicle telemetry
links (RF and hardwire), voice communication channels, and video (including launch
vehicle mounted camera video as applicable) to the NASA designated NASA LSP Data
Center prior to baseline launch vehicle processing. The Contractor shall provide the
downrange assets with the technical coordination needed to execute the telemetry
coverage (e.g. telemetry playback tapes, mission trajectory disks, etc) prior to the first
data flow test. The Contractor shall ship required electronic hardware and satisfy export
control and frequency authorizations as required by local and international
governments.

The Contractor shall provide data flow path diagrams and data flow schedules between
the NASA designated NASA LSP Data Center and down range assets to NASA NLT
fifteen (15) calendar days prior to launch and again at the Flight Readiness Review
(SDRL S6-4). The Contractor shall also provide down range asset status/readiness at
the Flight Readiness Review.

D1B-21


Section D NASA Launch Services II (NLS II)
Exhibit 5: Reserved Contract NNK10LB01B

CLINS 1 THROUGH 10 DATA SHEETS

RESERVED


Section D NASA Launch Services II (NLS II)
Attachment D11: Definitions Contract NNK10LB01B

Powered Flight: Any phase of vehicle flight where the vehicle stage main propulsion system is
operating, with the sole exception of propellant or pressurant venting phases where no
combustion occurs.

Preliminary ICD: Working copy of the ICD released prior to the first signed release

Primary Payload: The payload which serves to determine the launch day and time, and without
which the vehicle would not launch.

Related Party:
(i) Any of the Parties’ directors, officers, agents, employees or customers

(ii) Any of the Parties’ contractors, subcontractors, or suppliers at any tier
involved directly or indirectly in the performance of this Contract

(iil) Any entity having any right, title or interest, whether through sale, lease
or service arrangement or otherwise, directly or indirectly, in the payload,
the launch vehicle, or the launch service value

Secondary Payload: Any payload carried by the launch vehicle in space not required by the
primary payload. The secondary payload requires the approval of the primary payload
customer prior to manifesting. If the secondary payload is not ready to support scheduled
launch day, the secondary payload will be demanifested and replaced with a mass simulator.
Successful Flight: A launch which met primary mission requirements.

Third Party: Any person or entity other than NASA, the Contractor, and related parties.

D11-3


Section C NASA Launch Services |] (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

31.0

31.1

31.2

31.3

31.4

32.0

32.1

DOMESTIC SOURCE CRITERIA

In addition to the certification regarding United States commercial provider of space
transportation services (Public Law 105-303, Title Il, Section 201), the Contractor shall
continue to comply with domestic source criteria. Failure to comply with the criteria may
be grounds for “Termination for Cause” in accordance with contract Section C, Clause
1.0(m)

Participation in this procurement is restricted to prime Contractors from the United
States launch vehicle/services industry “United States industry” means any
corporation, partnership, joint venture, association, or other entity which is organized or
existing under the laws of the United States or any State, and whose controlling interest
is held by United States citizens. “Launch services” means all services required in the
performance of this contract, excluding those necessary to produce or manufacture
launch vehicles, its components and other equipment and facilities required in the
performance of the contract. “Controlling interest” means ownership of an amount of
equity in such entity sufficient to direct management or to void transactions entered into
by management. Ownership of at least fifty-one (51) percent of the equity creates a
rebuttable presumption that such interest is controlling

The Contractor shall provide in the performance of this contract launch vehicles that are
domestic end products. The launch vehicle shall be a domestic end product only if the
cost of its components, mined, produced or manufactured in the United States exceeds
50 percent of the cost of all its components. The cost of each component includes
transportation costs to the place of incorporation into the launch vehicle and any
applicable duty (whether or not a duty-free entry certificate is issued). “Components,”
as used in this contract clause, means those materials and supplies directly
incorporated into the end product.

The Contractor shall provide, in the performance of this contract, domestic launch
services. Launch services shall be considered to be domestic if the cost for launch
services performed by United States industry sources exceeds 50 percent of the cost of
the total required launch services.

LIABILITY FOR THIRD PARTY CLAIMS

This contract clause applies to Third Party claims that arise out of the conduct of
hazardous launch activities during the provision of launch services under this contract.
More specifically, this contract clause allocates between the Government and the
Contractor the risk of Third Party claims for damage to or loss of property or personal
injury or death arising from the burning, explosion, detonation, combustion or impact of
a launch vehicle, its payload, or a component thereof, whether or not the payload is
separated from the launch vehicle, from the time of launch until thirty (30) days after
launch.

C-49


Section D NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B
Application Test Analysis (No Test)
Yield Ultimate Yield Ultimate
Non-Man Rated 1.10 1.25 1.60 2.0

42

43

5.0

6.0

Table D1-B: Mission Unique Hardware Factors of Safety
Mission Unique Software

The Contractor shall provide source code and mission constants’ listings (CDRL C4-11)
with appropriate requirement specifications to support NASA approval of mission unique
software. The Contractor shall prepare and submit a pre-flight control system and
stability analysis report (CDRL C4-6) for the vehicle and mission unique software used
for each mission

Unanticipated Mission Unique Services

At the time of contract award, the Government may not have identified all mission
unique services required for each mission. As unanticipated mission unique services
are identified, the Contracting Officer will authorize the Contractor, in accordance with
FAR 52.243-1, Changes — Fixed Price Alt |, to perform these services. In performing
unanticipated mission unique services, the Contractor shall design the necessary
ground and flight hardware/software; conduct appropriate design reviews; and
manufacture, test and qualify for flight launch vehicle mission unique
hardware/software, i.e., other than that provided as a standard service (Exhibit 2) or
described in the non-standard services list (Exhibit 3).

SPECIAL TASK ASSIGNMENTS

The Contractor shall be required to perform special studies and analyses, provide
materials, or fabricate hardware in support of this contract. Each task will be initiated by
written direction from the NASA Contracting Officer. These tasks generally include:
advance planning and feasibility studies in support of future contemplated missions;
analyses in support of change requirements to authorized missions; development,
fabrication, and test of hardware/software to support planning studies or special tests;
mission unique studies; material provision; and hardware fabrication in support of
potential missions prior to mission authorization.

INFORMATION TECHNOLOGY SECURITY

The contractor shall comply with NPR 2810.1A, NASA’s Policy on the Security of
Information Technology for LSC IT hardware and/or software provided to NASA. New
IT hardware and/or software systems delivered to NASA shall be compliant prior to
authorization to process. The contractor shall develop, update and implement an IT
Security Plan compliant with NPR 2810.1A. NASA IT Security personnel will evaluate
the LSC IT hardware and/or software security and determine compliance prior to NASA
acceptance.

D1A-31


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

shall apply to any claims for Damage, whatever the legal basis for such claims,
against:

(i) A Party;

(ii) A Party to another NASA Agreement or contract that includes flight on the
same Launch Vehicle;

(iii) A Related Entity of any of the entities identified in (c)(1)(i) or (c)(1)(ii) of this
clause; or

(iv) The employees of any of the entities identified in (c)(1)(i) through (c)(1)(iii) of
this clause.

(2) The contractor agrees to extend the cross-waiver of liability as set forth in
paragraph (c)(1) of this clause to its own subcontractors at all tiers by requiring
them, by contract or otherwise, to:

(i) Waive all claims against the entities or persons identified in paragraphs
(c)(1)(i) through (c)(1)(iv) of this clause; and

(ii) Require that their Related Entities waive all claims against the entities or
persons identified in paragraph (c)(1)(i) through (c)(1)(iv) of this clause.

(3) For avoidance of doubt, this cross-waiver includes a cross-waiver of claims
arising from the Convention on International Liability for Damage Caused by Space
Objects, which entered into force on September 1, 1972, where the person, entity, or
property causing the Damage is involved in Protected Space Operations and the
person, entity, or property damaged is damaged by virtue of its involvement in
Protected Space Operations.

(4) Notwithstanding the other provisions of this clause, this cross-waiver of liability
shall not be applicable to:

(i) Claims between the Government and its own contractors or between its own
contractors and subcontractors;

(ii) Claims made by a natural person, his/her estate, survivors, or subrogees
(except when a subrogee is a Party to an Agreement or is otherwise bound by
the terms of this cross-waiver) for bodily injury to, or other impairment of health,
or death of such person;

(iii) Claims for Damage caused by willful misconduct;

(iv) Intellectual property claims;

C-67


Section C NASA Launch Services II (NLS 11)
Contract Terms and Conditions Contract NNK10LB01B

Launch Service Payment Schedule

Milestone/ Payment(s) Amount Cumulative Termination for
Commercial|Months Before /| (% of Amount of Convenience of the
Interim After Launch’ | Launch | Launch Service | Government Repayment
Payment ; Service Payments Schedule —
No. aaa errs {0 ins ne CLIN ($) Percentage (%) of
left containing invoice Price) Cumulative Payments
submission dates. Offerors to insert addition Made to Date to be
Me
‘individual dollar amounts, | Returned to Government

Table C-1: Launch Service Payment Schedule

The Government reserves the right to extend or shorten the above payment schedule by plus or minus three
months (i.e., L-33M or L-27M) at no increase in contract value to accommodate mission specific
requirements.

In the event that a mission requires an integration period greater than L-30M plus 3 months, the Government
shall have the right to order the Extended Integration non-standard services at the prices and for the launch
vehicle configurations identified in Table B-10. The payment numbers for L-"X”M through launch shall be
adjusted as specified in the RLSP. The cumulative amount of the payments for the extended integration
periods (L-"X”M) combined with the L-30M payment shall not exceed 10% of the total launch service price
unless specified in the RLSP.

The Contracting Officer will either approve the final payment (Launch + 03M) within thirty (30) days after
feceipt of the Final Flight Report, (CDRL C4-13) or withhold the final payment in accordance with the
provisions of contract Section C, Clause 24.0, Mission Success Determination, Investigation, and Corrective
Actions.

The final payment (Launch. + 03M) shall not be made in event of partial mission success or failed mission
determination by the Government in accordance with contract Section C, Clause 24.0. In the event of a
partial mission success or failed mission, the final payment shail be forfeited by the Contractor and is not
recoupable. In the event of a failed mission determination, an additional 15% of the launch service price shall
be applied as a credit to another launch service or be returned to the Government if it cannot be applied to a
subsequent launch service at the Government's discretion. If funds are not credited or returned within thirty
(30) days of a failed mission determination, the funds shall be subject to interest penalties at the prevailing
U.S. Treasury interest rate established for Prompt Payment.

C-19



Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

(D

(i) All technical problems and design anomalies have been resolved without
compromising system performance, reliability and safety.

(ii) The detailed design will meet performance, functional requirements, and
schedule.

(iii) Software simulations and prototyping results do not present any potential
mission risks.

(iv) All key subsystem and/or component engineering analyses are complete.

(v) Integrated safety analysis identifying any remaining hazards and proposed
resolution.

(vi) Launch vehicle/payload compatibility test plans have been defined.
(vii) 90% mission unique drawings released.
Mission Specific System Acceptance Review (MSSAR)

The NLS Contractor shall conduct an MSSAR after the design, fabrication,
qualification testing and analysis is complete and shall incorporate any flight data
available as part of the launch service. The Contractor shall address all mission
specific items for the payload and mission requirements to verify qualification,
compliance, and systems-level compatibility using completed analyses, test,
inspection, and demonstrations results. The mission unique system acceptance
shall be subject to NASA's approval. NASA reserves the right to withhold approval
until all action items have been closed. As a minimum, the Contractor shall provide
verification of the following items at the MSSAR:

(i) Results of the mission specific acceptance reviews of the major suppliers or
major subsystems;

(ii) Design changes that occurred subsequent to MSCDR or changes as a result of
new flight data;

(iii) Summary of applicable component tests (test setups, test cases, results and
significant anomalies), analyses, margins, or similarity assessments. Included
in the summary is component qualification rationale (similarity, test, analysis)
for all affected components that are new, changed or subject to new
environments or functional requirements;

(iv) Qualification rationale for the system as a whole;

(v) Methodology and results of current analyses.

D1A-13


Section B NASA Launch Services II (NLS II)
SF 1449 Continuation Contract NNK10LB01B

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B-20


Section C NASA Launch Services II (NLS Il)
Contract Terms and Conditions Contract NNK10LB01B

(v) Claims for damages resulting from failure of the contractor to extend the
cross-waiver of liability to its subcontractors and related entities, pursuant to
paragraph (c)(2) of this clause; or

(vi) Claims by the Government arising out of or relating to a contractor's failure to
perform its obligations under this contract.

(5) Nothing in this clause shall be construed to create the basis for a claim or suit
where none would otherwise exist.

(6) This cross-waiver shall not be applicable when 49 U.S.C. Subtitle IX, Chapter
701 is applicable.

43.0 RE-DETERIMINATION OF RANGE AND LAUNCH SITE COSTS

C468


Section D NASA Launch Services II (NLS I!)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

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D1A-2


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-10
PAYLOAD/LAUNCH VEHICLE EMC, RF, AND EED COMPATIBILITY ANALYSIS

DESCRIPTION/PURPOSE:

This Electromagnetic Compatibility (EMC), Radio Frequency (RF), and EED compatibility
analysis documents the results of EMC/RF acceptance tests, demonstrates that design
requirements in the ICD are satisfied, and ensures that S/C and launch vehicle ordnance sub-
systems will not be unintentionally triggered by electromagnetic disturbances generated by the
S/C, launch vehicle, Range or other external sources. This is to ensure payload, launch
vehicle, and Range are compatible and that payload electromagnetic (EM) energy exposure
requirements will not be exceeded.

DATA REQUIREMENTS:
At a minimum, the following data items shall be delivered in approved electronic formats:

(A) An EMC Control Plan including EMC management processes, design guidelines, test
requirements and standards used by the launch vehicle program per fleet and as

changed.
(B) A Spacecraft/Launch Vehicle EM Compatibility Analysis which should include:
(i) Identification of test levels for S/C and launch vehicle susceptibility, intentional

and unintentional emissions.

(ii) Field strengths expected from known ground and external emitters.

(iii) | Calculation of EMI safety margins between S/C and launch vehicle hardware
susceptibility levels and S/C, launch vehicle and external emissions sources.

(C) ALLightning Effects Analysis detailing:

(i) The methods by which S/C and launch vehicle hardware will be protected from
direct and indirect lightning effects.

(ii) The operational procedures and retest criteria to be used during lightning events

(D) An RF Compatibility Analysis to ensure all communication systems will operate as
intended without fundamental or harmonic interference from other transmission systems
onboard or external to the vehicle stack.

(E) An EED Compatibility Analysis per fleet and as assessed/changed per mission
detailing:

(i) Identification of EED Sub-System components and wiring.

(ii) Identification of discrete EED trigger/firing circuits inclusive of circuit topologies,
component identification and circuit parameters.

(iii) Identification of potential failure modes on EED devices and command/control
circuits from electromagnetic sources.

(iv) Verification Analysis using CAE tools, Franklin analysis or other appropriate
method, demonstrate EEDs and all ordnance circuitry meet NASA and Range
requirements for EMI safety margins.

(v) Descriptive Contractor recommendations to mitigate any risks identified by this
analysis.

D2-42


Section B NASA Launch Services If (NLS I!)
SF 1449 Continuation Contract NNK10LB01B

1.7. NTE Prices - Standard Launch Services for IDIQ Missions

The Government shall have the right to order the standard launch services at the prices and
for the launch vehicle configurations identified in Table B-9. Nothing in this clause precludes
the Contractor from proposing more favorable prices or discount terms in response to specific
requests for launch service proposals in accordance with contract Section C, Clause 14.0.

LAUNCH NOT-TO-EXCEED PRICE ($)
VEHICLE IN CALENDAR YEAR ORDERED*
CONFIGURATION 2010 2011 2012 2013 2014 2015
Jul-Dec

Pegasus XL

2016 2017 2018 2019 2020

Pegasus XL TBP TBP TBP TBP TBP
TEP TBP TBP TBP TBP

TBP TBP TBP TBP TBP

TBP TBP TBP TBP TBP

{Tap TBP TBP TBP TBP

* The Contractor shall submit pricing for order years beyond 2015 not yet proposed, no later than the CY 2014
On-Ramp period. Pricing is based on the standard integration period of L-30 plus or minus 3 months.

Table B-9: NTE Price List - Standard Launch Services for IDIQ Missions

B-8


Section D NASA Launch Services II (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

3.0

4.0

41

failures and anomalies. This shall include insight into fleet-wide problems, anomalies,
MRB actions, deviations or waivers to systems, subsystems, materials, processes, and
test equipment including those used on non-NASA missions.

In the event of an anomaly or launch failure, the Contractor shall support NASA’s
Failure Review Board, if activated, or shall allow NASA to fully participate in the
Contractor's Failure Investigation Board including those for non-NASA missions.

NASA may elect to have representation as a resident office at the Contractor's major
manufacturing and engineering facilities for the life of the contract. The Contractor shall
provide accommodations and services, such as badging, furniture, telephones, and use
of easily accessible fax and copy machines from one to three residents and up to four
visitors at each location. A minimum of two voice and two data telephone lines shall be
provided. Electronic data transfer compatibility between the resident office and off-site
NASA institutions is required. A resident office will not be required at CCAFS or VAFB,
but NASA will require operational support accommodations (i.e. office space, power,
telephone, communication end instruments for monitoring vehicle testing, etc.) at the
launch complex during NASA launch operations.

NON-STANDARD SERVICES

The Contractor shall provide the non-standard services identified in Exhibit 3 as directed
by the Contracting Officer. Implementation of all non-standard services shall be fully
compliant with this SOW.

MISSION UNIQUE REQUIREMENTS

The Contractor shall provide the mission unique services identified in Exhibit 9 as
directed by the Contracting Officer. Implementation of all mission unique services shall
be fully compliant with this SOW.

Mission Unique Hardware

The Contractor shall design, manufacture, test, and qualify for flight the mission unique
hardware that is required to support the payload and mission. The Contractor shall
prepare and submit drawings (CDRL C5-4), test plans (CDRL C5-2), and test reports
(CDRL C5-3) to support NASA insight and approval of mission unique hardware.

For vehicle changes initiated by the Contractor that are not fleet-wide changes, the
Contractor shall prepare and submit a vehicle data package (CDRL C5-1).

The Contractor shall use MIL-STD-1540 B or C as a guideline when developing
environmental qualification and acceptance criteria and related test and analysis.
Factors of safety for mission unique hardware shall meet the requirements of Table
D1-B.

D1A-30


NASA Launch Services 1! (NLS II)
Section D: Documents, Exhibits and Attachments Contract NNK10LB01B

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D-2


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CONTRACT DATA REQUIREMENTS LIST (CDRL)

The Contract Data Requirements List (CDRL) identifies critical elements of the contracted
effort where NASA requires aspects of mission integration insight and approval. The following
CDRL defines the scope of documentation required; however, NASA will utilize the
Contractor's existing documentation to the extent practicable. Where there is not a direct
match between a CDRL item and the Contractor's standard documentation, the Contractor's
documentation will be acceptable provided it contains equivalent data requirements. CDRL
approval may be assumed unless the Contractor is notified by NASA of disapproval within
thirty (30) days. Under certain circumstances, NASA may elect to eliminate certain submittal
cycles

The number of copies listed in Table D2-A represents the number of hard copies to be
delivered to NASA only if the CDRL data is not available electronically, except CDRLs C1-1,
C1-2, C1-3, C5-4, and C5-5 which must also be delivered in hard copy. All electronic formats
shall be mutually acceptable. All data requirements shall be delivered to the KSC ELV Library.
The Contractor shall notify the Contracting Officer in writing of CDRL delivery.

Item Document Approval/ Initial Submittal Subsequent No. of
Review Date Submittal Date | Copies

C1: Documentation

IC1-1*  |Formal Meeting & Review Approval (B &| (A)(i) at AIR AIR
Documentation E(vi); Review | Review minus 1W;
all other

(A)(ii) at Review;

(B,C,D,E)
Review plus 1W
IC1-2* —|Countdown Documentation Approval L-1W As Changed 5
(A.B);
Review (C)
IC1-3* _ |Mission Console Notebook Review 24 hours prior to As Changed 100
Mission Dress
Rehearsal
iC 1-4 Manifest Policy Review Contract Award As Changed 5
IC1-5*  |Operations Documentation for Review AIR in CDRL As Changed 2

Processing in NASA Provided
Payload Processing Facilities

* Required per mission
TABLE D2-A: CDRL INDEX

D2-3


Section D

NASA Launch Services II (NLS II)

Attachment D1A; Pegasus Statement of Work (SOW) Contract NNK10LB01B

(D) Fairing Internal and Payload Adapter Surface Cleaning. The internal surfaces of

the payload fairing compartment (with the exception of the Pegasus avionics
section, Stage 3 motor, and Stage 2/3 interstage) and the Payload Adapter (with
the exception of the clampband, electrical harnesses, and the bolt cutters) shall be
cleaned, certified, and maintained to IEST-STD-CC1246D Level 750A or better,
with the number and locations of samples to be determined by the integration team.
Cleaning and certification shall be accomplished in a clean room rated at or above
Class 8 IAW 1SO14644-1. The Pegasus avionics section, Stage 3 motor, and Stage
2/3 interstage, all of which are located within the payload fairing compartment, shall
be cleaned to GC per JSC-SN-C-0005D. Sub-components of the Payload Adapter,
including the bolt cutters, clampband, and electrical harnesses, that cannot be
precision cleaned shall be cleaned to GC per JSC-SN-C-0005D. In lieu of IEST-
STD-CC1246D Level 750A, the payload fairing and Payload Adapter may be
cleaned and certified such that contribution from taunch vehicle sources measured
from S/C turnover (Launch Vehicle Contractor control of S/C for integrated
operations) through CCAM shall not exceed 1% total obscuration and 150
Angstroms molecular contamination. The sampling methodology for particulate
shall be per ASTM E1216 and for molecular per ASTM E1235. The number and
locations of samples to be determined by the integration team

Reserved

Clean Room Garments. Personnel garments used, at a contractor facility, in the
integration of the payload shall be provided and cleaned by the Contractor.
Personnel garments used in the integration of the payload shall comply with
accepted clean room and personnel safety operating standards as specified in the
mission specific contamination control plan

Materials. All materials used in areas in close proximity to the payload shall be
selected based on NASA RP-1124 (Rev-4). Materials shall have a Total Mass Loss
(TML) of less than 1.0% and Collected Volatile Condensable Materials (CVCM) of
less than 0.10%, or be expressly identified and submitted to NASA for approval.

2.4.2.4 Operational Support Services

The Contractor shall provide safety training, instruction, and certification for all
Contractor-operated or provided integration facilities and launch sites to ensure users
are aware of facility, launch site, launch vehicle and payload hazards and have
adequate knowledge to carry out their tasks unescorted in a safe manner. The
Contractor shall provide access for payload personnel to the payload/launch vehicle or
storage facilities to accommodate payload customer requirements. The Contractor shall
provide security to meet the requirements for payload or personnel protection. The
Contractor shall provide to NASA, upon request, launch service user's guide and facility
information (SDRL S1-1).

2.4.3. Range Support and Services

D1A-26


Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

2.2.1.2 Design Reviews — Mission Specific

The Contractor shall conduct and chair/co-chair design reviews, as described below,
that apply to the system, subsystem, component, and software level for all mission
specific items. Where there is not a direct match between a SOW specified mission
specific design review(s) and the Contractor's standard review(s), the Contractor's
review process will be acceptable provided it addresses equivalent content. All derived
requirements from all system requirements must be identified and addressed in each of
these reviews. NASA will approve the Mission Unique items in these reviews.

(A) Mission Specific Requirements Review (MSRR)

The Contractor shall conduct an MSRR prior to the Mission Specific Preliminary
Design Review (MSPDR) with NNC to review the mission specific design
requirements for the following items

(vi)

(vii)

(viii

(ix)

System requirements’ identification and definition to a level adequate to verify
launch vehicle performance capabilities.

Design restrictions, limitations, and known violations.

Physical and mechanical interfaces (e.g., payload to launch vehicle, payload
envelope, and access provisions)

Electrical interfaces (e.g., launch vehicle to payload, payload to umbilical,
interfaces with electrical ground support equipment, pad electrical systems,
ground batteries, telemetry, grounding, and power).

Functional interfaces (e.g., structures, structural loads, and vibration).
Avionics systems and interfaces (e.g., payload avionics interfaces with launch
vehicle, separation systems, telemetry interfaces, payload command and
telemetry, and RF)

Mass properties.

Environmental requirements (e.g., thermal, contamination, vibration, pressure,
Electromagnetic Compatibility (EMC), shock, launch complex RF, and
lightning).

Orbital requirements, launch vehicle performance, launch window injection
accuracy, and deployment attitudes and rates

Payload/Launch Vehicle separation requirements (e.g., separation conditions,
launch vehicle post-separation maneuver requirements, and telemetry).

D1A-11


Section D NASA Launch Services II (NLS II)
Exhibit 7: Launch Vehicle Certification Data Contract NNK10LB01B

EXHIBIT 7

LAUNCH VEHICLE CERTIFICATION DATA

E7-1


Section D NASA Launch Services II (NLS II)
Exhibit 8: Mission Interface Control Documents (ICD) Contract NNK10LB01B

This page left intentionally blank.


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

Officer. Once reviewed, the policy or policies may not be modified or canceled
without the prior, written approval of the Contracting Officer.

(C) The foregoing insurance requirement does not preclude the Contractor from

acquiring or continuing in effect any additional insurance to protect the interests of
the Contractor or its Related Parties.

32.4 Third Party Claims in Excess of Required Insurance

(A) NASA has determined that launches, under this contract, are conducted by NASA

in performance of its functions, as specified in 42 U.S.C. § 2473(a). As a result,
once the Contractor or its insurers have paid out for Third Party claims the amount
of required insurance under paragraph 32.3(B), NASA will consider any additional
Third Party claims for damage to or loss of property or personal injury or death
arising from the launches as claims against the United States under the authority of
42 U.S.C. § 2473(c)(13).

The Contractor (once it or its insurers have paid to Third Party claimants, from their
own funds, an amount equal to the amount of required insurance for a Launch)
shall adjust, settle and pay meritorious and reasonable additional Third Party claims
in excess of the amount of required insurance. To the extent NASA determines that
such costs exceed $25,000, it will forward such claim to the Secretary of Treasury
for certification and payment pursuant to 31 U.S.C. § 1304(a). Such costs are
subject to the availability of funds and the usual tests for allowability and the total of
such costs shall be paid up to a limit of $1.5 billion above the insurance obtained by
the Contractor for each launch.

In evaluating Third Party claims against the United States paid by the Contractor,
NASA will consider such a claim to be meritorious unless the claim represents:

(i) Liabilities for which the Contractor is otherwise responsible under the express
terms or conditions of the contract or a task order issued under this contract

(ii) Liabilities for which the Contractor has failed to insure or to maintain insurance
as required by the Contracting Officer

(iii) Liabilities for which the Contractor has not reasonably adjusted, settled, or
paid on a meritorious and reasonable basis.

(iv) Liabilities that result from willful misconduct or lack of good faith on the part of
any of the Contractor’s directors, officers, managers, superintendents, or other
representatives who have supervision or direction of:

(a) All or substantially all of the Contractor's business

C-51


Section C

NASA Launch Services II (NLS tl)

Contract Terms and Conditions Contract NNK10LB01B

29.4 NASA Secondary Payload on a Non-NASA Primary Payload

(A)

(B)

(C)

Procedures

NASA may request to manifest a NASA secondary payload on a non-NASA primary
mission via a task order requesting a proposal for a non-standard service to
accommodate a secondary payload. The Contracting Officer will provide a
description of the proposed secondary payload including, as a minimum: volume,
mass, attachment requirements, and data requested by the Contractor. The task
order will also identify any additional non-standard services or mission unique
requirements. If the Government is unable to provide the secondary payload for
launch vehicle integration or there is insufficient time to complete a new mission
analysis before the launch date, the Government will bear the cost and the
Contractor shall be responsible for designing, fabricating, and installing a secondary
payload mass simulator.

Upon receipt of the task order, the Contractor shall develop a proposal to
accommodate the secondary payload or provide a response that the Contractor
cannot accommodate the secondary payload on any existing planned missions.
The Contractor's proposal shall include a firm-fixed price for the secondary payload,
any additional non-standard services required, any mission unique services, and a
proposed payment schedule with accomplishment criteria. The Contractor shall
identify the primary mission and the target launch date for the mission. The
Contractor shall make all arrangements for and coordinate the concurrence of
manifesting the secondary payload with the primary mission customer.

The terms and conditions of this contract shall apply to NASA secondary payload
efforts, however the level of NASA insight and approval will be limited to those
activities directly affecting the secondary payload. The Contracting Officer shall
identify any additional reductions to the terms and conditions of the contract in each
task order for NASA secondary payload services.

In the event of termination for convenience of the NASA secondary payload
services, all costs associated with terminating such service shall be determined in
accordance with contract Section C, Clause 1.0(I), “Termination for the
Government's convenience.”

Delays

The Contractor shall incur no costs or damages associated with delaying the
secondary mission. The secondary mission shall not cause the primary mission
launch date to be delayed without Contractor approval. If the Contractor approves
a launch delay caused by the secondary payload, delay damages shall not apply.

Mission Success

C-47


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

(i) Payment.

(1) Items accepted. Payment shall be made for items accepted by the Government
that have been delivered to the delivery destinations set forth in this contract.

(2) Prompt Payment. The Government will make payment in accordance with the
Prompt Payment Act (31 U.S.C. 3903) and prompt payment regulations at 5 CFR
Part 1315

(3) Electronic Funds Transfer (EFT). If the Government makes payment by EFT, see
52.212-5(b) for the appropriate EFT clause.

(4) Discount. In connection with any discount offered for early payment, time shall be
computed from the date of the invoice. For the purpose of computing the
discount earned, payment shall be considered to have been made on the date
which appears on the payment check or the specified payment date if an
electronic funds transfer payment is made

(5) Overpayments. If the Contractor becomes aware of a duplicate contract financing
or invoice payment or that the Government has otherwise overpaid on a contract
financing or invoice payment, the Contractor shall—

(i) Remit the overpayment amount to the payment office cited in the contract along
with a description of the overpayment including the—

(A) Circumstances of the overpayment (e.g., duplicate payment, erroneous
payment, liquidation errors, date(s) of overpayment);

(B) Affected contract number and delivery order number, if applicable;
(C) Affected contract line item or subline item, if applicable; and
(D) Contractor point of contact.

(ii) Provide a copy of the remittance and supporting documentation to the
Contracting Officer.

(6) Interest.

(i) All amounts that become payable by the Contractor to the Government under
this contract shall bear simple interest from the date due until paid unless paid
within thirty (30) days of becoming due. The interest rate shall be the interest
rate established by the Secretary of the Treasury as provided in Section 611
of the Contract Disputes Act of 1978 (Public Law 95-563), which is applicable
to the period in which the amount becomes due, as provided in (i)(6)(v) of this
Clause, and then at the rate applicable for each six-month period as fixed by
the Secretary until the amount is paid.

Cc-9


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C5-5
INTEGRATED PROCEDURES
DESCRIPTION/PURPOSE:

Site procedures for various operations that involve the payload and/or the launch
vehicle/payload interfaces.

DATA REQUIREMENTS:

Provide as a minimum, the following integrated procedures (If applicable):
(A)  Payload/ launch vehicle electrical interface verification test
(B) | Payload encapsulation and transport

(C) | Payload/iaunch vehicle mate (includes payload adapter and vehicle mates, if
separate)

(D) — Launch vehicle electrical readiness/flight simulation
(E) Fairing installation
(F) | Combined system test/final readiness test

Also provide a list of all Contractor-specific procedures used for integrated processing with a
brief description of their purpose.

Integrated procedures shall have incorporated all mission specific requirements and must be
provided to NASA forty-five (45) days prior to use for coordination, review and comments.
Final, coordinated integrated procedures, ready for NASA approval, must be provided to NASA
1 week prior to use.

02-50


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

(B) Within thirty (30) calendar days from submittal of the Final Flight Report (CDRL C4-

13), the Contracting Officer will either determine the launch a Mission Success or
inform the Contractor of the Government's intent to withhold final mission success
payment(s) until a final determination of mission success is made.

In the event of a partial mission success or mission failure under paragraphs
24.1(B) or 24.1(C), the Contracting Officer will utilize all available data for the
mission, in particular the focus will be on the Final Flight Report (CDRL C4-13),
findings from the Contractor's investigation board, if activated, and findings from the
NASA review board(s) if activated. The Contracting Officer will provide a final
mission success determination within thirty (30) calendar days of the delivery of
final reports for all applicable review board(s)

24.4 Performance-Based Payment for Final Mission Success Determination

(A) In the event the Contracting Officer determines the launch service a Mission

Success, the Contractor shall receive full payment of the final payment event for the
launch service.

(B) In the event the Contracting Officer determines the launch service a Partial Mission

Success, the Government will pay no portion of the final payment in accordance
with Table C-8.

woe . % of Total Launch Service (CLIN)
9
Mission Success % of Cumulative Price Reallocated/Refunded to the
Determination Payments
Government
Full Success 100 0
Partial Mission Success 90 ie)
Failed Mission 90 15

Table C-8: Mission Success Payment Schedule’

‘The Government reserves the right to tailor the combined amount for mission failure
from 0% to 25% of the total launch service price in a Request for Launch Service
Proposal (RLSP).

(C) In the event the Contracting Officer determines the launch service a Failed Mission,

the Government will pay no portion of the final payment (reference Table C-8) and
the Contractor shall reallocate 15% of the total launch service (CLIN) price to
another NASA mission or refund the 15% if a subsequent launch service is
unavailable at the Government's discretion. Withholding of the final payment and
an additional 15% reallocation/refund to the Government are the sole remedies of
the Government for a Failed Mission determination.


Section D NASA Launch Services (NLS II)
Attachment D5: Safety and Health Plan Contract NNK10LB01B

This page left intentionally blank.

D5-2


Section C
Contract Terms and Conditions

NASA Launch Services II (NLS II)
Contract NNK10LB018

25.8

(L) Launch countdown procedures and deviations that affect spacecraft/vehicle

integrated assembly

(M) Anomaly resolutions that affect the integrated assembly.

(N) Launch Go/No-Go
(O) Reserved.

Specific areas to be open to Government insight are:

(A) Baseline vehicle design, analyses, models, and configuration management.

(B) Production program reviews, plans, and schedules.

(C) Production and systems test, and Material Review Boards.

(D) Critical flight hardware pedigree.

(E) Safety and Mission Assurance compliance evaluations (prime and subcontractors).

(F) Pre-ship reviews.

(G) Design and qualification reviews.

(H) Major/critical problems.

(1) Major system and integrated systems tests.

(J) Post-test data

(K) Anomaly resolutions.

(L) Failure analysis.

(M) Vehicle/ground support equipment procedures.

(N) Launch site support work schedules and plans.

(O) Launch site vehicle preparations and closeout data.

(P) Vehicle walkdown inspections.
(Q) Operations and procedure discipline.

(R) Work practices and documentation.

C-42


Section D NASA Launch Services II (NLS II)
Attachment D4: SB and SDB Subcontracting Plan Contract NNK10LB01B

SMALL BUSINESS (SB), VETERAN-OWNED SMALL BUSINESS (VOSB), HUBZone SMALL
BUSINESS (HUBZone SB), SMALL DISADVANTAGED BUSINESS (SDB) AND WOMEN-
OWNED SMALL BUSINESS (WOSB) SUBCONTRACTING MASTER PLAN

Goals, expressed in terms of percentages of total planned subcontracting dollars, for the use
of Small Business, Veteran-Owned Smail Business (includes Service Disabled Veteran-
Owned) Small Business, HUBZone Small Business, Small Disadvantaged Business, and
Women-Owned Small Business concerns as subcontractors shall be attached in the following
format to the Master Plan. Dollars include all subcontracts that contribute to contract
performance. Indirect costs are not included in establishing goals.

The Subcontract value of direct material have been proposed at an unburdened total of
$

Large Business Subcontract Dollars

Large Business Subcontract Percentage Goal

Small Business Subcontract Dollars*

Small Business Subcontract Percentage Goal*

Veteran-Owned Small Business Subcontract Dollars

Veteran-Owned Small Business Subcontract Percentage Goal

Service-Disabled VO Small Business Subcontract Dollars

Service-Disabled VO Small Business Subcontract Percentage Goal

HUBZone Small Business Subcontract Dollars

HUBZone Small Business Subcontract Percentage Goal

Small Disadvantaged Business Subcontract Dollars**

Small Disadvantaged Business Subcontract Percentage Goal**

Women-Owned Smail Business Subcontract Dollars

Women-Owned Small Business Subcontract Percentage Goal

*The Small Disadvantaged Business, Veteran-Owned Small Business, Service-Disabled Veteran-Owned Small
Business, HUBZone Small Business, Small Disadvantage Business, Women-Owned Small Business, HBCU's
and MI's dollars and percentages are rolled into the Small Business dollars and goals.

** HBCU's and MIs dollars (TBP) and percentages are rolled into the Small Disadvantaged Small Business
dollars and goals.

04-6


NASA Launch Services {I (NLS I!)
Section D: Documents, Exhibits and Attachments Contract NNK10LB01B

SECTION D

DOCUMENTS, EXHIBITS AND ATTACHMENTS

D-1


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

(G) Materials. All materials used in areas in close proximity to the payload shall be
selected based on NASA RP-1124 (Rev-4). Materials shall have a Total Mass Loss
(TML) of less than 1.0% and Collected Volatile Condensable Materials (CVCM) of
less than 0.10%, or be expressly identified and submitted to NASA for approval

2.4.2.4 Operational Support Services

2.4.3

The Contractor shall provide safety training, instruction, and certification for all
Contractor-operated or provided integration facilities and launch sites to ensure users
are aware of facility, launch site, launch vehicle and payload hazards and have
adequate knowledge to carry out their tasks unescorted in a safe manner. The
Contractor shall provide access for payload personnel to the payload/launch vehicle or
storage facilities to accommodate payload customer requirements. The Contractor shall
provide security to meet the requirements for payload or personnel protection. The
Contractor shall provide to NASA, upon request, launch service user's guide and facility
information (SDRL S1-1).

Range Support and Services

Launch vehicles provided under this contract shall include all hardware, software,
analysis and support necessary to meet the applicable Range Safety Requirements
(e.g., EWR-127-1, AFSPCMAN 91-710, or RSM-2002).

As part of the launch service, the Contractor shall make all launch Range support
arrangements for: scheduling Range for launch and integrated testing, Range Safety
functions, communications and timing, metric C-band beacon (radar) coverage,
telemetry coverage, camera coverage of launch, and tracking and telemetry station
acquisition predictions. If required, NASA will provide down range telemetry aircraft,
Tracking and Data Relay Satellite System (TDRSS) and/or NASA owned ground station
support for tracking and data recovery. The Contractor shall be responsible for
coordinating and ensuring all tracking and data recovery support meets mission
requirements (CDRL C2-3).

The Contractor shall make arrangements for Range provided services necessary to
support the launch service. As a minimum, the following services are to be provided:
fluids, gases, propellants, ordnance storage, facility usage, equipment support, shop
and laboratory services, meteorology, base security, fire protection and environmental
health. Payload-unique Range services will be provided as a mission-unique service.

The mission specific Program Requirements Document/Operational Requirements
(PRD/OR)(CDRL C2-2), or equivalent mission specific Range support documentation,
shall be submitted to obtain Range support. The Contractor, with support from NASA,
shall complete all forms pertinent to the mission and submit them to the appropriate
Range for formal acceptance.

D1B-27


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.4.1.2.1 Vehicle Telemetry

Telemetry data shall be archived in an industry standard format compatible with NASA's
LSP Data Center. All recordings shall include direct receiver video-out data when
available, as well as reshaped data waveforms when applicable for each designated
telemetry link. Archived data should include, if available, receiver signal strengths,
tracking antenna azimuth/elevation and IRIG-B Timing. All media shall be clearly
documented and labeled with the mission, date, record length and any and all channel
assignments and associated digital sample rates or clock rates per channel recorded

2.4.1.2.2 Baseline and Integrated Vehicle Support

The Contractor shail provide, in electronic form, all raw launch vehicle and GSE
telemetry (RF and hardwire) formats described in sufficient detail to allow NASA to
process and verify the data prior to initial launch vehicle power-up at the launch site.
This shall include a detailed listing and description of all measurements and calibration
coefficients for all launch vehicle and GSE telemetry (TM) links including the guidance
system and any embedded data streams. The Contractor shall provide to the NASA
LSP Data Center, via electronic format, any changes to the launch vehicle and/or GSE
telemetry format as the change is implemented to the launch vehicle and/or GSE
telemetry streams (CDRL C6-1).

The Contractor shall provide NASA with a compatible data recording (CDRL C6-2)
representative of the telemetry (RF and hardwire) signals of the launch vehicle and GSE
prior to the initial launch vehicle power-up test on each mission. This will allow NASA to
verify its ability to process the Contractor's telemetry (SDRL S6-1)

The Contractor shall submit an initial end-to-end launch vehicle telemetry path test plan
(SDRL S6-2) NLT 6 months prior to launch. This plan shall describe the telemetry links
from the launch vehicle through down range and deployable telemetry assets specific to
that mission. The plan shall identify and/or suggest orbiting or ground locations and/or
mobile assets to meet LSP telemetry coverage requirements. The Contractor shall
submit a final end-to-end launch vehicle telemetry path test plan NLT sixty (60) calendar
days prior to launch. The final plan shall verify the adequacy of telemetry link margins
with down range assets, and shall include link margin analysis and shall present data
flow diagrams between the NASA designated NASA LSP Data Center and downrange
assets.

The Contractor shall record all launch vehicle and GSE telemetry streams while the
vehicle is powered prior to launch. The Contractor shall provide real-time launch
vehicle and GSE telemetry (RF and/or hardline) data to the NASA designated LSP Data
Center for system level launch vehicle testing (system-level testing to include anytime
the vehicle or stage is powered and exercised, with data transmitted from the flight
telemetry system for the purpose of evaluating system health and function). Examples
include, but are not limited to, telemetry test data during initial vehicle power-up, flight

D1B-20


Section C NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B
22.0 RESERVED...... . bottetetterettereereee B68
23.0 USE OF GOVERNMENT PROPERTY, FACILITIES, AND ASSETS... 36
24.0 MISSION SUCCESS DETERMINATION, INVESTIGATION, AND

CORRECTIVE ACTIONS 36
25.0 GOVERNMENT INSIGHT AND APPROVAL.............:c0ccceeseseeeee 40
26.0 GOVERNMENT LAUNCH READINESS ASSESSMENT ......0...ccceerteenes 43
27.0 LICENSES AND PERMITS FOR A LAUNCH SERVICE OPERATOR ..............00:..43
28.0 ADVANCE UNDERSTANDING REGARDING TERMINATION

29.0
30.0
31.0
32.0
33.0

34.0

35.0
36.0
37.0
38.0
39.0

40.0

41.0

42.0

43.0
44.0

SETTLEMENT UNDER FAR 582.212-4(I)...
CO-MANIFESTED PAYLOADS.. : vote eeteeeetttestieceettrereee . -
EXPORT CONTROL AND FOREIGN NATIONALS. 0000... ccecceecececeeeeteereneteeeeeeees 48

DOMESTIC SOURCE CRITERIA... ee cse cere teesestestscetsteteretr teres AQ
LIABILITY FOR THIRD PARTY CLAIMS... settee AQ
FAR 52.212-3 OFFEROR REPRESENTATIONS AND CERTIFICATIONS--
COMMERCIAL ITEMS (AUG 2009) ALT | (APRIL 2002) .. boeteeeeeeee 52
FAR 52.212-5 CONTRACT TERMS AND CONDITIONS REQUIRED TO IMPLEMENT
STATUTES OR EXECUTIVE ORDERS--COMMERCIAL ITEMS (FEB 2010) ..............52
RESERVED 200.0... cccccccece cc cseceseeceseeseseseeeesesesensceeestsssetsenenseaeseenenees fees : 59
LISTING OF CLAUSES INCORPORATED BY REFERENCE 59
FAR 52.252-2 CLAUSES INCORPORATED BY REFERENCE (FEB 1998)................. 60
RESERVED 000.0... cece cece cee es ces eececeestescenseececsavacseevscsseessesrssscseerstietetiscevseereesenseets 60
SPECIAL UNDERSTANDING REGARDING DAMAGE TO

GOVERNMENT PAYLOADS.. cove 60
SPECIAL UNDERSTANDING REGARDING LIABILITY FOR THIRD PARTY

CLAIMS FOR NUCLEAR INCIDENTS... terete voter OT
DEPARTMENT OF ENERGY (DOE) 952.250-70 NUCLEAR HAZARDS

INDEMNITY AGREEMENT (JUN 1996) ...0.02..0c cece cee eecee ee ceeteeeeresteeeeeeeeees 61

1852.228-78 CROSS-WAIVER OF LIABILITY FOR SCIENCE OR SPACE
EXPLORATION ACTIVITIES UNRELATED TO THE INTERNATIONAL SPACE

STATION (DEVIATION) (OCT 2009)... cece eects fees +. 65
RE-DETERIMINATION OF RANGE AND LAUNCH SITE COSTS |W... cece 68
USE OF GOVERNMENT PRODUCTION, RESEARCH PROPERTY,

TOOLING, AND FACILITIES ON A NO-CHARGE BASIS ...0.0.0.0.0cccceeteeee TO

C4


Section D NASA Launch Services II (NLS II)

Attachment D10: Acronyms and Abbreviations Contract NNK10LB01B
D Day

DADS Dynamic Analysis and Design System
dB Decibel

dBm Decibel Millivolts

DD Day

deg Degree

DIG Designated Industry Group

DLA Declination of Launch Asymptote
DMR Detailed Mission Requirements

DoD Department Of Defense

DoDSSP DOD Single Stock Point

DOF Degrees of Freedom

DOS Department of State

DOT Department of Transportation

DPA Dual Payload Adapter

DPAF Dual Payload Attach Fitting

DPAS Defense Priority Allocation System
DUNS Data Universal Numbering System
E.O. Executive Order ’
EAR Export Administration Regulations
ECS Environmental Control System

EDU Engineering Demonstration Unit

EED Electro Explosive Device

EEE Electrical, Electronic and Electromechanical
EFT Electronic Funds Transfer

EGSE Electrical Ground Support Equipment
EICD Electrical Interface Control Document
ELS Equivalent Level of Safety

ELV Expendable Launch Vehicle

EMC Electromagnetic Compatibility

EM Electromagnetic

EO Engineering Order

ER Eastern Range

ERB Engineering Review Board

EWR Eastern/Western Range

F Fahrenheit

FAR Federal Acquisition Regulation
FED-STD Federal Standard

FEM Finite Element Model

FFP Firm-Fixed-Price

FMA Final Mission Analysis

FOIA Freedom of Information Act

FPMR Federal Procurement Material Record
FRB Flight Readiness Board

010-2


Section D NASA Launch Services Ii (NLS II)
Attachment 01B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.4.1.2.3, Launch Countdown and Flight Support

The Contractor shall provide launch countdown procedures, Mission Constraints
Documents (CDRL C1-2) and a Mission Console Notebook (CDRL C1-3) for the launch
dress rehearsal and launch in hard copy and a mutually agreed upon electronic format.

The Contractor shall provide up to eight NASA personnel access to consoles, with
vehicle monitoring capabilities, co-located within the Contractor’s launch control center.
The Contractor shall provide access to real-time telemetry (RF and hardwire), voice
communication channels with talk/listen capabilities, video and telephones for the co-
located NASA personnel. To the extent possible, the Contractor shall implement the
NASA provided console communications configuration for those consoles occupied by
the NASA team within the Contractor's launch control center. The Contractor shall
support validation of this configuration with the designated NASA LSP Data Center prior
to launch dress rehearsal and launch.

The Contractor shall deliver real-time launch vehicle and GSE telemetry (RF and
hardwire), voice communication channels and video to the designated NASA LSP Data
Center from the start of launch countdown through Range Loss of Signal (LOS) when in
range of an existing ground receiving station, or as supplemented as described in SOW
paragraph 2.4.3, Range Support and Services. If the launch vehicle telemetry, voice
communication channels or video is uniquely encoded, the Contractor shall provide the
decoded launch vehicle telemetry, voice communication channels, and video to the
NASA LSP Data Center.

The Contractor shall receive and record the raw launch vehicle telemetry data for all
phases of powered flight, from two (2) minutes prior to stage ignition through 10
seconds after payload separation IAW NASA Policy LSP-PD-120.05. NASA shall
provide any downrange telemetry assets required if the Range utilized is unable to
support with its existing ground assets.

The Contractor shall provide real-time transmission back to the NASA designated NASA
LSP Data Center of all mandatory receive and record launch vehicle telemetry coverage
times IAW NASA Policy LSP-PD-120.05. The Contractor shall provide the raw
telemetry data recorded post launch (SDRL S6-3).

During the Launch Countdown, the Contractor shall poll NASA at key milestone events
for GO/NO-GO status. The final poll shall include the NASA Launch Manager's
GO/NO-GO status for launch. The Contractor shall provide NASA access to anomalies
and concurrence with anomaly resolution prior to proceeding with Launch Countdown.
The Contractor shall poll NASA for any recycle of the Launch Countdown

On day of launch, the Contractor shall maintain voice contact with the downrange
assets and provide status/readiness to the launch team as requested.

D1B-22


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

In the event the secondary payload causes primary mission failure, the
primary mission shall be determined a full success for purposes of
contract Section C, paragraph 24.2

29.3. Non-NASA Payload with NASA Primary Payload

(A) Procedures

The Contractor may propose to manifest a non-NASA payload on a NASA primary
mission. The Contractor shall propose the mission requirements and consideration
to be received by NASA. The Contractor shall submit, at no cost to NASA, a
detailed payload description, a dual payload compatibility assessment, and any
additional documentation or analyses requested by NASA. NASA maintains the
tight to approve or disapprove the non-NASA payload proposed for manifesting on
a NASA primary mission. NASA will respond to the Contractor's request within sixty
(60) calendar days after receipt of all NASA requested documentation and
analyses.

If the Contractor is unable to provide the non-NASA payload for launch vehicle
integration or there is insufficient time to complete a new mission analysis before
the launch date, the Contractor shall bear the cost and be responsible for
designing, fabricating, and installing a secondary payload mass simulator.

Delays

NASA shall incur no costs or damages associated with delaying the non-NASA
mission under any circumstance. The non-NASA payload shall not cause the
NASA primary mission launch date to be delayed without NASA approval. If NASA
approves a launch delay caused by the non-NASA payload, the NASA Contracting
Officer will unilaterally determine whether the Government will be entitled to
equitable adjustment under contract Section C, Clause 19.0, Adjustments to
Launch Schedule.

Mission Success
Mission success determination for the NASA primary payload shall be made in
accordance with contract Section C, Clause 24.0, Mission Success Determination,
Investigation, and Corrective Actions with the following exception:

In the event the non-NASA payload causes primary mission failure, the

primary mission shall be determined a full success for purposes of
contract Section C, paragraph 24.2.

C-~46


Section B NASA Launch Services II (NLS I!)
SF 1449 Continuation Contract NNK10LB01B

SECTION B
STANDARD FORM 1449 CONTINUATION

4.0 SCHEDULE OF SUPPLIES AND/OR SERVICES TO BE PROVIDED
The Contractor shall provide all services, facilities, and resources (except as may be expressly
stated in this contract as furnished by the Government) necessary to furnish the Contract Line
Item Number (CLIN) items (Tables B-4 through B-10) in accordance with (IAW) the Statement
of Work (SOW), Exhibits, and Documents attached hereto.
1.1. Reserved

Table B-1: Reserved
1.2. Reserved

Table B-2: Reserved
1.3. Reserved

Table B-3: Reserved

1.4. Reserved

Table B-4: Reserved

1.5. Special Task Assignments (Studies and Analyses)

Table B-5: Special Task Assignments (Studies and Analyses)

B-5


Section D NASA Launch Services !I (NLS II)
Exhibit 4: Sample Certificate of Flight Readiness Contract NNK10LB01B

EXHIBIT 4
SAMPLE CERTIFICATE OF FLIGHT READINESS

FLIGHT CERTIFICATION DOCUMENT
FOR THE (TBD) MISSION

The following agencies certify that the necessary launch test operations to date have been
completed for the launch vehicle and payload. Pending satisfactory closure of in-line work and
any open items identified in the Launch Readiness Review, the launch vehicle, payload, and
all supporting systems are ready for the launch operation.

(Launch Service Contractor) Launch Services Program Chief Engineer
NASA / KSC

Chief Safety Officer Launch Services Program Manager

NASA NASA / KSC

S/C Project Manager Launch Services Program Launch Director

NASA / TBP Center NASA / KSC

The following Government agencies, involved in supporting this (TBD) mission, certify that all
applicable requirements to date have been met and that all Government support elements are
making final preparations to support this mission. Pending satisfactory closure of in-line work
to prepare for support of this mission and any open items identified in the Launch Readiness
Review, all Government support elements are ready for the launch operation. Furthermore,
pending satisfactory closure of in-line launch vehicle and observatory processing and any open
items identified in the Launch Readiness Review, the (TBD) Space Wing foresees no national
resource protection or Range Safety issues which would preclude launch.

(TBD) Space Wing

Date


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C2-1.1
INTERFACE CONTROL DOCUMENT (ICD)
DESCRIPTION/PURPOSE:

The ICD identifies and defines the functional and environmental interfaces, and performance
requirements of the payload, and payload GSE with the launch vehicle and associated
payload/launch processing facilities. Thirty (30) days prior to launch, the approved ICD shail
be incorporated into the contract via contract modification as Exhibit 8 to Attachment D1. Any
approved changes after its inclusion into the contract will be incorporated prior to mission
success determination

Preliminary ICD is the first CDRL release of the ICD and is expected to have several TBD’s
Baseline ICD is the next release of the CDRL and is expected to have very few TBD’s.

DATA REQUIREMENTS:

The number of interface requirement changes incorporated in each new revision and
subsequent release of the ICD shall not exceed ten (10) approved requirements changes

Where there is not a direct match between the specified ICD data requirements identified
below and the Contractor's standard ICD, the Contractor's standard ICD will be acceptable
provided it addresses equivalent content

1.0 INTRODUCTION
1.1 Purpose
1.2 Scope
1.3. Definitions
1.4 Interface Change Control
1.4.1. ICD Change Procedure
1.4.2 Interface Requirement Discrepancy
1.5 Requirement Traceability
1.6 Requirements Status
2.0 APPLICABLE DOCUMENTS
2.1 Government Documents
2.2 Contractor Documents
2.3 Other Documents
3.0 INTERFACE REQUIREMENTS
3.1 Structural /Mechanical Interfaces

D2-13


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-5
PAYLOAD FAIRING CLEARANCE ANALYSIS
DESCRIPTION/PURPOSE:

This analysis documents/demonstrates that sufficient clearance exists under dynamic
conditions is available to prevent payload damage from lift-off through payload fairing jettison.

DATA REQUIREMENTS:

The Payload Fairing Clearance Analysis shall include, as a minimum, the effects of:
(A) Thermal pre-load
(B) Disconnect forces
(C) Actuator forces

(D) Dynamic response

D2-36


Section D

Exhibit 2B: Taurus Standard Services

NASA Launch Services II (NLS II)
Contract NNK10LB01B

SOW
Para.

| Standard Service

Description

E2B-3



Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B.

(vi)

(ii)

(iii)

(iv)

(v)

(vi)

(vii)

(viii)

issue or defense shail be effective regardless of whether such issue or defense
may otherwise be deemed jurisdictional or relating to an element in the cause of
action. The waiver shall be judicially enforceable in accordance with its terms by
the claimant against the person indemnified.

The term extraordinary nuclear occurrence means an event that DOE has
determined to be an extraordinary nuclear occurrence as defined in the Act. A
determination of whether or not there has been an extraordinary nuclear
occurrence will be made in accordance with the procedures in 10 CFR Part 840

For the purposes of that determination, "offsite" as that term is used in 10 CFR
part 840 means away from "the contract location” which phrase means any DOE
facility, installation, or site at which contractual activity under this contract is
being carried on, and any contractor-owned or controlled facility, installation, or
site at which the contractor is engaged in the performance of contractual activity
under this contract.

The waivers set forth above:

Shall be effective regardless of whether such issue or defense may otherwise be
deemed jurisdictional or relating to an element in the cause of action;

Shall be judicially enforceable in accordance with its terms by the claimant
against the person indemnified;

Shall not preclude a defense based upon a failure to take reasonable steps to
mitigate damages;

Shall not apply to injury or damage to a claimant or to a claimant's property which
is intentionally sustained by the claimant or which results from a nuclear incident
intentionally and wrongfully caused by the claimant;

Shall not apply to injury to a claimant who is employed at the site of and in
connection with the activity where the extraordinary nuclear occurrence takes
place, if benefits therefore are either payable or required to be provided under
any workmen's compensation or occupational disease law;

Shail not apply to any claim resulting from a nuclear incident occurring outside
the United States;

Shall be effective only with respect to those obligations set forth in this clause
and in insurance policies, contracts or other proof of financial protection; and

Shall not apply to, or prejudice the prosecution or defense of, any claim or portion

of claim which is not within the protection afforded under (A) the limit of liability
provisions under subsection 170e. of the Act, and (B) the terms of this agreement

C-63


Section C NASA Launch Services II (NLS 1)
Contract Terms and Conditions Contract NNK10LB01B

5.6

5.7

5.8

year. In:the event the contractor completes a milestone ahead of the milestone
completion date, the contractor may submit a proper invoice and the Government will
consider on a case-by-case basis, the early payment of the milestone.

In the event launch service SubCLINs are terminated independently of standard launch
service CLINs, the parties mutually agree the same termination refund schedule
percentage(s) shall be used and applied against the price for the terminated SubCLINs.
Table C-1 milestone events shall apply to each IDIQ LSTO issued under this contract.

This paragraph will apply to any postponement declared by the Government or the
Contractor for any reason, including launch schedule adjustments and Contractor failure
to make substantial progress in accordance with launch service milestone events (as
determined by the Government under this clause). In the event of a launch schedule
adjustment by the Government or Contractor in accordance with contract Section C,
Clause 19.0, Adjustments to Launch Schedule, the payment schedule for the applicable
launch service CLINs and SubCLINs shall be postponed for the length of the delay, if
necessary, by the Government to correspond with the new launch date and the
milestone events in the attached Work Plan. The requirement to make substantial
progress in general conformance with the attached Work Plan, however, is not waived
for any postponed launch service. In the event of a launch schedule adjustment by the
Government or Contractor, the Government or Contractor shall be entitled to an
equitable adjustment as determined by the contract Section C, Clause 19.0,
Adjustments to Launch Schedule.

The Contractor agrees in the event of a termination of this contract pursuant to contract
Section C, Clause 28.0, Advance Understanding Regarding Termination Settlement
Under FAR Clause 52.212-4(I), the Government shall not be obligated in any event to
pay or reimburse the Contractor any amount in excess of the amount already obligated
to the contract. The Contractor shall not be obligated to continue performance of the
work beyond such point. The Government shall not be obligated in any event to pay or
reimburse the Contractor in excess of the amount obligated to the contract on a
quarterly basis, notwithstanding anything to the contrary in contract Section C, Clause
28.0, Advance Understanding Regarding Termination Settlement Under FAR 52.212-
4(!) and NFS 1852.232-77 Limitation of Funds (Fixed-Price Contract) (Mar 1989)


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

40.0 SPECIAL UNDERSTANDING REGARDING LIABILITY FOR THIRD PARTY CLAIMS
FOR NUCLEAR INCIDENTS

In the event that a launch service acquired under this contract carries a payload containing a
Radioisotope Thermoelectric Generator (RTG) or other nuclear materials for which third party
liability insurance is not commercially available, NASA will obtain from the Department of
Energy (DOE) the necessary agreement to provide to the Contractor indemnification against
third party claims pursuant to the Price Anderson Act, 42 U.S.C. §2210. Such agreement shall
be obtained, and the Launch Service Task Order (LSTO) for the subject launch service shall
be modified to reflect the Price Anderson Act indemnification prior to integration of the RTG or
other nuclear materials into the launch vehicle. The Contractor shall not be required to
integrate the RTG or other nuclear materials into the subject mission’s launch vehicle prior to
the time at which Price Anderson Act or other indemnification for the nuclear risk has been
obtained. Any delay by NASA in timely obtaining Price Anderson Act indemnification prior to
scheduled integration which results in a launch delay, shall constitute a Government-caused
delay under clause 19.0 of the Contract. Such a Government-caused delay to the subject
mission shall be subject to the contract's changes clause

41.0 DEPARTMENT OF ENERGY (DOE) 952.250-70 NUCLEAR HAZARDS INDEMNITY
AGREEMENT (JUN 1996)
(a) Authority. This clause is incorporated into this contract pursuant to the authority
contained in subsection 170d of the Atomic Energy Act of 1954, as amended
(hereinafter called the Act.)

(b) Definitions. The definitions set out in the Act shall apply to this clause.

(c) Financial protection. Except as hereafter permitted or required in writing by DOE,
the contractor will not be required to provide or maintain, and will not provide or
maintain at Government expense, any form of financial protection to cover public
liability, as described in paragraph (d)(2) below. DOE may, however, at any time
require in writing that the contractor provide and maintain financial protection of
such a type and in such amount as DOE shall determine to be appropriate to
cover such public liability, provided that the costs of such financial protection are
reimbursed to the contractor by DOE.

(d)(1) Indemnification. To the extent that the contractor and other persons indemnified
are not compensated by any financial protection permitted or required by DOE,
DOE will indemnify the contractor and other persons indemnified against (i)
claims for public liability as described in subparagraph (d)(2) of this clause; and
(ii) such legal costs of the contractor and other persons indemnified as are
approved by DOE, provided that DOE's liability, including such legal costs, shall
not exceed the amount set forth in section 170e.(1)(B) of the Act in the aggregate
for each nuclear incident or precautionary evacuation occurring within the United
States or $100 million in the aggregate for each nuclear incident occurring
outside the United States, irrespective of the number of persons indemnified in
connection with this contract.

C61


Section D NASA Launch Services I! (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

4.0

4.1

42

43

MISSION UNIQUE REQUIREMENTS

The Contractor shall provide the mission unique services identified in Exhibit 9 as
directed by the Contracting Officer. Implementation of all mission unique services shall
be fully compliant with this SOW.

Mission Unique Hardware

The Contractor shall design, manufacture, test, and qualify for flight the mission unique
hardware that is required to support the payload and mission. The Contractor shall
prepare and submit drawings (CDRL C5-4), test plans (CDRL C5-2), and test reports
(CDRL C5-3) to support NASA insight and approval of mission unique hardware.

For vehicle changes initiated by the Contractor that are not fleet-wide changes, the
Contractor shall prepare and submit a vehicle data package (CDRL C5-1)

The Contractor shall use MIL-STD-1540 B or C as a guideline when developing
environmental qualification and acceptance criteria and related test and analysis.
Factors of safety for mission unique hardware shall meet the requirements of Table D1-
B

Application Test Analysis (No Test)
Yield Ultimate Yield Ultimate
Non-Man Rated 1.10 1.25 1.60 2.0

Table D1-B: Mission Unique Hardware Factors of Safety
Mission Unique Software

The Contractor shall provide source code and mission constants’ listings (CDRL C4-11)
with appropriate requirement specifications to support NASA approval of mission unique
software. The Contractor shall prepare and submit a pre-flight control system and
stability analysis report (CDRL C4-6) for the vehicle and mission unique software used
for each mission.

Unanticipated Mission Unique Services

At the time of contract award, the Government may not have identified all mission
unique services required for each mission. As unanticipated mission unique services
are identified, the Contracting Officer will authorize the Contractor, in accordance with
FAR 52.243-1, Changes — Fixed Price Alt I, to perform these services. In performing
unanticipated mission unique services, the Contractor shall design the necessary
ground and flight hardware/software; conduct appropriate design reviews; and
manufacture, test and qualify for flight launch vehicle mission unique
hardware/software, i.e., other than that provided as a standard service (Exhibit 2) or
described in the non-standard services list (Exhibit 3).

D1B-31


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

[x

Pd

p<

bed

Ix

bx

(iii) Alternate Il (Oct 2001) of 52.219-9

(12) 52.219-14, Limitations on Subcontracting (Dec 1996) (15 U.S.C.
637(a)(14)).

(13) 52.219-16, Liquidated Damages—Subcontracting Plan (Jan 1999)(15
U.S.C. 637(d)(4)(F)(i))

(14)(i) 52.219-23, Notice of Price Evaluation Adjustment for Small
Disadvantaged Business Concerns (Oct 2008) (10 U.S.C. 2323) (if the offeror
elects to waive the adjustment, it shall so indicate in its offer)

(ii) Alternate | (June 2003) of 52.219-23.

(15) 52.219-25, Small Disadvantaged Business Participation Program-
Disadvantaged Status and Reporting (Apr 2008) (Pub. L. 103-355, section
7102, and 10 U.S.C. 2323)

(16) 52.219-26, Small Disadvantaged Business Participation Program-
Incentive Subcontracting (Oct 2000) (Pub. L. 103-355, section 7102, and 10
U.S.C. 2323)

(17) 52.219-27, Notice of Total Service-Disabled Veteran-Owned Small
Business Set-Aside (May 2004) (15 U.S.C. 657f)

(18) 52.219-28, Post Award Small Business Program Rerepresentation (April
2009) (15 U.S.C. 632(a)(2)).

(19) 52.222-3, Convict Labor (June 2003) (E.O. 11755)

(20) 52.222-19, Child Labor-Cooperation with Authorities and Remedies (Aug
2009) (E.O. 13126).

(21) 52.222-21, Prohibition of Segregated Facilities (Feb 1999).
(22) 52.222-26, Equal Opportunity (Mar 2007) (E.O. 11246).

(23) 52.222-35, Equal Opportunity for Special Disabled Veterans, Veterans of
the Vietnam Era, and Other Eligible Veterans (Sep 2006) (38 U.S.C. 4212).

(24) 52.222-36, Affirmative Action for Workers with Disabilities (Jun 1998) (29
U.S.C. 793).

(25) 52.222-37, Employment Reports on Special Disabled Veterans, Veterans

of the Vietnam Era, and Other Eligible Veterans (Sep 2006) (38 U.S.C.
4212)

C-54


Section C

NASA Launch Services II (NLS I!)

Contract Terms and Conditions Contract NNK10LB01B

()

(n)

Risk of loss. Risk of loss of or damage to Government property under this contract
will be governed by FAR clause 52.246-25 Limitation of Liability--Services (Feb
1997) and is hereby incorporated by reference under contract Section C, Clause
36.0.

Taxes. The contract price includes all applicable Federal, State, and local taxes
and duties

Termination for the Government's convenience. The Government reserves the right
to terminate this contract, or any part hereof, for its sole convenience subject to the
terms of this contract specified in contract Section C, Clause 28.0, Advance
Understanding Regarding Termination Settlement under FAR Clause 52.212-4(I)

Termination for Cause. The Government may terminate this contract, or any part
hereof, for cause in the event of any default by the Contractor, including failure to
meet launch dates, certify or maintain certified launch vehicles, or if the Contractor
fails to comply with any contract terms and conditions, or fails to provide the
Government, upon request, with adequate assurances of future performance. In
the event of Termination for Cause, the Government shall not be liable to the
Contractor for any amount for supplies or services not accepted, including all
launch service payments previously paid and all launch service payments
remaining to be paid, and the Contractor shall be liable to the Government for any
and all rights and remedies provided by law. If it is determined that the Government
improperly terminated this contract for default, such termination shall be deemed a
termination for convenience

Title. Unless otherwise specified in a Task Assignment, title to items furnished in
conjunction with services under this contract shall remain with the Contractor. In
accordance with 42 U.S.C. 2465d, NASA shall not take title to launch vehicles
under contracts for launch services.

Warranty. Unless otherwise specified in a Task Assignment, the Contractor makes
no warranty, express or implied, with respect to the services delivered or performed
hereunder.

Limitation of liability. Except as provided for in paragraphs (a) and (j) above, the
Contractor will not be liable to the Government for consequential damages resulting
from any defect or deficiencies in accepted items.

Other compliances. The Contractor shall comply with all applicable Federal, State
and local laws, executive orders, rules and regulations applicable to its performance
under this contract.

Compliance with laws unique to Government contracts. The Contractor agrees to

comply with 31 U.S.C. 1352 relating to limitations on the use of appropriated funds
to influence certain Federal contracts; 18 U.S.C. 431 relating to officials not to

C-11


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

proposal. Proposals will be due within thirty (30) calendar days from the date of the
RLSP unless stated otherwise. The Contractor shall submit one original and five
copies of the proposal to the Contracting Officer at the address specified in the
RLSP

LSTO Proposal. The proposed common launch vehicle configuration shall achieve
one successful flight prior to submission of a proposal in order to be considered for
LSTO award. The Contractor, when submitting its firm-fixed price proposal, shall
indicate the proposal is compliant with the contract terms, statement of work, and
the specific requirements contained in the RLSP.

Firm-fixed pricing for all proposals shall not exceed the prices contained in the
Schedule. The prices contained in the Schedule are prices, which can be adjusted
downward by the Contractor for the specific launch service being proposed. Any
Contractor proposed reduction will be applicable to the current proposal only and
will not be deemed as a permanent reduction of the prices contained in the
Schedule. Any mission unique modifications not priced in the non-standard
services must be separately identified and individually priced, and are not limited by
the unit price in the Schedule.

The proposed launch service price, including applicable priced non-standard
services and mission uniques shall be totaled for a single firm-fixed price for all
efforts required under the order for that launch service. The total firm fixed-price
shall be applied to the percentages in contract Section C, Clause 5.0, Launch
Service Payments, Milestone Events and Completion Criteria, for conversion to
dollar amounts for each payment event, and shall identify any consideration being
provided as a result of changes to the Mission Success risk posture, as applicable.
In addition, the Work Plan milestones shall be appropriately modified to add any
non-standard and/or mission unique services. The Launch Service Task Order
Mission Solutions shall be incorporated in Exhibit 9.

Mandatory LSTO Proposal Submission. Unless otherwise agreed to by the
Contracting Officer, it is mandatory for contract holders under multiple award NLS
contracts to respond via a Proposal or Request for Waiver to each order for launch
service requirements provided these requirements are identified in the schedule
and do not conflict with the contract ordering limitations. The response shall include
all common launch vehicle configurations that meet the requirements for a
particular launch service task order. In the event there arises legitimate reasons for
an awardee not to submit a proposal for a particular launch service task order (e.g.,
limited capacity to perform, excessive performance capability, lack of one
successful flight, or launch service is no longer viable), the Contracting Officer may
waive the requirement for proposal submission.

LSTO Proposal Evaluation/LSTO Selection Criteria. All LSTO proposals shall be
submitted by the date and time specified in the RLSP, or it will be treated as a late
proposal in accordance with FAR 52.215-1, Instructions to Offerors — Competitive
Acquisition. If this requirement is met, the Contracting Officer will consider the
following three factors prior to award of an LSTO:


Section D NASA Launch Services II (NLS II)
Exhibit 2A: Pegasus Standard Services Contract NNK10LB01B

This page left intentionally blank.

E2A-2


Section D NASA Launch Services I! (NLS II)

Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B
SDRL DESCRIPTION Number: S3-1
RESERVED


Section C NASA Launch Services II (NLS I)
Contract Terms and Conditions Contract NNK10LB01B

29.5

30.0

30.1

30.2

30.3

Mission success determination for the NASA secondary payload shall be made in
accordance with contract Section C, Clause 24.0, Mission Success Determination,
Investigation, and Corrective Actions with the following exception:

In the event the primary payload causes secondary mission failure, the
secondary mission shall be determined a full success for purposes of
contract Section C, paragraph 24.2.

Contractor Risk Determination for NASA Secondary Missions

Upon receipt of a task order, the Contractor shall, as part of NASA secondary payload
integration activities, perform a payload compatibility assessment for all manifested
NASA secondary payloads. The Contractor shall notify the Contracting Officer, in writing
if, in the Contractor's opinion, the NASA secondary payload would pose unacceptable
risk to the success of the primary mission. The notification shall provide detailed
substantiation of said risks.

In the event the Contractor, or the primary mission Customer, determines the risk is
unacceptable, the Contractor and the Contracting Officer will mutually agree to
terminate the task order or re-manifest the NASA secondary payload on another
mission. In the event the task order is terminated, NASA will only be liable for the cost
of the compatibility analysis and any other payments made to the Contractor shall be
repaid to the Government or reallocated to another mission.

EXPORT CONTROL AND FOREIGN NATIONALS

The Contractor shall comply with all U.S. export contro! laws and regulations, including
the International Traffic in Arms Regulations (ITAR), 22 CFR Parts 120-130, and the
Export Administration Regulations (EAR), 15 CFR Parts 730-744, in the performance of
this contract. The Contractor shall be responsible for obtaining export licenses, where
required

The Contractor shall be responsible for obtaining the required export licenses before
utilizing foreign nationals in the performance of this contract, including instances where
the work is to be performed at launch sites. NASA will be responsible for all ITAR
requirements for their foreign national customers, as applicable

The Contracting Officer, or designated representative, may authorize the Contractor to
export ITAR-controlled technical data pursuant to the exemption set forth in 22 CFR
125.4(b)(3) where an international agreement provides for the export of such data and
the data does not disclose the details of the design, development, production or
manufacture of any defense article.

C48


Section D NASA Launch Services II (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: S$1-3
PROGRAM MASTER SCHEDULE AND LAUNCH VEHICLE PLANNING MANIFEST
DESCRIPTION/PURPOSE:

The contractor shall develop and provide a Program Master Schedule to include sub-tier
schedules, production schedules, and launch operations schedules for each launch service. In
addition, a Launch Vehicle Planning Manifest shall be provided which forecasts launch
services for a period of no less than five (5) years. To the extent possible, each release should
be consistent with the overall Manifest Policy. The contractor shall address mitigation steps for
when these submittals are not consistent with the Manifest Policy.

DATA REQUIREMENTS:

Documentation shall be delivered in a mutually acceptable format.

D3-4


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

2.2

2.3

under the basic contract. The intent of the On-Ramp is to foster competition for future
requirements for launch services.

The minimum IDIQ On-Ramp qualification criteria are:

(A) The Launch Service Contractor (LSC) shall be a domestic LSC pursuant to Section
201 of Public Law 105-303, Commercial Space Act of 1998.

(B) The LSC must obtain an ISO 9001/2000 third party certification (ISO 9001/2008
third party certification after November 2010), from a registrar accredited by either
the International Registrar of Certified Auditors (IRCA) or the Registrar
Accreditation Board (RAB), for any corporation, corporate divisions, subsidiaries,
joint ventures, partner(s) and/or other business entity actually performing launch
vehicle manufacturing, management, payload/launch vehicle integration, testing
and launch.

The parties mutually agree that the original solicitation, as revised, shall remain open
during the life of this contract and that at any time the Government may award
additional contracts for IDIQ requirements. Each August during the life of this contract,
or at any other time established via synopsis, the Government, will accept proposals
from new launch service providers for IDIQ contracts and proposals from existing IDIQ
contractors for additional launch services. A special On-Ramp Period will be held no
later than 2014 to obtain pricing for order years beyond 2015, not yet proposed. If the
Government issues a solicitation notice, new launch service providers and current IDIQ
contractors will be allowed to submit proposals, within the notice's stated response time.

The minimum contract requirements (as revised), the technical acceptability standards,
evaluation factors, solicitation terms and conditions, price reasonableness, and basis for
award shall remain in full force and effect for each new proposal. Upon award of each
additional contract, the Government shall notify all present Contractors of the award,
and the new Contractor shall thenceforth be eligible to compete with all present
Contractors for the award of IDIQ task orders. A new launch vehicle orientation may be
requested by the Government when appropriate as referenced in Attachment D1,
Paragraph 2.2.5.

Expansion of Performance Capabilities

NASA reserves the right to consider, in the future, expansion of the performance
capabilities covered by the IDIQ portion of the NLS contract, by properly soliciting offers
from all interested sources capable of meeting the requirements in the expanded
performance capabilities


Section D NASA Launch Services || (NLS I)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.5.2

2.5.3

Reliability Program

The Contractor shall implement and maintain a Reliability Program with an overall
vehicle design reliability of no less than 95% at an 80% confidence factor. The
Contractor's program shall facilitate evaluation of the Contractor and subcontractor’s
programs to determine if the product meets the overall design reliability requirements
Overall vehicle reliability predictions shall be incrementally revised to reflect design
modifications.

Quality Assurance Program

The Contractor shall maintain a quality management system that is ISO 9001/2000 third
party certified (ISO 9001/2008 third party certification is required after November 2010).
The Registrar shall be accredited by either the International Registrar of Certified
Auditors (IRCA) or the Registrar Accreditation Board (RAB). In the event the Contractor
certification is revoked, NASA shall be notified within five (5) business days (CDRL
C3-3)

The Contractor shall maintain a Software Assurance Program using ISO 90003 as a
guideline

The Contractor shall accommodate NASA participation in Contractor and subcontractor
audits and ISO audits. NASA insight will consist of monitoring audits with the
Contractor's auditors and inspectors in order to provide understanding of the
Contractor's quality system and insight of their processes

The Contractor shall support NASA performance of ISO 2TM party audits, as required.
The audits will be performed IAW ISO 19011 requirements.

The Contractor shall provide a current Audit Plan and schedule for in-house and
subcontractor audits upon request from NASA (CDRL C3-4). The Contractor shall
provide a copy of both the Contractor performed internal Quality Audit Report and the
subcontractor/vendor Quality Audit Reports (CDRL C3-5).

The Contractor shall provide for NASA attendance at any flight hardware reviews the
Contractor performs at Contractor or subcontractor facilities. The Contractor shall make
available to NASA any build paper, test results, nonconformance reports, discrepancy
history, statistical process control, and failure analyses that are relevant to the reviews.

The Contractor shall provide NASA remote terminal access (via a secure HTTPS (FTP)
website updated daily) to the following existing quality assurance databases: Non-
Conformance Reports (NCs) and Cause/Corrective Actions (CCAs); Limited Life Item
list (released once prior to launch); As Designed As Built (ADAB) database (released
once prior to launch); Software Problem Report (SPR) database; and Orbital-generated
alerts (technical and sibling).

D1B-29


Section D NASA Launch Services II (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

(ii) Thermal environments specified not to exceed 72°C, + 2°C (161.6°F, + 3.6°F)
during ascent on any launch vehicle component inside the fairing with a view
factor to the payload, with the exception of the upper stage motor and fairing
wall which shall not exceed 177°C (351°F). Maximum thermal environments
shall be specified in the mission specific Interface Control Document (ICD)
(CDRL C2-1.1).

(iii), Thermal and/or acoustic blankets sealed or filtered such that venting of blanket
material debris does not contaminate the payload.

(E) Flight instrumentation, as specified in Exhibit 1, paragraph 9.0, Payload
Environment Instrumentation, to provide data adequate to support Section C,
paragraph 24.2, Mission Success Determination.

(F) Capability to spin payloads, when applicable, prior to deployment over a minimum
range of zero (0) to 355 degrees per second with an accuracy of +2 degrees per
second of the target rate.

(G) Post mission maneuvers:

(i) A Collision/Contamination Avoidance Maneuver (CCAM), when applicable,
following payload separation to minimize payload contamination and any
chance of re-contact with the separated payload

(ii) End of mission maneuvers after CCAM shall support the limiting of orbital
debris [AW mission requirements and vehicle capability

(H) Provisions for the prevention of static charging on umbilical connectors that may be
subjected to static charging from plasma heating or atmospheric particulate matter
(e.g., bleed resistors, dead facing, or connector covers)

(I) Decals of a NASA logo and mission patch in accordance with NASA provided
artwork. The size of the logo and patch shall be a maximum of 24 in. x 24 in. The
logo and mission patch installation shall be appropriately documented in the
mission Interface Control Document (ICD) (CDRL C2-1.1).

(J) Availability of a Test Payload Adapter (TPA), with appropriate mechanical interfaces
and payload separation system, to support payload integration and testing at
NASA/NASA Customer (NNC) facilities (within the continental United States) or
such other locations as defined by the ICD. At this facility, the Contractor shall
support, with necessary personnel and equipment, the following: a fit check of the
payload with the flight PA, two consecutive weeks of environmental testing with a
TPA (personnel support is limited to one installation and one removal of TPA), one
week of consecutive payload shock testing with a TPA, and sufficient pyrotechnics
for two shock test firings.

D1A-9



Section D NASA Launch Services II (NLS II)

Attachment D10: Acronyms and Abbreviations Contract NNK10LB01B
N/A Not Applicable

NASA National Aeronautics and Space Administration
NDE Nondestructive Examination

NEPA National Environmental Policy Act

NFS NASA FAR Supplement

NLS NASA Launch Services

NLT No Later Than

NM Nautical Miles

NNC NASA and NASA Customer(s)

No. Number

NPD NASA Policy Directive

NPR NASA Procedural Requirements

NSSC NASA Shared Services Center

NTE Not To Exceed

NVAFB North Vandenberg Air Force Base

NVR Nonvolatile Residue

OCA Orbital Carrier Aircraft

OD Operations Directive

OMB Office of Management and Budget

OME! Other Minority Educational Institutions

OR Operational Requirements

Orbital Orbital Sciences Corporation

ORCA Online Representations and Certifications Application
OSHA Occupational Safety & Health Administration
P/FR Problem/Failure Reporting

PA Payload Adapter

PAF Payload Attach Fitting

PCM Pulse Code Modulation

PD Policy Directive

PDU Pyro Driver Unit

PGAA Performance and Guidance Accuracy Analysis
PHSF Payload Handling and Storage Facility

PLA Payload Adapter

PLF Payload Fairing

POCC Payload Operation Control Center

PPC Procurement Placement Code

P-POD Poly-Picosatellite Orbital Deployer

PPE Personal Protection Equipment

PPF Payload Processing Facility

PRD Program Requirements Data

PSWG Payload Safety Working Group

Pub. L. Public Law

010-5


Section D NASA Launch Services II (NLS II)
Exhibit 3B: Taurus Non-Standard Services List Contract NNK10LB01B

EXHIBIT 3B

TAURUS NON-STANDARD SERVICES LIST

E3B-1


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

19.9

19.10

19.11

19.12

19.13

payments shifted by the amount (length) of the delay. For NASA delays only, the
Contractor may elect to receive payments as major program milestone events are
completed in lieu of the payment of postponement fees or the Contracting Officer may
approve the addition of a new milestone payment event at the time of postponement,
provided funding is available and obligated to the contract

NASA/Contractor will not be charged with postponement fees/liquidated damages when
the delay in delivery or performance arises solely out of causes beyond the control of
NASA/Contractor and not due to the fault or negligence of NASA/Contractor. Such
causes include, but are not limited to the following:

Delays resulting from Range Mission Rules and Range Launch
Requirements (Mandatory and Required Assets), acts of God, acts
(including delay or failure to act) of any Governmental authority (De Jure
or De Facto), wars (declared or undeclared), riots, revolution, hijacking,
fires, freight embargoes, sabotage, epidemics, strikes and interruptions of
essential services such as electricity, natural gases, fuels and water, or
any condition which jeopardizes the safety of the employees of the
Contractor, NASA, or its subcontractors; or a launch vehicle failure
investigation, provided NASA retains its original position in the order of the
queue sequence and that all data related to the failure investigation is
made available to NASA without restriction

Once a specific launch date and time have been established, they may be changed by
the cumulative amount of the grace period established above by NASA or the
Contractor without consideration to the other party if the mission requirements can be
met. The cumulative total of grace periods exercised by either NASA or the Contractor
shall not exceed 150 days for either party.

The amount of postponement fees shall be added to/subtracted from (as applicable) the
next milestone payment made pursuant to the contract Section C, Clause 5.0, Launch
Service Payments, Milestone Events and Completion Criteria. In addition, the delivery
schedule shall be adjusted to reflect the revised launch date.

In the event of an anomaly on any sub-orbital or orbital vehicle provided by the
Contractor that involves hardware or software directly applicable to this launch service,
NASA reserves the right to delay the launch service, until the next available launch
opportunity, without accruing damages or providing an equitable adjustment to the
Contractor until acceptable resolution of the anomaly.

This clause, including grace periods, shall not apply to missions with limited launch
periods. Requests for launch adjustments for missions with limited launch periods shall
be in accordance with the “Changes” clause of this contract. Contractor requests for
launch adjustments for missions with limited launch periods are subject to equitable
adjustment and require approval of NASA prior to implementation. If NASA approval is
granted, the Contractor shall be obligated to launch at the next opportunity capable of
meeting the mission’s scientific requirements, irrespective of other launch commitments
or customer's priorities.

C-35


Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B
3.0 NON-STANDARD SERVICES ooo. er etter eres DIA-30
4.0 MISSION UNIQUE REQUIREMENTS ......0.0.000 0002 DIA-30
41 Mission Unique Hardware......... .. D1A-30
4.2 Mission Unique Software............ . D1A-31
43 Unanticipated Mission Unique Services.......................... . D1IA-31
5.0 SPECIAL TASK ASSIGNMENTS... tects, DIA31
6.0 INFORMATION TECHNOLOGY SECURITY.......0..0...00000 0c DIA-31
7.0 GUIDELINE DOCUMENTS... ttre, DIA-32
8.0 RESERVED ooo. terete DIA-33

EXHIBIT 1A PEGASUS CAPABILITIES, SPECIFICATIONS AND ENVIRONMENTS

E1A.1 VEHICLE CONFIGURATION

E1A.2 PAYLOAD DELIVERY CAPABILITY

E1A.3 INSERTION ACCURACIES

E1A.4 PAYLOAD SEPARATION ATTITUDE ACCURACY AND RATES

E1A.5 PAYLOAD FAIRING (PLF)

E1A.6 MECHANICAL INTERFACE

E1A.7 ELECTRICAL INTERFACE

E1A.8 PAYLOAD ENVIRONMENT

E1A.9 PAYLOAD ENVIRONMENT INSTRUMENTATION

E1A.10 GENERIC SECONDARY PAYLOAD CHARACTERISTICS/INTERFACE

EXHIBIT 2A PEGASUS STANDARD LAUNCH SERVICES LIST

EXHIBIT 3A PEGASUS NON-STANDARD SERVICES LIST

EXHIBIT 4

EXHIBIT 5

EXHIBIT 6

EXHIBIT 7

EXHIBIT 8

EXHIBIT 9

SAMPLE CERTIFICATE OF FLIGHT READINESS
RESERVED

RESERVED

LAUNCH VEHICLE CERTIFICATION DATA

MISSION INTERFACE CONTROL DOCUMENTS (ICD)

LAUNCH SERVICE TASK ORDER MISSION SOLUTIONS

D1A-4


Section D NASA Launch Services II (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SORL DESCRIPTION Number: S6-4
DATA FLOW DIAGRAMS, SCHEDULES AND DOWN RANGE ASSET STATUS
DESCRIPTION/PURPOSE:

To provide data flow path diagrams, schedules and down range asset status allowing NASA to
verify status/readiness of critical assets and data flow planning/coordination.

DATA REQUIREMENTS:
Provide data flow path diagrams, schedules and down range asset status between the NASA

designated NASA LSP Data Center and down range assets NLT fifteen (15) calendar days
prior to launch and at the Flight Readiness Review

D3-15


Section D
Attachment D10: Acronyms and Abbreviations

NASA Launch Services II (NLS II)
Contract NNK10LB01B

QA Quality Assurance

QMS Quality Management System

RAB Registrar Accreditation Board
RAAN Right Ascension of Ascending Node
RCS Reaction Control System

REA Rocket Engine Assemblies

REM Reaction Engine Module

RF Radio Frequency

RFO Request For Order

RFP Request For Proposal

RFQ Request For Quote

RHC Right Hand Circular

RHU Radioisotope Heater Unit

RLSP Request for Launch Services Proposals
RP Reference Procedure

RTG Radioisotope Thermal Generator
RTS Reagan Test Site

RX Receive

S/R Shipping/Receiving

SB Smail Business

S/C Spacecraft

SCFM Standard Cubic Feet per Minute
SDB Small Disadvantaged Business
SDRL Supplemental Data Requirements List
SDVOSB Service-Disabled Small Business
sec Second

SF Standard Form

SIC Standard Industrial Classification
SIGI Space Integrated GPS/INS

SOW Statement of Work

SRM Solid Rocket Motor

SSA Source Selection Authority

STD Standard

SVAFB South Vandenberg Air Force Base
SW Southwest

Sync Synchronous

T Time (as referenced from launch)
TBD To Be Determined

TBP To Be Proposed

TDRSS Tracking and Data Relay Satellite System
TIC Target Industry Categories

TIM Technical Interchange Meeting
TIN Taxpayer Identification Number

D10-6


Section D NASA Launch Services II (NLS II)
Exhibit 5: Reserved Contract NNK10LB01B

EXHIBIT 5

RESERVED

Table D1-R: Reserved

Table D1-S: Reserved


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C3-3

!SO 9001/2000 CERTIFICATION CERTIFICATE (ISO 9001/2008 CERTIFICATION
CERTIFICATE AFTER NOVEMBER 2010)

DESCRIPTION/PURPOSE:

The certificate that is provided by the Registrar upon successful completion of ISO 9001/2000
certification (ISO 9001/2008 certification after November 2010).

DATA REQUIREMENTS:
After completion of ISO 9001/2000 3% party certification (ISO 9001/2008 3” party certification

after November 2010), a copy of the certificate shall be provided to NASA. Upon loss of
certification, NASA shall be notified within five (5) business days.

D2-27


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C2-1.2
INTERFACE CONTROL DOCUMENT (ICD) REQUIREMENTS VERIFICATION MATRIX
DESCRIPTION/PURPOSE:

A verification matrix will document and track all ICD requirements and methods by which they
will be verified and responsible organization. The verification matrix shall list the final
documentation of the verification approved by the cognizant LSC engineer.

DATA REQUIREMENTS:

The verification matrix shall be released no later than three (3) months after the Preliminary
ICD CDRL approval and shall be updated upon release of each ICD revision

Where there is not a direct match between the specified ICD Verification Matrix data
requirements identified below and the Contractor's standard ICD Verification Matrix, the
Contractor's standard ICD Verification Matrix will be acceptable provided it addresses
equivalent content:

ICD requirement language

ICD requirement paragraph number

Verification Method (Test, Inspection, Analysis, Demonstration)
Responsible Organization

Verification Plan

Verification Source

Notes/Comments

Status

D2-17


Section C NASA Launch Services 1! (NLS II)
Contract Terms and Conditions Contract NNK10LB01B,

X (1) 52.203-6, Restrictions on Subcontractor Sales to the Government (Sep
2006), with Alternate | (Oct 1995) (41 U.S.C. 253g and 10 U.S.C. 2402)

X = (2) 52.203-13, Contractor Code of Business Ethics and Conduct (Apr 2010)
(Pub. L. 110-252, Title VI, Chapter 1 (41 U.S.C. 251 note))

(3) 52.203-15, Whistleblower Protections under the American Recovery and
Reinvestment Act of 2009 (Mar 2009) (Section 1553 of Pub L. 111-5) (Applies
to contracts funded by the American Recovery and Reinvestment Act of
2009)

_ (4): 52.204-11, American Recovery and Reinvestment Act—Reporting
Requirements (Mar 2009) (Pub. L. 111-5)

(5) 52.219-3, Notice of Total HUBZone Set-Aside (Jan 1999) (15 U.S.C.
657a).

X (6) 52.219-4, Notice of Price Evaluation Preference for HUBZone Small
Business Concerns (Jul 2005) (if the offeror elects to waive the preference, it
shall so indicate in its offer) (15 U.S.C. 657a).

(7) [Reserved]

(8)(i) 52.219-6, Notice of Total Small Business Set-Aside (June 2003) (15
U.S.C. 644).

(ii) Alternate | (Oct 1995) of 52.219-6.
(iii) Alternate Il (Mar 2004) of 52.219-6.

(9)(i) 52.219-7, Notice of Partial Small Business Set-Aside (June 2003) (15
U.S.C. 644).

(ii) Alternate 1 (Oct 1995) of 52.219-7.
(iii) Alternate II (Mar 2004) of 52.219-7

X_ (10) 52.219-8, Utilization of Small Business Concerns (May 2004) (15 U.S.C.
637(d)(2) and (3)).

X  (11)(i) 52.219-9, Small Business Subcontracting Plan (Apr 2008) (15 U.S.C.
637(d)(4))

(ii) Alternate | (Oct 2001) of 52.219-9.

C-53


Section D NASA Launch Services II (NLS 11)
Attachment D9: Most Favored Customer Certification Plan Contract NNK10LB01B

This page left intentionally blank.

D9-2


Section D NASA Launch Services I! (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

1.0

1.1

1.2

PEGASUS STATEMENT OF WORK

INTRODUCTION
Scope

This Statement of Work (SOW) and all Exhibits and documents attached or referenced
herein define the Government's requirements for the Contractor to provide launch
services in support of NASA's Launch Services Program (LSP). Unless expressly stated
otherwise, Exhibits are supplemental to the SOW and do not replace requirements in
the SOW. The scope of this contract effort includes risk category 2 and 3 launch
services Capable of delivering, at a minimum, a 250kg payload to orbit at an altitude of
200 km and a launch inclination of 28.5°.

This SOW defines the overall launch service requirements for ‘NASA or NASA-
sponsored payloads’ (hereinafter referred to as ‘payloads’). The Contractor shall
perform all tasks necessary, consistent with the terms and conditions of this contract
and the SOW provisions identified herein, to safely and reliably launch payloads in
accordance with NASA-defined mission objectives. The Contractor shall support
advanced planning and perform analysis tasks as directed by the Contracting Officer.

It is the general contemplation of the parties to this contract that the Contractor shall
have a broad mission in performing launch service related functions for the Government
and designees. Therefore, the general scope of the contract covers any launch service
and launch service related activities arising from the SOW in support of earth and space
science exploration, and space station re-supply.

Objectives

The goal of the NASA Launch Services (NLS) contract is to provide the Agency with
domestic launch services that are safe, successful, reliable, and affordable. The launch
services will be provided at a fixed price. The contract will, to the maximum extent
practical, incorporate best commercial practices

The objectives of this contract are to:

e Ensure the safety of the public, as well as all personnel, hardware, and property
associated with the launch services.

e Provide affordable, accurate, and on-time delivery of NASA and/or NASA-sponsored
payloads to space on expendable launch vehicles.

« Provide a mechanism to incorporate new launch services, technology upgrades,

improved systems engineering processes, and advances in manufacturing
techniques.

D1A-5


Section D NASA Launch Services II (NLS 11)
Attachment D11: Definitions Contract NNK10LB01B

This page left intentionally blank.

011-4


Section D
Attachment

NASA Launch Services II (NLS I!)
01B: Taurus Statement of Work (SOW) Contract NNK10LB01B

Provide risk mitigation while utilizing commercial practices.

Provide flexible manifesting policy that recognizes the national priorities of NASA
missions.

Provide a capability to optimize cost, schedule, and performance to satisfy mission
objectives.

Provide for clear Government visibility into program schedule, technical
performance, and risk.

Foster competition and create opportunities for new, emerging launch service
providers.

Promote partnering among customers, launch service providers, and the LSP to
maximize flexibility and responsiveness to customers’ needs.

1.3. Compliance Documents

The Contractor shall comply with the requirements contained in the following

documents.

Document No. Revision Document Title

Applicable Range Safety (e.g., EWR-127-1, AFSPCMAN 91-710, RSM-

Requirements 2002)

ISO 9001/2000" 2000 International Organization of Standardization

AS9100 2009 Aerospace Quality Management System

KNPR 8715.3? KSC Safety Practices Procedural Requirements

LSP-PD-120.05 BASIC Launch Telemetry Requirements

NPR 8715.6° A NASA Procedural Requirements for Limiting
Orbital Debris

NASA-STD-8719.92 NASA Safety Standard for Lifting Devices and
Equipment

' ISO 9001/2008 is required after November 2010

The Contractor shall comply with the latest revisions of these documents. These documents apply to

NASA property, personnel, software, and processes performed in NASA-owned facilities.

this

NASA has the obligation to comply with this policy. The Contractor shall support NASA's compliance with

document.

D1B-6


Section D

Attachment D2: Contract Data Requirements List

CDRL DESCRIPTION

MISSION CONSOLE NOTEBOOK

DESCRIPTION/PURPOSE:

A mission console notebook to assist on-console users during pre-count, terminal count, and

plus count operations.

DATA REQUIREMENTS:

As a minimum, the notebook shall include:

(H)
(I)

(J)
(K)

Terminal or abbreviated countdown procedure
Flight sequence of events

Range, payload, launch vehicle mandatory items
Communication channel matrix

Down-range telemetry coverage plan

Launch window for all possible attempts

Launch decision flowchart

Control center seating

Call sign matrix

Protocol for calling holds

Day of launch winds plan

D2-10

NASA Launch Services II (NLS II)
Contract NNK10LB01B

Number: C1-3


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

(ii) Thermal environments of the upper stage motor (with a view factor to the
payload) shall not exceed 177°C (351°F). Maximum thermal environments
shall be specified in the mission specific Interface Control Document (ICD)
(CDRL C2-1.1).

(ili) Acoustic blankets sealed or filtered such that venting of blanket material debris
does not contaminate the payload

(E) Flight instrumentation, as specified in Exhibit 1, paragraph 9.0, Payload
Environment Instrumentation, to provide data adequate to support Section C,
paragraph 24.2, Mission Success Determination

(F) Capability to spin payloads, when applicable, prior to deployment over a minimum
range of zero (0) to 355 degrees per second with an accuracy of +2 degrees per
second of the target rate.

(G) Post mission maneuvers:

(i) A Collision/Contamination Avoidance Maneuver (CCAM), when applicable,
following payload separation to minimize payload contamination and any
chance of re-contact with the separated payload

(ii) End of mission maneuvers after CCAM shall support the limiting of orbital
debris IAW mission requirements and vehicle capability

(H) Provisions for the prevention of static charging on umbilical connectors that may be
subjected to static charging from plasma heating or atmospheric particulate matter
(e.g., bleed resistors, dead facing, or connector covers).

(l) Decals of a NASA logo and mission patch in accordance with NASA provided
artwork. The size of the logo shall be a maximum of 24 in. x 24 in. The size of the
mission patch shall be a maximum of 42 in. high and 36 in. wide (63” fairing) or 54
in. high and 60 in. wide (92” fairing). The logo and mission patch installation shall
be appropriately documented in the mission specific ICD (CDRL C2-1.1).

(J) Availability of a Test Payload Adapter (TPA), with appropriate mechanical interfaces
and payload separation system, to support payload integration and testing at
NASA/NASA Customer (NNC) facilities (within the continental United States) or
such other locations as defined by the ICD. At this facility, the Contractor shall
support, with necessary personnel and equipment, the following: a fit check of the
payload with the flight PA, two consecutive weeks of environmental testing with a
TPA (personnel support is limited to one installation and one removal of TPA), one
week of consecutive payload shock testing with a TPA, and sufficient pyrotechnics
for two shock test firings.

D1B-9


Section C NASA Launch Services II (NLS I)
Contract Terms and Conditions Contract NNK10LB01B

7.0

71

7.2

7.3

7.4

SECURITY FOR LAUNCH SERVICE PAYMENT FINANCING

Requirements for payment. Payments will be made under this contract upon
submission of properly certified invoices or vouchers by the Contractor, and approval by
the administering office, NASA John F. Kennedy Space Center. The amount of all
invoices or vouchers submitted shall not exceed the total contract price for all CLINs,
authorized LSTOs issued under the IDIQ contract, and special task assignments
(studies and analyses)

Security. Pursuant to FAR Subpart 32.202-4 Security for Government Financing and 10
U.S.C. 2307(f) and 41 U.S.C. 255(f), the Government is required to obtain adequate
security for Government financing. Adequate security for payments made under this
contract shall be required in the form of a preferred creditor's lien. The Contractor shall
grant the Government a preferred creditor's lien i.e., a first lien paramount to all other
liens against all work in process sufficient to recompense the Government for all monies
advanced under this contract should the Contractor's performance prove to be
materially unsatisfactory

Insurance. The Contractor represents and warrants that it maintains with responsible
insurance carriers (1) insurance on plant and equipment against fire and other hazards
to the extent similar properties are usually insured by others operating plants and
properties of similar character in the same general locality; (2) adequate insurance
against liability on account of damage to persons or property; and (3) adequate
insurance under all applicable workers’ compensation laws. The Contractor agrees
that, until work under this contract has been completed and all payments made under
this contract have been liquidated, it will maintain this insurance and furnish any
certificates with respect to its insurance that the administering office may require.

Representations and Warranties. The Contractor represents and warrants the
following:

(A) The balance sheet, the profit and loss statement, and any other supporting financial
statements furnished to the administering office fairly reflect the financial condition
of the Contractor at the date shown or the period covered, and there has been no
subsequent materially adverse change in the financial condition of the Contractor.

(B) No litigation or criminal or civil proceedings are presently pending or threatened
against the Contractor, which would jeopardize performance under this contract,
except as shown in the financial statements

(C) The Contractor has disclosed all contingent liabilities in the financial statements
furnished to the administering office.

(D) None of the terms in this clause conflict with the authority under which the

Contractor is doing business or with the provision of any existing indenture or
agreement of the Contractor.

C-22


Section D NASA Launch Services II (NLS Il)
Exhibit 2A: Pegasus Standard Services Contract NNK10LB01B

EXHIBIT 2A

PEGASUS STANDARD SERVICES

E2A-1


Section D NASA Launch Services II (NLS I!)
Exhibit 6: Reserved Contract NNK10LB01B

IDIQ 1 THROUGH 10 DATA SHEETS

RESERVED

E6-2


Section B NASA Launch Services II (NLS I!)
SF 1449 Continuation Contract NNK10LB01B

1.8. NTE Prices — Non-Standard Services for IDIQ Missions

The Government shall have the right to order the following non-standard services at the prices
and for the launch vehicle configurations identified in Table B-10. Nothing in this clause
precludes the Contractor from proposing more favorable prices or discount terms in response
to specific requests for launch service proposals in accordance with contract Section C,
Clause 14.0.


Section D NASA Launch Services II (NLS 11)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C2-5
MISSION SUCCESS CRITERIA & DETERMINATION METHODOLOGY
DESCRIPTION/PURPOSE:

This data item proposes the criteria and methodology to support the Contracting Officer's
determination of mission success.

DATA REQUIREMENTS:

(A) A list of proposed criteria to be used to determine the success of the mission
These criteria shall be based on applicable flight related ICD requirements.

(B) The Contractor's proposed methods, including required vehicle telemetry
measurements, ground observation, and analysis/reconstruction techniques, for
verifying that each proposed mission success criterion is satisfied. Allowances for
sensor measurement accuracy shall be explicitly identified and justified.

The following notes shall apply to success criteria subject to mission specific requirements:

NOTES:

1. Insertion and Non-insertion altitudes are referenced to WGS-84 Earth equatorial radius.

2. Environmental levels will be determined from the installed instrumentation and telemetry
from the launch vehicle.

3. In defining the orbital parameters, “insertion” occurs at the time of spacecraft
separation.

4. Loss of launch vehicle telemetry signal or failure of the launch vehicle instrumentation
during flight will not be factored into mission success.

5. In the event of inadvertent flight termination by the range, as determined by an anomaly
investigation board, no mission success criteria shall apply and full mission success
payment shall be made.

6. In the event of a mission peculiar environmental exceedance, no reduction to mission
success shall be made if the spacecraft operates successfully to meet the mission
objectives.

D2-21


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.4.2.2 Launch Site Payload Integration Support

The Contractor shall provide all services, equipment, and support required for the
integration and launch of each payload. Services shall include, as a minimum, the
following:

(A) Encapsulation of the payload complement at the PPF, for either flight or transport to
the launch complex, transport, mate with the launch vehicle and performance of
integrated checkout activities.

(B) Verification of the end-to-end functionality of the umbilical lines provided for payload
use

(C) Support for the installation and checkout of the payload GSE (provided by the
payload customer) at the launch site as defined in the Mission ICD, and payload
communication accommodations (ethernet and/or voice) from the pad to the PPF.
The Contractor shall also provide for a NASA console at the Contractor's launch
control center.

(D) Provision of the mountings for, and the installation of, the payload GSE (provided
by the payload customer) at the launch complex and/or remote sites

(E) Provisions for access to the payload for contingency off-loading of payload
propellants prior to the vehicle vertical erection operation in accordance with the
appropriate Range Safety requirements and appropriate payload procedures. Per
agreement with Vandenberg Range Safety, once the vehicle is vertical, a faulty
hazardous propellant system is allowed to leak until empty, with the site cleared of
all personnel.

(F) Provision for launch site services to meet payload requirements agreed to in the
Mission ICD such as: power, air conditioning, GN,/GHe purges, and contamination
control.

(G) Support of all activities required to de-mate and to return the payload to the
processing facility if necessary at any time before the mechanical mate of the
Encapsulated Cargo Element (ECE) to the launch vehicle. After ECE-to-vehicle
mechanical mate, payload de-mate activities can be performed as a mission-unique
service.

(H) Preparation of the procedures for integrated launch vehicle/payload operations for

NASA approval and incorporation of the payload procedures as appropriate (CDRL
C5-5).

D1B-24


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

5.0

6.0

7.0

SPECIAL TASK ASSIGNMENTS

The Contractor shall be required to perform special studies and analyses, provide
materials, or fabricate hardware in support of this contract. Each task will be initiated by
written direction from the NASA Contracting Officer. These tasks generally include
advance planning and feasibility studies in support of future contemplated missions;
analyses in support of change requirements to authorized missions; development,
fabrication, and test of hardware/software to support planning studies or special tests;
mission unique studies; material provision; and hardware fabrication in support of
potential missions prior to mission authorization.

INFORMATION TECHNOLOGY SECURITY

The contractor shall comply with NPR 2810.1A, NASA's Policy on the Security of
Information Technology for LSC IT hardware and/or software provided to NASA. New
IT hardware and/or software systems delivered to NASA shall be compliant prior to
authorization to process. The contractor shall develop, update and implement an IT
Security Plan compliant with NPR 2810.1A. NASA IT Security personnel will evaluate
the LSC IT hardware and/or software security and determine compliance prior to NASA
acceptance.

GUIDELINE DOCUMENTS

The following documents are to be used as guidelines to the extent specified in this SOW. Ifa
revision number or date is not specified, the latest revision of the documents shall be used as
guidelines to the extent specified in the SOW.

Document No Rev. Document Title

ISO 14644-1 Basic Clean rooms and associated controlled environments —

Part 1: classification of air cleanliness

ISO 14644-2 2000 Clean rooms and associated controlled environments —

Part 2: specifications for testing and monitoring to prove
continued compliance with ISO 14644-1-First Edition

IRIG-106-07 2007 Telemetry Standards

ISO 90003 2004 Software Engineering - Guidelines for the Application of
ISO 9001:2000 to Computer Software

ISO 19011 2002 Guidelines for Quality And/Or Environmental Management
Systems Auditing

MIL-STD-1553' B Digital Time Division Command/Response Multiplex Data
Bus

MIL-STD-1540 Borc Test Requirements for Launch, Upper-Stage, and Space
Vehicles

D1B-32


Section D NASA Launch Services II (NLS II)

Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B
SDRL DESCRIPTION Number: S3-2
RESERVED

D3-6


Section D NASA Launch Services I! (NLS Il)
Exhibit 1B: Taurus Capabilities, Specifications and Environments Contract NNK10LB01B

EXHIBIT 1B

TAURUS CAPABILITIES, SPECIFICATIONS AND ENVIRONMENTS

E1B-1


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

24.2

24.3

(iv) There is a violation of the criteria documented in Mission Success Criteria &
Determination Methodology (CDRL C2-5) and reported in Final Flight Report
(CDRL C4-13); however, there is no launch vehicle/service caused
degradation of the payload’s ability to perform its intended function as defined
in the Payload Program Level Requirements

(B) A mission will be determined a Partial Mission Success when there is a violation of
the criteria documented in Mission Success Criteria & Determination Methodology
(CDRL C2-5) and reported in Final Flight Report (CDRL C4-13) during launch/flight
which results in degradation of the payload’s ability to perform its intended function
as defined in the Payload Program Level Requirements.

(C) Amission will be determined a Failed Mission when the payload:
(i) Is destroyed during launch/flight, or
(ii) Cannot be separated from the launch vehicle, or

(iii) Experiences a violation of the criteria documented in Mission Success Criteria
& Determination Methodology (CDRL C2-5) and reported in Final Flight
Report (CDRL C4-13) during flight which results in degradation of the
payload’s ability to meet minimum success as defined in the Payload
Program Level Requirements

Mission Success Determination

(A) NASA will provide the Contractor the Payload Program Level Requirements that
establish payload mission success criteria.

(B) The Contractor shall be responsible for providing telemetry data confirming the
required orbit conditions and payload environments were met as documented in
Mission Success Criteria & Determination Methodology (CDRL C2-5) and reported
in Final Flight Report (CDRL C4-13). The Contractor shall measure and provide
telemetry data to the extent required by the SOW.

(C) The Contracting Officer has authority to determine whether a launched mission is a
Mission Success, Partial Mission Success, or a Failed Mission in accordance with
Section C, paragraph 24.1.

Procedures
(A) Not less than two (2) months prior to launch of a payload, NASA will provide the

Contractor the Payload Program Level Requirements that establish payload
mission success criteria.


Section D NASA Launch Services II (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: S3-4
SAFETY DATA PACKAGE
DESCRIPTION/PURPOSE:

This item covers the submission of system safety documentation required to be delivered to
the applicable Federal or Commercial Range Safety Organizations for launch vehicle
operations for NASA Missions under this contract. This includes, but is not limited to, United
States Air Force (USAF) Eastern/Western Ranges, Reagan Test Site, Kodiak Island Launch
Complex, and Wallops Flight Facility

DATA REQUIREMENTS:

Contactors performing launch vehicle operations for NASA under this contract shall make
available to NASA the launch processing site required system safety documentation for launch
vehicle systems and associated ground support equipment (e.g. Tailored Requirements,
MSPSP, Hazard Reports, Ground Operations Plan, Test Plans, Nondestructive Examination
(NDE) Test Plans). All Range required documentation shall also be available to NASA upon
request.

The contractor shall update the system safety documentation and any technical analyses as
necessary to keep the data current.

This shall also include all agreements, determinations, interpretations, waivers, deviations,

Equivalent Level of Safety (ELS), mishaps and close calls documented for the launch
processing site safety organization.

D3-8


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C3-2

MISHAP NOTIFICATION, INVESTIGATION AND MISHAP PREPAREDNESS, AND
CONTINGENCY PLAN

DESCRIPTION/PURPOSE:

To provide NASA with an understanding of the Contractor's processes notifying NASA of
mishaps, as well as how the Contractor plans to investigate and establish corrective action
plans for mishaps that occur while performing the work required in support of this SOW.
Contractor employee on NASA-owned property, custodian of NASA assets elsewhere to the
extent those assets are involved, or Contactors involved in payload to launch vehicle
integrating operations, shall report mishaps or close calls. Mishap Preparedness and
Contingency Plan (MPCP) describes the immediate actions required in response to a mishap.

DATA REQUIREMENT:

a. GENERAL:
Mishap reporting, investigation and corrective action requirements differ according to
whether the specific mishap occurs on NASA property or on Contractor property.
Mishaps occurring on third party property will be handled in the same manner as those
occurring on Contractor property.

a.1. MPCPs shall describe how the Contractor responds to mishaps described below. This
plan shall identify, by name, and responsibility all Contractor personnel with
responsibilities for mishap response, data impoundment, and hardware impoundment
(includes retrieval of mishap generated debris). It shall describe: impoundment
process, notification of NASA and other authorities, public release of information, and
debris collection process. Additionally, it shall describe special procedures for
emergency response and debris retrieval personnel and identify potential post mishap
hazards along with PPE and other hazard mitigation procedures. MSDSs shall be
made available to first responders if requested. The MPCP shall also contain a
description how the contractor interfaces with the NASA IRT and the process for
transferring impounded data and material to the investigation authority. A template
MPCP plan shall be delivered no later than six months prior to the first launch and will
be updated after each launch based on lessons learned. The mission unique MPCP
shall be delivered no later than one week prior to launch.

D2-23


Section D

NASA Launch Services II (NLS II)

Attachment D2: Contract Data Requirements List

Contract NNK10LB01B

CDRL DESCRIPTION

Number: C4-9 (cont)

(G) Descriptive contractor recommendations to mitigate any risks identified by this

[MISSION] [VEHICLE SYSTEM] LINK ANALYSIS
[LAUNCH DATE] [GROUND STATION] [ANTENNA]

LINK DATA

Vehicle Transmitter Power (Wy:

analysis.
8
RHC
7 LHC
VERT or HORIZ
6
5

Power Received Above Noise (JB)

Ground Antenna Location (HT, LAT. LON):
Vehicle Losses (dB): [TM}

Noise Bancwith (kHz): [TM]

Ground Station G/T (dB): [TM]

Vehicle Transmitter Frequency (MHz). [TM]
Bit Rate {kBits/Second): [TM}

Ground Station Loss (4B). [CRO]

Ground Antenna Gain (48): [CRO]
Vehicle Losses, CRD (dB): [CRD]

CRD Threshold (yV): [CRD]

Frequency (MHz): [CRO]

Uplink Frequency (MHz) [C-band]

Reply Frequency (MH2): [C-band]

Radar EIRP (d8m): [C-band]
Transponder Sensitivity (d8my: [C-band

Show Significant Events
‘Show Significant Events

Desired

200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200
Time from liftoff (sec)

Figure D2-1: Power -Vs- Plus Count Time

02-41


Section B

NASA Launch Services II (NLS I!)
SF 1449 Continuation Contract NNK10LB01B
LAUNCH 2010
VEHICLE Jubb. 2011 2012 2013 2014 2015
CONFIGURATION ul-Dec
i 7”
- 4
[2016 | 2017 [| 2018 | 2019 | 2020

Table B-9A: Quantity Discount Schedule

B-9


Section D NASA Launch Services II (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

ATTACHMENT D3
SUPPLEMENTAL DATA REQUIREMENTS LIST (SDRL)

The SDRL identifies the non-CDRL documents generated in the course of production,
integration, test, pre-launch, and launch activities that shall be provided to NASA. These items
shall be delivered to NASA upon request within ten (10) days. Exceptions shall be negotiated
on a case-by-case basis and shall not exceed sixty (60) days. Where there is not a direct
match between an SDRL item and the Contractor's standard documentation, the Contractor's
documentation will be acceptable provided it contains equivalent data requirements.

ITEM DESCRIPTION
$1: Documentation
S1-1 Launch Service User's Guide and Facility
Information
Mission Integration Meeting Documentation
S1-3 Program Master Schedule and Launch Vehicle

Planning Manifest

$3: Safety & Mission Assurance

IS3-1 Reserved
IS3-2 Reserved
IS3-3 As-Built Configuration List
IS3-4 Safety Data Package
S4: Analysis
S4-1 Mission Battery Budget Analysis
IS4-2 Reserved

S5: Engineering
S5-1 Vehicle Test Procedures

$6: Telemetry and Communications

S6-1 Telemetry Test Data

S6-2 End to End Link Test Plan

S6-3 Recorded Launch Vehicle and GSE Telemetry
(Test, Pre-Launch, Launch)

S6-4 Data Flow Diagrams, Schedules and Down

Range Asset Status

Table D3-A: SDRL Index


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

(iv) Product or service to be delivered
(v) Task order price

(vi) Completion/Delivery date

(vii) Reserved

(vill) Any other necessary information

15.0 PRESERVATION, PACKING, PACKAGING, AND MARKING FOR
DOCUMENTATION

Preservation, packing, packaging and marking for shipment of all items ordered hereunder
shall be in accordance with commercial practice and adequate to insure safe transportation,
acceptable by common carrier, and transportation at the most economical rate(s). The
Contractor shall place identical requirements on all subcontracts for items delivered to NASA.
16.0 FAR 52.246-11 HIGHER LEVEL CONTRACT QUALITY REQUIREMENT (FEB 1999)

The Contractor shall comply with the higher-level quality standard selected below.

Title Number Date Tailoring

X ISO 9001/2000 2000 Third Party Certification
Required (ISO 9001/2008
after November 2010)

xX Aerospace QMS AS9100 2009
RevC

17.0 INSPECTION SYSTEM RECORDS

The Contractor shall maintain records evidencing inspections in accordance with the
Inspection clauses of this contract for one year after delivery of all items and/or completion of
all services called for by the contract.

18.0 REQUIRED TIME OF DELIVERY FOR LAUNCH SERVICES

18.1 The Government requires launch service delivery to be made according to the schedule
provided in Table C-4.

Table C-2: Reserved
Table C-3: Reserved


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

1.0

1.1

1.2

TAURUS STATEMENT OF WORK

INTRODUCTION
Scope

This Statement of Work (SOW) and all Exhibits and documents attached or referenced
herein define the Government's requirements for the Contractor to provide launch
services in support of NASA's Launch Services Program (LSP). Unless expressly stated
otherwise, Exhibits are supplemental to the SOW and do not replace requirements in
the SOW. The scope of this contract effort includes risk category 2 and 3 launch
services capable of delivering, at a minimum, a 250kg payload to orbit at an altitude of
200 km and a launch inclination of 28.5°.

This SOW defines the overall launch service requirements for ‘NASA or NASA-
sponsored payloads’ (hereinafter referred to as ‘payloads’). The Contractor shall
perform all tasks necessary, consistent with the terms and conditions of this contract
and the SOW provisions identified herein, to safely and reliably launch payloads in
accordance with NASA-defined mission objectives. The Contractor shall support
advanced planning and perform analysis tasks as directed by the Contracting Officer.

It is the general contemplation of the parties to this contract that the Contractor shall
have a broad mission in performing launch service related functions for the Government
and designees. Therefore, the general scope of the contract covers any launch service
and launch service related activities arising from the SOW in support of earth and space
science exploration, and space station re-supply.

Objectives

The goal of the NASA Launch Services (NLS) contract is to provide the Agency with
domestic launch services that are safe, successful, reliable, and affordable. The launch
services will be provided at a fixed price. The contract will, to the maximum extent
practical, incorporate best commercial practices

The objectives of this contract are to:

e Ensure the safety of the public, as well as all personnel, hardware, and property
associated with the launch services

e Provide affordable, accurate, and on-time delivery of NASA and/or NASA-sponsored
payloads to space on expendable launch vehicles.

e Provide a mechanism to incorporate new launch services, technology upgrades,

improved systems engineering processes, and advances in manufacturing
techniques.

D1B-5


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C3-5
QMS AND SUPPLIER/VENDOR AUDIT/ASSESSMENT REPORT

DESCRIPTION/PURPOSE:

Audit/Assessment Report documenting the findings and _ corrective actions of
Audit/Assessments conducted. Reports will be used to monitor Quality Management System
and the Supplier Management/Procurement System

DATA REQUIREMENTS:

The report shall include the date and location of the audit/assessment, participating individuals,
purpose of the audit/fassessment, assessment duration, method of assessment (i.e.,

1S09001/2000 (ISO 9001/2008 after November 2010), AS9100, internal policies/procedures),
objective, findings, corrective action, discussions/comments, and conclusion.

D2-29


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

(ii) The Government may issue a demand for payment to the Contractor upon
finding a debt is due under the contract.

(ii) Final decisions. The Contracting Officer will issue a final decision as required
by 33.211 if—

(A)

(B)

(C)

The Contracting Officer and the Contractor are unable to reach
agreement on the existence or amount of a debt within thirty (30) days;

The Contractor fails to liquidate a debt previously demanded by the
Contracting Officer within the timeline specified in the demand for
payment unless the amounts were not repaid because the Contractor
has requested an installment payment agreement; or

The Contractor requests a deferment of collection on a debt previously
demanded by the Contracting Officer (see 32.607-2).

(iv) !f a demand for payment was previously issued for the debt, the demand for
payment included in the final decision shall identify the same due date as the
original demand for payment.

(v) Amounts shall be due at the earliest of the following dates:

(A)

(B)

The date fixed under this contract

The date of the first written demand for payment, including any demand
for payment resulting from a default termination

(vi) The interest charge shall be computed for the actual number of calendar days
involved beginning on the due date and ending on—

(A)

(B)

(C)

The date on which the designated office receives payment from the
Contractor;

The date of issuance of a Government check to the Contractor from
which an amount otherwise payable has been withheld as a credit
against the contract debt; or

The date on which an amount withheld and applied to the contract debt
would otherwise have become payable to the Contractor.

(vii) The interest charge made under this clause may be reduced under the
procedures prescribed in 32.608-2 of the Federal Acquisition Regulation in
effect on the date of this contract.


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

LIST OF TABLES

Table C-1: Launch Service Payment Schedule... eee eeen treet ececeeeneeees 19

Table C-2: Reserved 31
Table C-3: Reserved...... betes tenes vee 31
Table C-4: IDIQ LSTO Delivery Schedule oo... cece cececeeteeecseseeeeteettestereetente B2
Table C-5: Contractor Liquidated Damages and Grace Periods................ : cee OS
Table C-6: NASA Postponement Fees and Grace Periods 0.0.0.0... ccccececccceeeeceeereneees 34
Table C-7: RESOPVEM 20... ececcecesccececeeeeseecseetsereeserectereeeeseetetsteseseseeecetienienreatiteeees 36
Table C-8: Mission Success Payment Schedule .............0.0.cccccceeeeeeeeeteeeseeneeees 38

Table C-9: RESEPVED ooo. ec ee etree et eeeeetee
Table C-10: | Range Costs Included in LSTO Base Price.

C-5


Section B NASA Launch Services II (NLS II)

SF 1449 Continuation Contract NNK10LB01B
HOURLY LABOR FIRM FIXED-PRICE ($)
RATE IN CALENDAR YEAR ORDERED*
(COMPOSITE SKILL MIX 2010 2011 2012 2013 2014 2015 2016
AND BURDENED) _|_Jul-Dec Loo. .
Labor Rate | TBP
; |
2017 2018 2019 2020 2021 2022
TBP TBP TBP TBP TBP TBP

* The Contractor shall submit pricing for calendar years beyond 2015 not yet proposed, no later than the CY 2014 On-Ramp
period. The proposed fabor rates shall be negotiated using the applicable procedures of FAR Part 15 and incorporated herein.

Table B-6: Hourly Labor Rate - FFP List

Table B-7: Reserved

1.6. IDIQ Launch Service Task Order (LSTO)

The Government reserves the unilateral right to order launch services at any time from
contract award through the second quarter of CY 2020 in accordance with contract Section C,
Clause 14.0, Launch Service Task Ordering Procedures. These launch services are identified
in Tables B-9 and B-10 and described in Exhibits 2 and 3 to the Statement of Work. Launch
dates will be mutually agreed upon prior to issuance of an LSTO.

NTE prices for launch services for IDIQ missions will be part of the price evaluation and best
value selection for award of an IDIQ task order contract.

In no event shall the Government be obligated to pay for any launch service prior to Authority
To Proceed and obligation of funds for that launch service. The minimum order amount for
each NLS IDIQ contract awarded in accordance with Section C, Clause 2.0, On-Ramp and
Technology Insertion, is $20,000. The maximum potential quantity for this IDIQ contract
portion for all NLS contracts combined is seventy (70) Launch Service Task Orders and
associated non-standard services/mission unique services.

Once payment begins on a qualified standard launch service and NASA insight commences,
the Government reserves the right to approve any Contractor initiated substitution of the
launch vehicle or reallocation of launch vehicle hardware designated for a NASA mission
under this contract, in accordance with Section C, Clause 25.0, Government Insight and
Approval.


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.3
2.3.1

Mission Integration Services
Mission Integration Management

The Contractor shall be responsible for managing the mission integration of the payload
flight and ground systems with the launch vehicle and its associated GSE. In
accordance with this responsibility, the Contractor shall perform, as a minimum, the
following services:

(A) Provide a single point of contact with overall mission responsibility for each mission.
This single point of contact shall be responsible for coordinating support from all
technical disciplines and management during the integration process.

(B) Conduct mission integration meetings (kick-off, working group, technical
interchange) approximately quarterly from Mission Integration Start (L-30M) to
launch.

(C) Provide a co-chairperson along with NASA for all working groups and technical
interchange meetings. The Contractor co-chairperson shall be responsible for
preparing and distributing agendas, minutes and action item logs for each meeting
(SDRL S1-2). The Contractor shall maintain the action item database and ensure
closure of all actions

(D) Provide appropriate technical/engineering representation at payload preliminary
and critical design reviews.

(E) Plan, schedule, and manage mission analyses required to define and verify
compatibility of the payload with the interface requirements and environments
(reference Table D1-A, SOW paragraph 2.3.2)

(F) Track development status of and resolve issues associated with mission specific
hardware and software.

(G) Coordinate interface and support requirements for the mission

(H) Plan/coordinate mission specific flight operations.

(I) Manage integration activities at the launch site.

(J) Manage and coordinate the launch vehicle safety approval process.

(K) Prepare, maintain and implement a payload to launch vehicle ICD for each mission.
The ICD shall include all mission requirements including launch vehicle and launch
site interface definition and environments (including GSE). The ICD shall include
the payload to launch vehicle/launch site electrical and mechanical interface
drawings (CDRL C2-1.1). Thirty (30) days prior to launch, the approved ICD shall
be incorporated into the contract via contract modification as Exhibit 8 to
Attachment D1. Any approved changes after its inclusion into the contract will be
incorporated prior to mission success determination.

D1B-17


Section D NASA Launch Services II (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

26

The Contractor shall accommodate NASA participation in Contractor and subcontractor
audits and ISO audits. NASA insight will consist of monitoring audits with the
Contractor’s auditors and inspectors in order to provide understanding of the
Contractor's quality system and insight of their processes.

The Contractor shall support NASA performance of ISO 2TM party audits, as required.
The audits will be performed IAW ISO 19011 requirements.

The Contractor shall provide a current Audit Plan and schedule for in-house and
subcontractor audits upon request from NASA (CDRL C3-4). The Contractor shall
provide a copy of both the Contractor performed internal Quality Audit Report and the
subcontractor/vendor Quality Audit Reports (CDRL C3-5).

The Contractor shall provide for NASA attendance at any flight hardware reviews the
Contractor performs at Contractor or subcontractor facilities. The Contractor shall make
available to NASA any build paper, test results, nonconformance reports, discrepancy
history, statistical process control, and failure analyses that are relevant to the reviews.

The Contractor shall provide NASA remote terminal access (via a secure HTTPS (FTP)
website updated daily) to the following existing quality assurance databases: Non-
Conformance Reports (NCs) and Cause/Corrective Actions (CCAs); Limited Life Item
list (released once prior to launch); As Designed As Built (ADAB) database (released
once prior to launch); Software Problem Report (SPR) database; and Orbital-generated
alerts (technical and sibling)

The contractor shall provide NASA all anomaly resolutions that affect the integrated
payload/launch vehicle assembly, including both hardware and software. NASA will
approve all integrated payload/launch vehicle anomaly resolutions. The contractor shall
provide insight to Material Review Board (MRB) and failure reporting for all launch
vehicle nonconformances.

The Contractor shall participate in the Government/Industry Data Exchange Program
(GIDEP) and provide Alert System Documentation (CDRL C3-1).

NASA Insight and Approval

The Contractor shall comply with the Government's implementation of NPD 8610.23
and NPD 8610.24 as defined under Section C, Clause 25.0 and the SOW paragraph
2.2.1, Formal Reviews. As part of the standard launch service, the Contractor shall
provide the data, documentation, drawings, analytical models, and support services as
necessary to accommodate the requirements specified under contract Section C,
Clause 25.0, Government Insight and Approval.

The Contractor shall notify NASA of qualification or test anomalies involving similar

launch vehicles, systems, subassemblies and components. The Contractor shall make
available to NASA all problem reports or discrepancy reports on launch vehicle systems’

D1A-29



Section C NASA Launch Services II (NLS I!)
Contract Terms and Conditions Contract NNK10LB01B

36.2 NASA FAR SUPPLEMENT (48 CFR CHAPTER 18) CLAUSES

NFS 1852.215-84 Ombudsman (Oct 2003) James E. Hattaway, Jr. at
(321) 867-7246

NFS 1852.219-74 Use of Rural Area Small Businesses (Sep 1990)

NFS 1852.219-75 Small, Small Disadvantaged, and Women-Owned Small
Business Subcontracting Reporting (May 1999)

NFS 1852.219-76 NASA 8 Percent Goal (Jul 1997)

NFS 1852.223-70 Safety and Health (April 2002)

NFS 1852.223-75 Major Breach of Safety or Security (Feb 2002)

NFS 1852.225-70 Export Licenses (Feb 2000) Alternate | (Feb 2000)

NFS 1852.228-75 Minimum Insurance Coverage (Oct 1988)

NFS 1852.243-71 Shared Savings (Mar 1997)

36.3 KENNEDY SPACE CENTER STANDARD CLAUSES
KSC 52.204-96 Security Controls for KSC & CCAFS (Apr 2010)
37.0 FAR 52.252-2 CLAUSES INCORPORATED BY REFERENCE (FEB 1998)
This contract incorporates one or more clauses by reference, with the same force and effect as
if they were given in full text. Upon request, the Contracting Officer will make their full text

available. Also, the full text of a clause may be accessed electronically at this/these
address(es):

http://www. arnet.gov/far/ GSA FAR Homepage

http:/Awww.hq.nasa.gov/office/procurement/regs/nfstoc.htm NASA FAR Supplement
Homepage

http://procurement.ksc.nasa.gov/clauses.htm KSC Standard Unique Clauses

38.0 RESERVED

39.0 SPECIAL UNDERSTANDING REGARDING DAMAGE TO GOVERNMENT
PAYLOADS

Prior to intentional ignition of the launch vehicle on the launch pad, the Contractor shall not be
responsible for damage to the spacecraft while the spacecraft is under the control of the
Contractor, except when such damage is caused by the gross negligence, willful misconduct,
or lack of good faith by the Contractor. In the event the Contractor is determined to be
responsible for such damage, the Contractor shall reimburse the Government for the cost of
spacecraft repairs as well as any costs associated with launch delays as set forth in Section C,
Clause 19.0, entitled “Adjustments to Launch Schedule.” After intentional ignition, the
provisions of Contract Section C, clause 24.0 shall apply.

C60


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION : Number: C3-1
ALERT SYSTEM DOCUMENTATION
DESCRIPTION/PURPOSE:

A Government Industries Data Exchange Program (GIDEP) Alert Report will be generated for
matches of all hardware covered by this contract.

DATA REQUIREMENTS:
(A) _ This report will identify all matches of hardware provided under this contract:

(B) The report shall identify the GIDEP Alert number, flight hardware impacted,
analysis of the problem, and any corrective action required.

(C) The report shall include results from any subcontractor GIDEP Alert reviews.

D2-22


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

2.4

2.5

3.0

3.1

3.2

Additional Launch Services Requirements

A) Prior to proposal submittal for a Launch Services Task Order (LSTO), the proposed
launch vehicle must have one successful flight, as established in contract Section C,
Clause 14.0, Launch Service Task Ordering Procedures.

B) Launch vehicles will be certified based on the requirements established by NPD
8610.7, ELV Risk Mitigation Policy for NASA-Owned and NASA-Sponsored
Payloads, and contract Section C, Clause 3.0, Launch Vehicle Certification, prior to
launch of a NASA mission

C) Launch services must comply with all the conditions and requirements of contract
Attachment D1, Statement of Work (SOW).

The minimum order amount for IDIQ contracts awarded in accordance with this On-
Ramp Clause is $20,000

LAUNCH VEHICLE CERTIFICATION

Any common launch vehicle configuration utilized by the Contractor to provide launch
services under this contract must be certified by NASA in accordance with NPD 8610.7,
ELV Risk Mitigation Policy for NASA-Owned or NASA-Sponsored Payloads. Common
launch vehicle configuration certification will be performed in accordance with LSP-PLN-
324.01, Expendable Launch Vehicle Certification.

Certification Criteria:

(A) Reserved

(B) Reserved

(C) For contract award of IDIQ launch services, the Contractor must provide a detailed,
viable plan, subject to Government assessment and acceptance, to achieve all
certification requirements prior to launch. If a certification plan (Attachment D1,

Exhibit 7) is submitted, it shall be exempt from disclosure as provided under the
FOIA.

ic)

Services under this contract will only include launch vehicles certified to risk
mitigation Category 2 and 3 in accordance with NPD 8610.7. The Contractor shall
submit all required documentation for NASA evaluation and determination of
certification category. NASA shall not bear any cost associated with the
development of any LSC documentation required for the certification of a common
launch vehicle configuration.

(E) The proposed common launch vehicle configuration shall achieve one successful
flight prior to submittal of a proposal for a Launch Service Task Order (LSTO).

C-15


Section D NASA Launch Services II (NLS II)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.5

2.5.1

Safety, Reliability, and Quality Assurance

During the period of performance the Contractor shall establish, implement, and
maintain comprehensive safety and health, reliability and quality assurance programs
covering program management, mission integration management, and the design,
development, production, test, integration and launch of the LVS

Safety and Health Program

The Contractor shall provide a Safety and Health Pian that will implement safety and
health requirements consistent with federal, state, and local government regulations and
applicable launch processing site Safety and Health requirements. This Plan shall
describe the Safety organization including structure of management interfaces and also
system safety methods employed to ensure compliance with applicable launch
processing site safety requirements.

The Contractor shall implement a system safety program to identify hazards of
systems/subsystems and impose applicable design requirements and management
controls to prevent mishaps. The Contractor shall develop system safety
documentation, plans, procedures, technical analyses, etc., IAW safety requirements of
the applicable launch processing site. For launches at the Eastern Range or Western
Range, any previously approved agreements between the contractor and the Range for
a tailored EWR 127-1 are acceptable to NASA. Likewise, any previous Range Safety
Agreements between the Contractor and WFF are acceptable to NASA. In accordance
with Section C, Clause 25.0 of the contract, the Contractor shall provide NASA with
insight and approval into future tailoring of Range Safety Requirements for launch
vehicle systems and operations. Launch processing site safety required documentation
shall be made available to NASA (SDRL S3-4) upon request. The Contractor shall
participate in all safety working groups (i.e. payload safety working group (PSWG), etc.)
as the launch vehicle safety representative for each NASA mission under this contract.

When the contractor is performing work in any NASA owned facility (e.g., buildings 836
and SLC-2W at VAFB and PHSF at KSC), all NASA requirements and safety
documentation as contained in the SOW, paragraph 1.3, Compliance Documents, shall
be adhered to. The Contractor shall submit system safety documentation (baseline and
any changes) to NASA for review/approval [AW CDRL C3-7 for processing at all NASA
provided facilities. NASA will review the safety documentation to ensure designs,
processing and operations do not pose an unacceptable safety risk to NASA
personnel/contractors, resources or risk to Mission Success.

The Contractor shall report Close Calls/Mishaps to NASA IAW CDRL C3-2. The

Contractor shall make provisions for NASA safety representative insight into integrated
Payload/launch vehicle processing.

D1B-28


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

This page left intentionally blank.

D2-54


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B.

SECTION C

CONTRACT TERMS AND CONDITIONS

C-1


Section D

NASA Launch Services II (NLS II)

Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

encapsulation. During the transition from the PPF to launch site, one momentary
interruption in air conditioning does occur. Conditioned air filtration shall be capable
of removing 99.97% of all particles greater than 0.3 microns and removing 95% of
all hydrocarbons with a molecular weight greater than 70. GNp2 shall be Grade B,
Type 1, (or better) IAW MIL-PRF-27401F. Transportation GN2 purging or
conditioned air shall not impinge directly on the payload at any point.

Fairing Environment. Following fairing installation and payload mate to the launch
vehicle, the PLF environment (as measured at a sensor located inside the fairing
volume immediately upstream of the payload cone air exit hole) shall be purged
with conditioned filtered air and shall maintain a temperature set point range,
selectable by the payload, of 13 to 23°C (55 to 73°F), controllable to +/- 3.3°C (5°F),
through T-0. Relative humidity shall be maintained within 30% to 50%. Relative
humidity will be controlled to preclude condensation within the fairing. Note that
since Taurus cannot control the lower humidity limit, conditions <30% may occur
after payload encapsulation. During the transition from the PPF to launch site, one
momentary interruption in air conditioning does occur. Conditioned air filtration
shall be capable of removing 99.97% of all particles greater than 0.3 microns and
removing 95% of all hydrocarbons with a molecular weight greater than 70. After
the fairing has been closed out for flight, Grade B, Type 1, GN2 (or better) IAW MIL-
PRF-27401F, may be used for purging the fairing environment. Fairing GNz
purging or conditioning air shall not impinge directly on the payload at any point.

Fairing Internal and Payload Adapter Surface Cleaning. The internal surfaces of
the payload fairing compartment (with the exception of the payload separation
system) shall be cleaned, certified, and maintained to IEST-STD-CC1246D Level
750A or better, with the number and locations of samples to be determined by the
integration team. Cleaning and certification shall be accomplished in a clean room
rated at or above Class 8 IAW 1ISO14644-1. The complexity of the separation
system (payload adapter) prevents its cleaning to Level 750A; therefore, this
assembly is cleaned to VC-HS +UV per JSC-SN-C-0005D. In lieu of IEST-STD-
CC1246D Level 750A, the payload fairing compartment (including Payload Adapter)
may be cleaned and certified such that contribution from launch vehicle sources
measured from S/C turnover (Launch Vehicle Contractor control of S/C for
integrated operations) through CCAM shall not exceed 1% total obscuration and
150 Angstroms molecular contamination. The sampling methodology for particulate
shall be per ASTM E1216 and for molecular per ASTM E1235. The number and
locations of samples to be determined by the integration team.

Reserved

Clean Room Garments. Personnel garments used, at a contractor facility, in the
integration of the payload shall be provided and cleaned by the Contractor.
Personnel garments used in the integration of the payload shall comply with
accepted clean room and personnel safety operating standards as specified in the
mission specific contamination control plan.

D1B-26


Section D NASA Launch Services II (NLS II)
Exhibit 9: LSTO Mission Solutions Contract NNK10LB01B

EXHIBIT 9
LAUNCH SERVICE TASK ORDER MISSION SOLUTIONS

Launch service task order mission solutions will be attached to the contract upon award of task
order(s)

TBD


Section C NASA Launch Services II (NLS I!)
Contract Terms and Conditions Contract NNK10LB01B

5.9 The Contracting Officer will unilaterally determine the Contractor's accomplishment and
successful completion of each milestone event. The Contracting Officer's determination of
milestone event completion will include, but is not limited to, the accomplishment criteria listed
for the major milestone events set forth in Attachment D8, Work Plan. In addition, the
Contracting Officer will determine if the following are complete for each payment requested: all
Contract Data Requirements List (CDRL) data item deliverables for which delivery is required
prior to the requested payment and all previous events have been met. Approval of the final
payment will be made in accordance with contract Section C, Clause 24.0, Mission Success
Determination, Investigation, and Corrective Actions.

6.0 NFS 1852.232-77 LIMITATION OF FUNDS (FIXED-PRICE CONTRACT) (MAR 1989)

(a) Of the total price of CLINs [TBD] through [TBD], the sum of $TBD is presently
available for payment and allotted to this contract. It is anticipated that from time to
time additional funds will be allocated to the contract as required by the payment
schedule in contract Section C, Clause 5.0, Launch Service Payments, Milestone
Events and Completion Criteria, until the total price of said CLINs is allotted

(b) The Contractor agrees to perform or have performed work on the items specified in
paragraph (a) of this clause up to the point at which, if this contract is terminated
pursuant to contract Section C, Clause 1.0(!) “Termination for the Government's
convenience” of this contract, the total amount payable by the Government
pursuant to contract Section C, Clause 1.0(l) would equal the amount retained by
the Contractor pursuant to Section C, Clause 5.0 and Table C-1. The Contractor is
not obligated to continue performance of the work beyond that point. The
Government is not obligated in any event to pay or reimburse the Contractor more .
than the amount from time to time allotted to the contract, anything to the contrary
in contract Section C, Clause 1.0(l) “Termination for the Government's
convenience” notwithstanding.

(c) (1) It is contemplated that funds presently allotted to this contract will cover the
work to be performed until [TBD].

(2) If funds allotted are considered by the Contractor to be inadequate to cover the
work to be performed until that date, or an agreed date substituted for it, the
Contractor shall notify the Contracting Officer in writing when within the next
sixty (60) days the work will reach a point at which, if the contract is terminated
pursuant to contract Section C, Clause 1.0(I) “Termination for the Government's
convenience” of this contract, the total amount payable by the Government
pursuant to contract Section C, Clause 1.0(1) would equal the amount retained
by the Contractor pursuant to contract Section C, Clause 5.0 and Table C-1

(3) (i) The notice shall state the estimate when the point referred to in paragraph
(c)(2) of this clause will be reached and the estimated amount of additional

C-20


Section D

Exhibit 2B: Taurus Standard Services

NASA Launch Services II (NLS I)

Contract NNK10LB01B

sow
Para.

Standard Service

Description

E2B-6



Section D ‘ NASA Launch Services II (NLS II)
Attachment D9: Most Favored Customer Certification Plan Contract NNK10LB01B

ATTACHMENT D9
MOST FAVORED CUSTOMER CERTIFICATION PLAN

Subject to the provisions of NLS Contract Article B.4.0, the Contractor hereby certifies that the
CLIN prices for NLS standard launch services (including standard mission integration)
awarded under this contract are no higher than the lowest price charged to any other
commercial or U.S. Government customer for an equivalent launch service during the twelve
(12) months both preceding and following placement of a Launch Service Task Order (LSTO)
The Government shall be entitled to a one-time reduction in contract price for each standard
launch service failing to meet this certification. For NLS missions that are under firm contract
LSTO the price credit will be equal to the difference between the total firm fixed price standard
launch service under this contract including non-standard services and mission unique
requirements and the lower price awarded for an equivalent launch service.

This plan only applies to LSTOs that are authorized by orders issued in accordance with
contract Section C, Clause 11.0, FAR 52.216-18 and shall not serve to reduce IDIQ prices in
Section B, Schedules for future launch services.

In determining whether the prices for standard launch vehicle services under this contract
(including mission integration, mission unique, and non-standard services) are no higher than
the lowest price charged by the Contractor within the preceding or following twelve (12)
months, the Government and Contractor shall agree to recognize the differences in NLS vs.
new Contract requirements in order to establish equivalency. As such, equivalent pricing will
be determined only after considering price discriminating components including but not limited
to:

Technical and Mission-Unique Requirements

Schedule/Period of Performance

Performance and Vehicle Type/Configuration

Dedicated Mission

Hardware Availability or Residual Inventory from previous missions
Mission Success Requirements

Quantity of Launches and/or Repetitive missions

Frequency of Procurements

Amount of Government Furnished Equipment, Facilities, and/or Services Provided
10. | Commercial Launch Service versus U.S. Government Launch Service
11 Data, Insight, and Approval Requirements

12 Overall Contract Terms and Conditions and Deliverables

OANOAARWN>

09-1


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

ATTACHMENT D2

CONTRACT DATA REQUIREMENTS LIST (CDRL)

D2-1


CDM RELEASED

Orbifal

NASA LAUNCH SERVICES
SPACE LAUNCH VEHICLE
SAFETY AND HEALTH PLAN

WARNING: INFORMATION SUBJECT TO U.S. EXPORT CONTROL LAWS. The attached documents
contain technical data within the definition of the International Traffic in Arms Regulations, and are subject
to the export control laws of the U.S. Government.

PREPARED BY

Orbital Sciences Corporation
Launch Systems Group

CAGE Code
ORIGINAL ISSUE DATE TM-18422 REVD
11 JUNE 2004 7 MAY 2010

CODE A1-0-C8



Section D NASA Launch Services II (NLS II)
Attachment D4: SB and SDB Subcontracting Plan Contract NNK10LB01B

Table II

Individual Subcontracting Goals for: NASA LAUNCH SERVICES (NLS)

Contract/Proposal Number: RFP 10-99-0021- Rev D

Principal types of supplies and/or services planned to be subcontracted:

Product/Service to be subcontracted Supplier type/size

Machined Hardware to OSC drawing Small, HUBZone small business, small
disadvantaged, veteran-owned & women-owned
small business

Printed Circuit Boards Small & small disadvantaged
Misc. Hardware Small, HUBZone small business, small

disadvantaged, veteran-owned & women-owned
small business

Motors Large (if not GFE)
Antenna's Minority Institution
Cable Assemblies Small, HUBZone small business, small

disadvantaged & women-owned small business
(if not manufactured in house)

Photo plots Small disadvantaged
Computers and peripherals Large, small, small disadvantaged & women-owned

See Master Subcontracting plan for additional plan elements.

D4-12


Section D NASA Launch Services II (NLS I!)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

2.3

2.3.1

Mission Integration Services
Mission Integration Management

The Contractor shall be responsible for managing the mission integration of the payload
flight and ground systems with the launch vehicle and its associated GSE. In
accordance with this responsibility, the Contractor shall perform, as a minimum, the
following services

(A) Provide a single point of contact with overall mission responsibility for each mission
This single point of contact shall be responsible for coordinating support from all
technical disciplines and management during the integration process.

(B) Conduct mission integration meetings (kick-off, working group, technical
interchange) approximately quarterly from Mission Integration Start (L-30M) to
faunch.

(C) Provide a co-chairperson along with NASA for all working groups and technical
interchange meetings. The Contractor co-chairperson shall be responsible for
preparing and distributing agendas, minutes and action item logs for each meeting
(SDRL S1-2). The Contractor shall maintain the action item database and ensure
closure of all actions.

iS)

Provide appropriate technical/engineering representation at payload preliminary
and critical design reviews.

(E) Plan, schedule, and manage mission analyses required to define and verify
compatibility of the payload with the interface requirements and environments
(reference Table D1-A, SOW paragraph 2.3.2).

(F) Track development status of and resolve issues associated with mission specific
hardware and software

(G) Coordinate interface and support requirements for the mission.

(H) Plan/coordinate mission specific flight operations.

(I) Manage integration activities at the launch site.

(J) Manage and coordinate the launch vehicle safety approval process.

(K) Prepare, maintain and implement a payload to launch vehicle ICD for each mission.
The ICD shall include all mission requirements including launch vehicle and launch
site interface definition and environments (including GSE). The ICD shall include

the payload to launch vehicle/launch site electrical and mechanical interface
drawings (CDRL C2-1.1). Thirty (30) days prior to launch, the approved ICD shall

D1A-17


Section D

NASA Launch Services II (NLS II)

Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

(1)

Coordination of payload and launch vehicle operations into an integrated
operational flow, preparation of the schedules, and provision of the schedules with
updates as needed to NNC.

Provision of contamination control for payloads while they are in the possession of
the Contractor, or in a Contractor-provided PPF IAW the SOW, paragraph 2.4.2.3.

Reserved.

Certification of payload contamination control requirements for: fairing surface
cleanliness, cleanroom environments, and purge system cleanliness.

(M) Support for the installation of customer provided RF re-radiating equipment as

ground support equipment in the payload processing facility.

(N) Provision for the planning and execution of activities associated with the integrated

testing of the customer's payload with the launch vehicle on the launch pad.

2.4.2.3 Contamination and Environmental Control

The Contractor shall provide and implement a generic payload contamination control
plan and, if required, provide and implement a contamination control implementation
plan for each payload. Using lIEST-STD-CC1246D, MIL-PRF-27401, ISO 14644-1, ISO
14644-2,and NASA RP-1124 (Rev-4) as guidelines, the launch service shall meet the
following minimum requirements:

(A) Payload/Vehicle Integration Environment. For all Contractor provided facilities

where the payload resides and is exposed (including payload processing facilities,
integration facilities, or facilities at the launch pad), a Class 8 clean room
environment IAW ISO 14644-1 shall be provided. In addition, the temperature and
humidity environment shall have the ability to be controlled and maintained within a
range of 19 to 25°C (66 to 77°F) and 30% to 65%, respectively. This environment
shall be maintained at all times unless the payload is encapsulated within a
transportation container or payload fairing and purge air has been established IAW
2.4.2.3(B) or (C), herein. The Contractor shall provide contamination and
environmental monitoring when the payload is exposed

Transportation Environment. The following shall apply to all payload transportation
containers (including the payload fairing, if used for transportation) provided by the
Contractor. Following payload encapsulation, the transportation container shall be
purged with conditioned filtered air or GNz. The payload environment, as measured
at a sensor located inside the fairing volume immediately upstream of the payload
cone air exit hole, shall be maintained within a temperature and humidity range of
13 to 23°C (55 to 73°F) and 30% to 50%, respectively. Relative humidity will be
controlled to preclude condensation within the fairing. Note that since Taurus
cannot control the lower humidity limit, conditions <30% may occur after payload

D1B-25


Section D NASA Launch Services II (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) : Contract NNK10LB01B

2.2

2.2.1

(K) Command, control, and power signal capability from the launch control facility to the
payload umbilical Ground Support Equipment (GSE) IAW the mission specific ICD.

(L) All mechanical GSE required to interface with the payload mechanical adapters and
accomplish the payload to launch vehicle mating operation IAW the mission ICD.

(M) Both halves of the electrical connector at each spacecraft-to-launch vehicle
interface. The Contractor shall provide three (3) sets for each electrical connector
interface: a flight set, a flight spare set, and a set for spacecraft testing

(N) All other hardware equipment, software, infrastructure, and logistics necessary to
perform the contracted launch services.

Program Management

The Contractor shall provide all program management functions required to provide the
launch services and to satisfy the mission requirements for each NASA mission. The
program management function of this contract shall provide insight to NASA for all
technical and programmatic activities performed under this contract.

The Contractor shall coordinate all program management functions and issues directly
with the KSC LSP designated representative(s). The NASA Contracting Officer is the
only NASA representative authorized to provide formal contract direction

Formal Reviews

The Contractor shall conduct program reviews, design reviews, and readiness reviews,
and shall provide for the participation of NNC. The Contractor shall provide minutes and
action items resulting from each review to NASA within one week after the review. A
copy of the presentation material shall be available at the review for all NNC attendees
(CDRL C1-1).

2.2.1.1 Program Reviews

During the contract performance period, the Contractor shall conduct Program Reviews
with NASA at least once per year to: report development and production status, ensure
schedules support program objectives, review action items, review program schedules,
and discuss any issues. The intent of the program review is to provide a forum for open
dialog between NASA and the Contractor with respect to launch services. NASA will
provide status of Agency direction at the reviews. The review location shall alternate
between NASA and Contractor facilities unless mutually agreed upon to do otherwise.

D1A-10



Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-3
PAYLOAD/EXPENDED STAGE SEPARATION ANALYSIS
DESCRIPTION/PURPOSE:

The Payload/Expended Stage Separation Analysis is required to demonstrate that adequate
separation distance exists between the payload and the upper stage during the relative motion
predicted following payload deployment. The analysis is also required to demonstrate that
payload tip-off rates satisfy requirements. This analysis supports pre-flight verification of
compliance with mission requirements.

DATA REQUIREMENTS:

(A) | Provide nominal, 3-sigma, or worst-case payload tip-off rates and cone angles
(cone angles if deployed while spinning) at deployment

(B) The analysis shall include the effects of residual thrust, vehicle and payload
mass properties uncertainties, and separation mechanism uncertainties.
Additionally, include any methods utilized to ensure contamination upon
separation is prevented.

(C) The report documenting this analysis shall list and describe all dispersion
sources used for the analysis, mass properties data sources, and all coordinate
systems used

(0) Expended stage/payload relative motion analysis following payload deployment

D2-34


Section D NASA Launch Services II (NLS I!)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C1-2
COUNTDOWN DOCUMENTATION
DESCRIPTION/PURPOSE:
To provide the documents necessary to launch the vehicle and also assist NASA management
in determination of a GO or NO-GO.
DATA REQUIREMENTS:
Appendices for the documents listed below shall be provided when necessary to present
supplemental or incidental information, detailed tabulations or deviations, or graphic
representations.

(A) | Countdown

The Countdown document shall provide:

(i) All necessary steps and built-in holds required to successfully launch the
vehicle and its payload during the launch window

(ii) Procedures required to safe the vehicle after a launch attempt
(iii) | Procedures required to recycle the countdown for another launch attempt
The necessary steps shall be listed as a sequence of events with each entry
including a T-time. T-time is defined as the time before launch, not including
planned holds, and with T-O being the time of launch vehicle lift-off from the
launch pad. T+ time is any event after T-0. Each member of the launch team
shall be identified by call sign and communication channel. All mission
constraints to launch shall also be identified.

(B) Mission Constraints Document
This document is a summary of all the launch vehicle, payload and range mission
constraints to launch. The launch vehicle constraints shall include, but not be
limited to:
(i) Weather

(ii) Communication

02-8


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

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C2


Section D NASA Launch Services | (NLS Il)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

2.2.2

2.2.3

2.2.4

2.2.5

(iii) Open corrective actions/problems reports
(iv) Mission Unique and First flight items
(E) Launch Readiness Review (LRR)

NASA will conduct/chair, and the Contractor shall participate in an LRR one day
prior to launch to verify all actions from the FRR are complete and final processing
has been successfully completed. NASA will appoint the chairperson for this
review. At the conclusion of this review, an “approval to proceed with launch
countdown’ is given. Representatives from the Contractor, Range, and NNC
agencies sign the Certificate of Flight Readiness. The Contractor shall prepare the
Certificate of Flight Readiness. A sample Certificate of Flight Readiness is provided
in Exhibit 4

Risk Management

The Contractor shall implement risk management techniques that address the
identification, analysis, mitigation, and tracking of potential impacts to mission success
The Contractor shall develop the criteria, methods, and procedures used for identifying
critical items in the Risk Management Plan (CDRL C3-6).

Configuration Management

The Contractor shall perform configuration management of the launch vehicle design
and production for all launch vehicle components/subsystems, hardware, and software.

Manifest Policy

The Contractor shall develop and provide a Manifest Policy as described in CDRL C1-4
that addresses the Contractor's overall approach to ensuring timely launch of payloads.
The Contractor shall provide a Program Master Schedule and Launch Vehicle Planning
Manifest (SDRL S1-3) to support Government mission scheduling.

New Launch Vehicle Orientation

The Contractor shall conduct an orientation briefing at KSC. This briefing shall
introduce Contractor personnel and establish project interfaces with NASA personnel
and describe the Contractor's organization and infrastructure. The briefing shall contain
information summarizing the design, performance, fabrication, integration, testing,
qualification and operational features of the launch vehicle systems and supporting
facilities required to provide the launch service in the form of diagrams, schematics,
pictures, drawings, videos, etc.

D1A-16


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

This page left intentionally blank


Section D NASA Launch Services II (NLS II)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

simulation prior to payload mate, and flight simulation following payload mate (SDRL
S6-3).

The Contractor shall provide compatible data of all recorded launch vehicle and GSE
telemetry (CDRL C6-2)

The Contractor shall provide a mutually agreed upon transport interface or extend the
Spacecraft command and telemetry streams between the launch complex and the
NASA designated NASA LSP Data Center

The Contractor shail provide voice and video communications from the launch complex
to the designated NASA LSP Data Center during integrated and stand-alone spacecraft
operations at the launch complex.

The Contractor shall implement the NASA provided console communications
configuration for those consoles occupied by the NASA team within the Contractor's
launch control center. The Contractor shall validate this configuration with the
designated NASA LSP Data Center prior to launch vehicle testing and mission
simulations

The Contractor shall provide to NASA, upon request, launch vehicle processing test
procedures in a mutually agreed upon electronic format prior to the test (SDRL S5-1).

The Contractor shall submit to NASA a draft version of a preliminary Statement of Work
for each downrange asset no later than four (4) months prior to launch

The Contractor shall coordinate the downrange assets and shall provide NASA the
latest documentation required by the downrange assets (e.g. PRD, Expedite OR, etc)
for receiving, recording, and relaying the data no later than sixty (60) days prior to
launch. The Contractor shall ensure proper operation of all launch vehicle telemetry
links (RF and hardwire), voice communication channels, and video (including launch
vehicle mounted camera video as applicable) to the NASA designated NASA LSP Data
Center prior to baseline launch vehicle processing. The Contractor shall provide the
downrange assets with the technical coordination needed to execute the telemetry
coverage (e.g. telemetry playback tapes, mission trajectory disks, etc) prior to the first
data flow test. The Contractor shall ship required electronic hardware and satisfy export
control and frequency authorizations as required by local and international
governments.

The Contractor shall provide data flow path diagrams and data flow schedules between
the NASA designated NASA LSP Data Center and down range assets to NASA NLT
fifteen (15) calendar days prior to launch and again at the Flight Readiness Review
(SDRL S6-4). The Contractor shalt also provide down range asset status/readiness at
the Flight Readiness Review.

D1A-21


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-7
COUPLED DYNAMIC LOADS ANALYSIS
DESCRIPTION/PURPOSE:

This analysis defines flight loads to major vehicle and payload structure. This analysis also
supports pre-flight verification of compliance with mission requirements.

DATA REQUIREMENTS:

(A) | A description of the model and forcing functions used in the analysis shall be provided
The payload model provided must be in an MSC-NASTRAN compatible format. The
model may be provided in Craig-Bampton format or as a Finite Element Model having
no more than 30,000 grid points (180,000 Degrees of Freedom (DOF)).

(B) The flight events and conditions that cause the greatest loads on the payload shall be
identified and included in the analysis. The flight events and conditions that cause the
greatest deflections in the fairing and payload (including instances of minimum
clearance) shall be identified and included in the analysis.

(C) Output from each flight event shall include maximum/minimum tables of payload
selected Acceleration Transformation Matrices (ATM), interface forces, and internal
Load Transformation Matrices (LTM). No more than 1,000 rows of output may be
requested.

(D) | Worst-case payload fairing dynamic relative deflections shail be identified and included.

(E) Three load cycles will be required per mission: A preliminary loads cycle, intermediate
loads cycle, and a verification loads cycle

D2-38


Section D

NASA Launch Services II (NLS II)

Attachment D2: Contract Data Requirements List Contract NNK10LB01B

3.4

3.5

3.3.6

Mission Satisfaction Kit

Flight Design

3.4.1

3.4.2
3.4.3
3.4.4
3.4.5
3.4.6

Contract Orbit Requirements

3.4.1.1 Mission Orbit Specification

3.4.1.2 Reference Mission

Launch Window

SC Separation

Sun Angle Constraint

Thermal Roll

LV Telemetry Data

3.4.6.1 SC Separation State Vector
3.4.6.2 SC Provided Post Separation Data

Ground Operations

3.5.1
3.5.2
3.5.3

3.6.4

3.5.5

3.5.6

Spacecraft Contractor Supplied Ground Support Equipment
Payload Processing Facility
Launch Complex Ground Operations
3.5.3.1 GSE
3.5.3.2 Ground Operations Communications
3.5.3.2.1 Countdown Clock
3.5.3.2.2 Closed Circuit TV
3.5.3.2.3 Public Address
3.5.3.2.4 Telephone
3.5.3.2.5 Operating Voice System
3.5.3.2.6 Contingency Operations
SC Transport
3.5.4.1. Processing Facility to Launch Complex Transport
3.5.4.2 SC Hoist and Mate Loads
Environmental Control System
3.5.5.1 PLF Environmental Control System
Fluids and Gases Requirements

3.6 Safety Requirements

D2-16


Section D NASA Launch Services II (NLS I!)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CORL DESCRIPTION Number: C1-1
FORMAL MEETING & REVIEW DOCUMENTATION

DESCRIPTION/PURPOSE:

To provide presentation and handout material, minutes, and accompanying action item lists

from each formal review.

DATA REQUIREMENTS:
Formal review documentation shall include:

(A) | Presentation packages and hand-out materials provided at the review for NASA
attendees

(i) Mission Specific Design Reviews
(ii) All other formal reviews

(B) Minutes from each formal review

(C) List of attendees

(D) Agreements from each formal review

(E) An action item list maintained and updated by the Contractor. The list shall

include:
(i) Due Date
(ii) Subject

(iii) | Assigned tracking number for each action item
(iv) Person or organization responsible for completing the action
(v) Status of action (i.e., open, closed, or deleted)

(vi) | Closure rationale

02-7


Section D

NASA Launch Services II (NLS Il)

Attachment 01B: Taurus Statement of Work (SOW) Contract NNK10LB01B

TABLE OF CONTENTS

INTRODUCTION...........0..0.....
Scope..........
Objectives...
Compliance Documents.
Reserved ......

STANDARD LAUNCH SERVICE
Launch Vehicle ceeeeee ee
Program Management....................6008
Formal Reviews...
Program Review:
Design Reviews - Mission Specific
Readiness Reviews.....

Risk Management..
Configuration Management...
Manifest Policy..

New Launch Vehicle Orientation.
Mission Integration Services... ...
Mission Integration Management. se
Mission Analyses... .
Mission Success Determination.
Launch Site Support...
Pre-Launch Checkout an
Launch Vehicle Preparation and Launch.. bees
Telemetry Data and Launch Countdown n Support .
Vehicle Telemetry :
Baseline and Integrated ‘Support...
Launch Countdown and Flight Support.
Launch Dress Rehearsal..
Launch Site Payload Support
Payload Processing Facility.....
Launch Site Payload Integration Support......
Contamination and Environmental Control.
Operational Support Services..
Range Support and Services...
Safety, Reliability, and Quality Assuranc:
Safety and Health Program..
Reliability Program.....
Quality Assurance Progra
NASA Insight and Approval..

D1B-3


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB018

(36) 52.232-29, Terms for Financing of Purchases of Commercial Items (Feb
2002) (41 U.S.C. 255(f), 10 U.S.C. 2307(f)).

(37) 52.232-30, Installment Payments for Commercial Items (Oct 1995) (41
U.S.C. 255(f), 10 U.S.C. 2307(f))

(38) 52.232-33, Payment by Electronic Funds Transfer-Central Contractor
Registration (Oct 2003)(31 U.S.C. 3332)

(39) 52.232-34, Payment by Electronic Funds Transfer-Other than Central
Contractor Registration (May 1999)(31 U.S.C. 3332).

(40) 52.232-36, Payment by Third Party (Feb 2010) (31 U.S.C. 3332).
(41) 52.239-1, Privacy or Security Safeguards (Aug 1996) (5 U.S.C. 552a)

(42)(i) 52.247-64, Preference for Privately Owned U.S.-Flag Commercial
Vessels (Feb 2006) (46 U.S.C. Appx 1241(b) and 10 U.S.C. 2631).

(ii) Alternate | (Apr 2003) of 52.247-64.

The Contractor shall comply with the FAR clauses in this paragraph (c), applicable
to commercial services, that the Contracting Officer has indicated as being
incorporated in this contract by reference to implement provisions of law or
executive orders applicable to acquisitions of commercial items:

(1) 52.222-41, Service Contract Act of 1965 (Nov 2007) (41 U.S.C. 351, et
seq.).

(2) 52.222-42, Statement of Equivalent Rates for Federal Hires (May 1989)
(29 U.S.C. 206 and 41 U.S.C. 351, et seq.).

(3) 52.222-43, Fair Labor Standards Act and Service Contract Act -- Price
Adjustment (Multiple Year and Option Contracts) (Sep 2009) (29 U.S.C. 206
and 41 U.S.C. 351, et seq.).

(4) 52.222-44, Fair Labor Standards Act and Service Contract Act -- Price
Adjustment (Sep 2009) (29 U.S.C. 206 and 41 U.S.C. 351, et seq.).

(5) 52.222-51, Exemption from Application of the Service Contract Act to
Contracts for Maintenance, Calibration, or Repair of Certain Equipment--
Requirements (Nov 2007) (41 U.S.C. 351, et seq.).

(6) 52.222-53, Exemption from Application of the Service Contract Act to

Contracts for Certain Services--Requirements (Feb 2009) (41 U.S.C. 351, et
seq.).

C-56


Section D NASA Launch Services I! (NLS II)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: $1-2
MISSION INTEGRATION MEETING DOCUMENTATION

DESCRIPTION/PURPOSE:

To provide presentation and handout material, minutes, and accompanying action item lists
from each mission integration meeting (e.g., MIWG kick-off, telecons, working groups, and
technical interchange).

DATA REQUIREMENTS:

Mission integration meeting documentation shall include

(A) Presentation packages and hand-out materials provided at the meeting for
NASA attendees

(B) | Agendas (delivered prior to meeting)

(C) | Minutes from each Mission integration meeting

(D) List of attendees

(E) | Agreements from each Mission integration meeting

(F) — An action item list maintained and updated by the Contractor. The list
shall include

(i) Due Date

(ii) Subject

(iii) | Assigned tracking number for each action item

(iv) Person or organization responsible for completing the action
(v) Status of action (i.e., open, closed, or deleted)

(vi) Decisions/resolutions of action items as determined by joint
NASA/Contractor mission integration team


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

(e)(4

(2)

(ii)

(iii

(iv)

The public liability referred to in subparagraph (d)(1) of this clause is public
liability as defined in the Act which (i) arises out of or in connection with the
activities under this contract, including transportation; and (ii) arises out of or
results from a nuclear incident or precautionary evacuation, as those terms are
defined in the Act.

Waiver of Defenses. In the event of a nuclear incident, as defined in the Act,
arising out of nuclear waste activities, as defined in the Act, the contractor, on
behalf of itself and other persons indemnified, agrees to waive any issue or
defense as to charitable or governmental immunity.

In the event of an extraordinary nuclear occurrence which:

Arises out of, results from, or occurs in the course of the construction,
possession, or operation of a production or utilization facility; or

Arises out of, results from, or occurs in the course of transportation of source
material, by-product material, or special nuclear material to or from a production
or utilization facility; or

Arises out of or results from the possession, operation, or use by the contractor
or a subcontractor of a device utilizing special nuclear material or by-product
material, during the course of the contract activity; or

Arises out of, results from, or occurs in the course of nuclear waste activities, the
contractor, on behalf of itself and other persons indemnified, agrees to waive:

Any issue or defense as to the conduct of the claimant (including the conduct of
persons through whom the claimant derives its cause of action) or fault of
persons indemnified, including, but not limited to:

Negligence;

Contributory negligence:

Assumption of risk; or

Unforeseeable intervening causes, whether involving the conduct of a third
person or an act of God;

Any issue or defense as to charitable or governmental immunity; and
Any issue or defense based on any statute of limitations, if suit is instituted within

3 years from the date on which the claimant first knew, or reasonably could have
known, of his injury or change and the cause thereof. The waiver of any such


Section D

NASA Launch Services I (NLS II)

Attachment D2: Contract Data Requirements List Contract NNK10LB01B

3.3.2

3.3.3
3.3.4

3.3.5

3.3.1.1 SC Thermal Environments
Contamination
3.3.2.1 Payload Fairing Purge
3.3.2.1.1 Spacecraft Transport to the Launch Complex
3.3.2.1.2 Spacecraft at Launch Complex
3.3.2.2 GHe Concentration
3.3.2.3 Payload Compartment Cleanliness
3.3.2.3.1 Non-Volatile Residue
3.3.2.3.2 PLF Inspection
3.3.2.3.3_ PLA Inspection
3.3.2.3.4 Witness Plate Access
3.3.2.3.5 Spacecraft Cleanliness
3.3.2.4 Spacecraft Contaminant Deposition Limits
3.3.2.4.1 Particulate
3.3.2.4.2 Molecular
3.3.2.5 Spacecraft Instrument GN2 Purge
Ascent Pressure
Dynamics
3.3.4.1 Sine Vibration
3.3.4.2 Acoustics
3.3.4.3 Shock
Electromagnetic Compatibility
3.3.5.1 EMI Safety Margin
3.3.5.2 Radiated Emissions
3.3.5.2.1 Spacecraft Maximum Allowable Radiated Emissions
3.3.5.2.2 Launch Vehicle Maximum Allowable Radiated Emissions
3.3.5.2.3 SC RF Susceptibility
3.3.5.2.4 Launch Site RF Environment
3.3.5.2.5 Portable Sources Radiated Emissions
3.3.5.3. PLF Electrostatic Discharge
3.3.5.4 Thermal Blanket Electrostatic Discharge
3.3.5.5 RF Transmitter/Receiver Systems EMC
3.3.5.6 Lightning
3.3.5.7 SC/LV Interface Electrical Bonding

D2-15


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

(e)

time requirement for proposal submission is increased from thirty (30) days to (60)
sixty days

Disputes. This contract is subject to the Contract Disputes Act of 1978, as
amended (41 U.S.C. 601-613). Failure of the parties to this contract to reach
agreement on any request for equitable adjustment, claim, appeal or action arising
under or relating to this contract shall be a dispute to be resolved in accordance
with the clause at FAR 52.233-1, Disputes, which is incorporated herein by
reference. The Contractor shall proceed diligently with performance of this contract,
pending final resolution of any dispute arising under the contract.

Definitions. The clause at FAR 52.202-1, Definitions, is incorporated herein by
reference under contract Section C, Clause 36.0.

Excusable delays. The Contractor shall be liable for default unless nonperformance
is caused by an occurrence beyond the reasonable control of the Contractor and
without its fault or negligence such as, acts of God or the public enemy, acts of the
Government in either its sovereign or contractual capacity, fires, floods, epidemics,
quarantine restrictions, strikes, unusually severe weather, and delays of common
carriers. The Contractor shall notify the Contracting Officer in writing as soon as it
is reasonably possible after the commencement of any excusable delay, setting
forth the full particulars in connection therewith, shall remedy such occurrence with
all reasonable dispatch, and shall promptly give written notice to the Contracting
Officer of the cessation of such occurrence. Excusable delays for launch delays by
either party are identified and shall be resolved in accordance with contract Section
C, Clause 19.0, Adjustments to Launch Schedule.

Invoice.
(1) The Contractor shall submit an original invoice and three copies (or electronic
invoice, if authorized) to the address designated in the contract to receive invoices.
An invoice must include:

(i) Name and address of the Contractor;

(ii) Invoice date and number;

(iii) Contract number, contract line item number, and, if applicable, the order
number,

(iv) Description, quantity, unit of measure, unit price and extended price of the
items delivered;

(v) Shipping number and date of shipment including the bill of lading number
and weight of shipment if shipped on Government bill of lading;

C-7


Section D NASA Launch Services II (NLS II)
Exhibit 3A: Pegasus Non-Standard Services List Contract NNK10LB01B

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E3A-40


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C5-2
MISSION UNIQUE HARDWARE TEST PLAN

DESCRIPTION/PURPOSE:

This plan describes the qualification, test and analysis effort for mission unique hardware
DATA REQUIREMENTS:

The mission unique hardware test plan shall include, as a minimum:

(A) Description, sequence, configuration, factors of safety, and success criteria for all
tests and analyses that support qualification of mission unique hardware

(B) A verification matrix of requirements versus tests/analyses

(C) | Reference to or description of any applicable industry standards used to support
testing

D2-47


Section D

NASA Launch Services II (NLS Il)

Attachment D1A:; Pegasus Statement of Work (SOW) Contract NNK10LB01B

(t)

Es

be incorporated into the contract via contract modification as Exhibit 8 to
Attachment D1. Any approved changes after its inclusion into the contract will be
incorporated prior to mission success determination.

Create and maintain an ICD Verification Matrix (CDRL C2-1.2) which shall include a
verification plan for each requirement in the ICD based on the appropriate method.
The Contractor shall perform verification of each ICD requirement based upon the
verification plan identified in the Verification Matrix.

Manage the design, development, qualification, testing and integration of mission
unique requirements.

Provide an initial assessment of the capability of the launch vehicle and define any
performance and payload volume the Contractor may make available to NASA for
secondary payloads.

Provide mission status to NNC throughout the launch campaign from Authority to
Proceed (ATP) through mission success determination.

Provide appropriate representation and participation at NASA conducted Ground
Operations Working Groups (GOWGs) approximately 2 times a year from L-27
months to spacecraft arrival at the launch site and at the NASA Ground Operations
Review (GOR)

2.3.2 Mission Analyses

All vehicles provided under this contract shall include the following analysis for each
mission as part of the standard launch service. The Contractor shall prepare and
submit the standard mission analyses as listed in Table D1-A.

CDRL ANALYSIS
C4-1 Performance and Guidance Accuracy Analysis
C4-2 Final Mission Analysis (FMA)

C4-3 Payload/Expended Stage Separation Analysis
C4-4 Payload Fairing Venting Analysis

C4-5 Payload Fairing Clearance Analysis

C4-6 Pre-Flight Controls and Stability Analysis

C4-7 Coupled Dynamic Loads Analysis

C4-8 Integrated Thermal Analysis

C4-9 RF Link Analysis

C4-10_| Payload/Launch Vehicle EMC, RF, and EED Compatibility Analysis
C4-11_| Mission Unique Software

C4-12_| Quick Look Flight Report

C4-13_| Final Flight Report

Table D1-A: Mission Analyses to Support Payload Integration

D1A-18


Section C

NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB01B

(t)

benefit; 40 U.S.C. 3701, et seq., Contract Work Hours and Safety Standards Act;
41 U.S.C. 51-58, Anti-Kickback Act of 1986; 41 U.S.C. 265 and 10 U.S.C. 2409
relating to whistleblower protections; Section 1553 of the American Recovery and
Reinvestment Act of 2009 relating to whistleblower protections for contracts funded
under that Act; 49 U.S.C. 40118, Fly American; and 41 U.S.C. 423 relating to
procurement integrity

Order of precedence. Any inconsistencies in this solicitation or contract shall be
resolved by giving precedence in the following order:

(1) The schedule and description of supplies/services (Section B, C, and
Statement of Work, excluding contract clauses incorporated by reference)

(2) The Assignments, Disputes, Payments, Invoice, Other Compliances, and
Compliance with Laws Unique to Government Contracts paragraphs of this
clause

(3) The clause at FAR 52.212-5 (Section C, Clause 34.0).

(4) Addenda to this solicitation or contract, including any license agreements for
computer software.

(5) Solicitation provisions if this is a solicitation
(6) Other paragraphs of this clause.

(7) The Standard Form 1449.

(8) Contract clauses incorporated by reference.
(9) Other documents, exhibits, and attachments.
(10) The specification.

Central Contractor Registration (CCR)

(1) Unless exempted by an addendum to this contract, the Contractor is
responsible during performance and through final payment of any contract for
the accuracy and completeness of the data within the CCR database, and for
any liability resulting from the Government's reliance on inaccurate or
incomplete data. To remain registered in the CCR database after the initial
registration, the Contractor is required to review and update on an annual
basis from the date of initial registration or subsequent updates its information
in the CCR database to ensure it is current, accurate and complete. Updating
information in the CCR does not alter the terms and conditions of this contract
and is not a substitute for a properly executed contractual document.


Section C NASA Launch Services II (NLS I!)
Contract Terms and Conditions Contract NNK10LB01B

25.4

25.5

25.6

25.7

operations organization of meetings, reviews, or tests in sufficient time to permit
meaningful Government participation

Should approval or insight identify non-compliance with the terms and conditions of the
contract, a difference in interpretation of test results, or disagreement with the
Contractor technical directions, the Government will take appropriate action within the
terms of the contract to ensure compliance via written direction to the Contractor.

NASA shall have insight into any Contractor initiated fleet changes or any changes that
may affect NASA missions. This insight shall be accommodated with no increase in
contract price.

Specific areas where the Government requires approval and/or insight are listed in
paragraphs 25.7 and 25.8 respectively. The paragraphs document requirements
specified in NPD 8610.23 Launch Vehicle Technical Oversight Policy.

Specific areas requiring Government approval are:

(A) Spacecraft-to-launch vehicle interface control documents/drawings.

(B) Decisions/resolutions of action items as determined by joint NASA/Contractor
mission integration teams.

(C) Mission unique hardware design, analysis, manufacture, and test.

(D) Mission unique software design, analysis, and test

(E) Baseline and changes to the Contractor's Risk Management, Reliability, Safety and
Health, and Quality Management Plans, consistent with the intent of NPD 1280.1,
NPR 7120.5, and NPR 8715.3

(F) Top-level test plans, requirements, and success criteria for integrated vehicle
systems and for tests that verify the integrated vehicle interfaces.

(G) Launch commit criteria.

(H) Closeout of actions from NASA-Chaired Mission and Flight Readiness Reviews.
(1) Spacecraft handling procedures and deviations.

(J) Integrated spacecraft/vehicle mate, test, and closeout procedures and deviations.

(K) Integrated spacecraft/vehicle mate, test, and closeout as performed procedures and
deviations.

Cc-41


Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

2.2.1.3 Readiness Reviews

The Launch Vehicle Systems Readiness Review, Pre-Mate Readiness Review, Launch
Management Coordination Meeting (LMCM), Flight Readiness Review (FRR) and
Launch Readiness Review (LRR) described herein will be conducted for each NASA
mission.

(A) Launch Vehicle Systems Readiness Review

(B)

The Contractor shal! conduct a Launch Vehicle Systems Readiness Review to
demonstrate that the launch site and launch vehicle are ready to proceed with
launch vehicle processing activities at the launch site. The Contractor shall present
as a minimum:

(i) Mission description including S/C and launch vehicle configuration; integration
status; summary of waivers; post launch data review of previous flights (NASA
and non-NASA); mission specific analyses results and status; vehicle hardware
assignments, assessments and status; and launch site status

(ii) A detailed schedule showing all activities (ground and flight) remaining to
achieve a successful, on-time launch

Pre-Mate Readiness Review

The Contractor shall conduct a Pre-Mate Readiness Review to demonstrate the
launch site and launch vehicle are ready for payload mechanical and electrical
integration. The Contractor shall conduct a launch vehicle/site walk-down
[reference SOW Section 2.4.1.1(D)] with NNC participation prior to or in conjunction
with the Pre-Mate Readiness Review. The Contractor shall present as a minimum:

(i) Action item status, safety status, payload mating plan, closure plan, payload
integration/launch site documentation, interface verifications, checkout and
launch software status, nonconformance reports, launch site status, S/C
readiness, and review of flight profile.

(ii) A detailed schedule showing all activities remaining to achieve an on-time
launch

Launch Management Coordination Meeting (LMCM)

The Contractor shall participate in an LMCM conducted by NASA before each
launch dress rehearsal or launch. The LMCM is used to ensure the readiness of
the launch team to execute the procedures necessary to conduct the launch dress
rehearsal (reference SOW Section 2.4.1.3) or launch. At this meeting, participant
roles and responsibilities during countdown shall be identified. The Contractor shall

D1A-14


Section D NASA Launch Services II (NLS I!)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C6-2
VEHICLE AND GSE TELEMETRY (TEST, PRE-LAUNCH, AND LAUNCH)
DESCRIPTION/PURPOSE:

To provide real time launch vehicle and GSE telemetry (RF and Hardwire) to the NASA
designated NASA LSP Data Center which will allow NASA to perform independent data
processing and analysis.

DATA REQUIREMENTS:
Provide as a minimum:

(A) All real time launch vehicle and GSE telemetry (RF and hardwire) test data to the
NASA designated NASA LSP Data Center for all system and sub-system testing
upon request. This data must be able to be time correlated in a manner that
enables time synchronization and must conform to the standards defined in IRIG
Standard 106-07.

(B) All real time launch vehicle and GSE telemetry (RF and Hardwire) to the NASA
designated NASA LSP Data Center from the start of Launch Countdown through
all phases of powered flight up to LOS. This data must be able to be time
correlated in a manner that enables time synchronization and must conform to
the standards defined in IRIG Standard 106-07.

D2-53


Section C

Contract Terms and Conditions

NASA Launch Services II (NLS II)
Contract NNK10LB01B

9.0

9.4

9.2

ORDERING PROCEDURE AND PAYMENT FOR SPECIAL TASK ASSIGNMENTS
(STUDIES AND ANALYSES) (CLIN 10)

The Contractor shall incur hours under CLIN 10 of this contract only in the performance
of task orders and revisions to task orders issued in accordance with this ordering
procedure. No other costs or hours under CLIN 10 are authorized. Special Task
Assignments shall be performed on a Firm-Fixed-Price (FFP) completion basis unless
specifically authorized otherwise by the Contracting Officer

Special Task Assignments shall be subject to the following ordering procedure:

(A) The Contracting Officer shall request a Task Plan from the Contractor. The request
shall include:

(E

(i)

(ii)
(iii)
(iv)

Statement of Work

Required Completion Date
Government Point of Contact

Due date for Contractor's Task Plan

The Contractor's Task Plan shall include:

(i)

Discussion of the technical approach for performing the work and
rationale for any proposed changes to the Statement of Work and required
completion date.
Required authorization to proceed date.
Basis of Estimate (BOE) - The total price broken down by task with the
following elements identified:
(a) The direct labor hours broken down by work element subject to the
Hourly Labor Rates in Section B, Clause 1.5, Table B-6
(b) Other Direct Costs identified by element (Travel, Material, Subcontracts) if
applicable.

The Contracting Officer shall accept the Contractor's Task Plan within ten (10)
working days of receipt or enter into negotiations with the Contractor. The parties
shall execute a bi-lateral Special Task Assignment.

The Special Task Assignment will contain, as a minimum, the following information:

(i)

(ii)
(iii)
(iv)

(v)
(vi)

Signature of the Contracting Officer's Technical Representative and the
Government's Contracting Officer

Contract number, Special Task Assignment number, effective date and
completion date

Title and Statement of Work

Total firm fixed price, including the number of labor hours

Quality assurance standards, as appropriate

Any other necessary information

The Special Task Assignments may be revised in the same manner as they are
executed via formal revisions.

C-24


Section D NASA Launch Services 1! (NLS II)

Exhibit 2B: Taurus Standard Services Contract NNK10LB01B
“sow ; —
Para. Standard Service Description

E2B-8


Section D

NASA Launch Services II (NLS II)

Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

(L)

(P)

Create and maintain an ICD Verification Matrix (CDRL C2-1.2) which shall include a
verification plan for each requirement in the ICD based on the appropriate method
The Contractor shall perform verification of each ICD requirement based upon the
verification plan identified in the Verification Matrix.

Manage the design, development, qualification, testing and integration of mission
unique requirements.

Provide an initial assessment of the capability of the launch vehicle and define any
performance and payload volume the Contractor may make available to NASA for
secondary payloads.

Provide mission status to NNC throughout the launch campaign from Authority to
Proceed (ATP) through mission success determination.

Provide appropriate representation and participation at NASA conducted Ground
Operations Working Groups (GOWGs) approximately 2 times a year from L-27
months to spacecraft arrival at the launch site and at the NASA Ground Operations
Review (GOR).

2.3.2 Mission Analyses

All vehicles provided under this contract shall include the following analysis for each
mission as part of the standard launch service. The Contractor shall prepare and
submit the standard mission analyses as listed in Table D1-A

CDRL ANALYSIS
C4-1 Performance and Guidance Accuracy Analysis
C4-2 Final Mission Analysis (FMA)

C4-3 Payload/Expended Stage Separation Analysis
C4-4 Payload Fairing Venting Analysis

C4-5 Payload Fairing Clearance Analysis

C4-6 Pre-Flight Controls and Stability Analysis

C4-7 | Coupled Dynamic Loads Analysis

C4-8 Integrated Thermal Analysis

C4-9 RE Link Analysis

C4-10 | Payload/Launch Vehicle EMC, RF, and EED Compatibility Analysis
C4-11__| Mission Unique Software

C4-12 | Quick Look Flight Report

C4-13_| Final Flight Report

Table D1-A: Mission Analyses to Support Payload Integration

The standard launch service shall include all analyses required to support NASA's
assessment of compliance with NPR 8715.6A, NASA Procedural Requirements for

D1B-18


Section C

NASA Launch Services II (NLS I)

Contract Terms and Conditions Contract NNK10LB01B

(vi) | Terms of any discount for prompt payment offered:
(vii) Name and address of official to whom payment is to be sent;

(viii) Name, title, and phone number of person to notify in event of defective
invoice; and

(ix) | Taxpayer Identification Number (TIN). The Contractor shall include its TIN
on the invoice only if required elsewhere in this contract

(x) Electronic funds transfer (EFT) banking information.

(A) The Contractor shall include EFT banking information on the
invoice only if required elsewhere in this contract.

(B) If EFT banking information is not required to be on the invoice, in
order for the invoice to be a proper invoice, the Contractor shall
have submitted correct EFT banking information in accordance with
the applicable solicitation provision, contract clause (e.g., 52.232-
33, Payment by Electronic Funds Transfer—Central Contractor
Registration, or 52.232-34, Payment by Electronic Funds
Transfer—Other Than Central Contractor Registration), or
applicable agency procedures.

(C) EFT banking information is not required if the Government waived
the requirement to pay by EFT.

(2) Invoices will be handled in accordance with the Prompt Payment Act (31
U.S.C.3903) and Office of Management and Budget (OMB) prompt payment
regulations at 5 CFR part 1315.

Patent indemnity. The Contractor shall indemnify the Government and its officers,
employees and agents against liability, including costs, for actual or alleged direct
or contributory infringement of, or inducement to infringe, any United States or
foreign patent, trademark or copyright, arising out of the performance of this
contract, provided the Contractor is reasonably notified of such claims and
proceedings.

C-8


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

(b) All or substantially all of the Contractor's operations at any one plant or
separate location in which this contract is being performed

(c) A separate and complete major industrial operation in connection with the
performance of this contract

(v) Liabilities that arise from the willful misconduct or gross negligence of the
Claimant or, in the case of a claim based on death, the claimant's
descendant.

32.5 Third Party Liability for NASA Secondary Payloads on Non-NASA Primaries

The requirements of this clause 32.0 shall apply to all launch services provided under
this contract except for those services involving NASA secondary payloads which are
manifested on a launch service for non-NASA (commercial) primary payloads. In the
event that a NASA secondary payload is manifested on a launch service for a non-
NASA (commercial) primary payload, the contractor shall obtain third party liability
insurance and indemnification for third party claims in excess of insurance pursuant to
the Commercial Space Launch Act, 49 U.S.C. 70101 et seq

33.0 FAR 52.212-3 OFFEROR REPRESENTATIONS AND CERTIFICATIONS--
COMMERCIAL ITEMS (AUG 2009) ALT | (APRIL 2002)

The Offeror Representations and Certifications (Attachment E1) as completed by the
Contractor are hereby incorporated in their entirety by reference with the same force and effect
as if they were given in full text.

34.0 FAR 52.212-5 CONTRACT TERMS AND CONDITIONS REQUIRED TO IMPLEMENT
STATUTES OR EXECUTIVE ORDERS--COMMERCIAL ITEMS (APR 2010)

(a) The Contractor shall comply with the following Federal Acquisition Regulation
(FAR) clauses, which are incorporated in this contract by reference, to implement
provisions of law or Executive orders applicable to acquisitions of commercial
items:

(1) 52.222-50, Combating Trafficking in Persons (FEB 2009) (22 U.S.C. 7104(g))

Alternate | (AUG 2007) of 52.222-50 (22 U.S.C. 7104 (g))

(2) 52.233-3, Protest After Award (AUG 1996) (31 U.S.C. 3553).
(3) 52.233-4, Applicable Law for Breach of Contract Claim (OCT 2004) (Pub. L.
108-77, 108-78).

(b) The Contractor shall comply with the FAR clauses in this paragraph (b) that the
Contracting Officer has indicated as being incorporated in this contract by reference
to implement provisions of law or Executive orders applicable to acquisitions of
commercial items:

C-52


Section D NASA Launch Services II (NLS II)
Attachment D2: Contract Data Requirements List Contract NNK10LB01B

CDRL DESCRIPTION Number: C4-1
PERFORMANCE AND GUIDANCE ACCURACY ANALYSIS (PGAA)
DESCRIPTION/PURPOSE:

This analysis is prepared using the best available mission requirements (payload mass
properties, insertion state vector requirements, tracking requirements, etc.) to identify any
potential problems inherent in accomplishing the mission objectives. This analysis shall
include parametric trade studies.

DATA REQUIREMENTS:

The analysis shall include, as a minimum:

(A) The nominal and 3-sigma limits for orbit elements and associated covariance
matrix

(B) | Performance impacts as a function of launch date and time

(C) Performance capability, margins and reserves, including description of how
performance reserve is calculated

(D) Sequence of events and tracking coverage

(E) Time history of trajectory from launch to targeted condition and end of mission
maneuvers

(F) Launch vehicle summary weight statement

(G) Sources and magnitude for all dispersions used. If statistical dispersions are
used, then the distribution method (e.g., normal, gaussian) shall be specified for
each parameter

(H) Definition of all coordinate systems used

(I) Reference to the source(s) for all payload and launch vehicle inputs to this
analysis (e.g., requirements, mass properties)

(J) Evaluation of compliance with applicable ICD requirements and constraints
(K) Launch windows determined by analysis

(L) Input file

D2-32


Section D

NASA Launch Services II (NLS I!)

Attachment 01B: Taurus Statement of Work (SOW) Contract NNK10LB01B

(D

authority to issue a GO, NO GO, and HOLD during launch countdown. The
Contractor shall describe its launch day management activities, identify key team
members, and define responsibilities and communications between the launch
vehicle, NASA, and payload teams.

Flight Readiness Review (FRR)

NASA will conduct/chair, and the Contractor shall participate in an FRR for each
mission to ensure the specific launch vehicle is acceptable for flight and all Range
and other mission requirements have been met, or will be satisfied prior to launch.
The FRR is held approximately three (3) days before launch. As a minimum, the
Contractor shall provide verification that:

(i) All critical items required to proceed into final launch countdown are ready

(ii) Vehicle configuration is defined and all vehicle systems have been verified
IAW launch site test plans

(iii) All previously recorded action items have been closed or are reflected on the
schedule

(iv) All previously held Contractor's readiness review actions have been closed or
resolved

(v) Launch site/Range support organizations have committed to launch
(vi) Tracking and data support resources are committed to launch

(vii), Any open work is identified and closeout plans and schedules are in place and
supportable

(viii) Any constraints to launch are identified and resolution plans developed
(ix) Mission risks are known and documented

(x) Launch commit criteria for payload and launch vehicle is approved and
released

The Contractor shall also discuss:
(i) Anomalies from previous missions, including non-NASA missions

(ii) Hardware/software failures in the field either on the NASA assigned launch
vehicle or in the fleet

D1B-15


Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

Document No Rev. Document Title

NPD 8610.24 Launch Services Program (LSP) Pre-Launch Readiness
Reviews

NPD 8610.7 Launch Services Risk Mitigation Policy for NASA-Owned and/or

LSP-PLN-324.01
NPR 8621.1

LSP-PLN-353.01
NPD 1280.1
NPR 7120.5

NPR 8715.3
1

8.0 RESERVED

NASA-Sponsored Payloads/Missions
Expendable Launch Vehicle Certification

NASA Procedural Requirements for Mishap and Close Call
Reporting, Investigating, and Recordkeeping

Launch Services Program Risk Management Plan
NASA Management System Policy

NASA Space Flight Program and Project Management
Requirements

NASA General Safety Program Requirements

MIL-STD-1773 may be substituted

D1A-33


Section D NASA Launch Services II (NLS II)
Attachment D4: SB and SDB Subcontracting Plan Contract NNK10L801B

ORBITAL SCIENCES CORPORATION
LAUNCH SYSTEMS GROUP (LSG)
3380 SOUTH PRICE ROAD
CHANDLER, AZ 85248

SMALL BUSINESS

VETERAN-OWNED SMALL BUSINESS
(Includes Service Disabled Veteran Owned Small Business)

HUBZone SMALL BUSINESS

SMALL DISADVANTAGED BUSINESS
(Includes Historically Black Colleges and Universities and Minority Institutions)

WOMEN-OWNED SMALL BUSINESS

SUBCONTRACTING MASTER PLAN

Submitted By: Dnos

Taragh Mulvihill
Sr. Mgr. Procurement Compliance

D4-5


Section D

NASA Launch Services II (NLS I!)

Attachment D10: Acronyms and Abbreviations Contract NNK10LB01B
FRR Flight Readiness Review

FSC Federal Supply Class

FSG Federal Supply Group

FTS Flight Termination System

g Acceleration of Gravity

G&A General and Administrative

GACS Ground Air Conditioning System

GAO General Accounting Office

GFP Government-Furnished Property

GHe Gaseous Helium

GIDEP Government/ Industries Data Exchange Program
GN&C Guidance Navigation and Control

GN2 Gaseous Nitrogen

GOR Ground Operations Review

Govt. Government

GOWG Ground Operations Working Group

GPA Agreement on Government Procurement from World Trade Organization
GSA General Services Administration

GSE Ground Support Equipment

GSFC Goddard Space Flight Center

GSO Geo-Synchronous Orbit

GTO Geosynchronous Transfer Orbit

HAPS Hydrazine Auxiliary Propulsion System

HBCU Historically Black Colleges and Universities
Horiz Horizontal

HUBZone Historically Underutilized Business Zones

Hz Hertz

Lloads Inertial Loads

IAW In Accordance With

ICD Interface Control Document

ID Identification

IDIQ Indefinite Delivery/Indefinite Quantity

IEEE Institute of Electrical and Electronics Engineers
IEST-STD Institute of Environmental Sciences and Technology Standard
IFB Invitation For Bid

IMU Inertial Measurement Unit

INS Inertial Navigation System

IRCA International Registrar of Certified Auditors
IRIG Inter-Range Instrumentation Group

IRS Internal Revenue Service

ISO International Organizations for Standardization
IT Information Technology

ITAR International Traffic in Arms Regulations

D10-3


Section D NASA Launch Services II (NLS Il)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

ATTACHMENT D1B

TAURUS STATEMENT OF WORK

D1B-1


Section D NASA Launch Services II (NLS II)
Attachment D10: Acronyms and Abbreviations Contract NNK10LB01B

ATTACHMENT D10

ACRONYMS AND ABBREVIATIONS

AIR As Required

AACS Airborne Air Conditioning System

AAM Acquisition Assistance Message

ABCL As Built Configuration List

ACS Attitude Control System

AFS Agency Filing Scheme

AFSPCl Air Force Space Command Instruction
AFSPCMAN _ Air Force Space Command Manual

Amps Amperes

ASCII American Standard Code for Information Interchange
ASE Airborne Support Equipment

ASO Astrotech Space Operations

ASTM American Society for Testing and Materials
ATM Acceleration Transformation Matrix

ATP Authority to Proceed

Attn. Attention

BVS Best Value Solicitation

Cc Celsius

C3 Earth escape energy expressed in km/sec?
CAE Computer Aided Engineering

CCAM Collision/Contamination Avoidance Maneuver
CCAFS Cape Canaveral Air Force Station

CCB Configuration Control Board

CCR Central Contractor Registration

CCRIP Contamination Control Requirements & Implementation Plan
CDRL Contract Data Requirements List

CFR Code of Federal Regulations

CG Center of Gravity

CLA Coupled Loads Analysis

CLIN Contract Line Item Number

cM Configuration Management

cm centimeter

COLA Collision Avoidance

COTR Contracting Officer's Technical Representative
COTS Commercially Available Off-the-Shelf

CST Combined Systems Test

CVCM Collected Volatile Condensable Materials

CY Calendar Year

D10-1


Section D NASA Launch Services II (NLS Il)
Attachment D3: Supplemental Data Requirements List (SDRL) Contract NNK10LB01B

SDRL DESCRIPTION Number: S4-1
MISSION BATTERY BUDGET ANALYSIS
DESCRIPTION/PURPOSE:

This analysis verifies sufficient energy and peak load margin exists to satisfy both vehicle and
payload requirements.

DATA REQUIREMENTS:

Contractor formats acceptable.

D3-9


Section B

SF 1449 Continuation

NASA Launch Services II (NLS II)
Contract NNK10LB01B

CLIN

Description of
Supplies and Services

Contract
Mod‘

Qty

Total
Amount

($)

Unit

Unit Price ($)

x!

IDIQ Launch Service Task
Order (LSTO)

Launch Vehicle Configuration
___TBD. for Mission
___"TBD.
Launch Date TBD.
Launch Period, if applicable

TBD.

TBD

TBD?

Service TBD TBD

SubCLIN

xX'A

x'c

Standard Launch Services and
Standard Mission Integration in
accordance with the SOW and
Exhibit 2

Launch Vehicle Configuration
_—_TBD___

Non-Standard Services in
accordance with the SOW and
Exhibit 3

Nonstandard Services
__TBD__

Known Mission Unique Hardware
and Software Non-recurring
Items in accordance with SOW
Exhibit 6

Mission Unique Services
_TBD_

TBD*

TBD

TBD

Lot See
Table B-9

Lot See
Table B-10

Lot TBD

The Contracting Officer shall determine the CLIN number to be assigned.

2 The actual number of LSTOs to be awarded is TBD.

table.

The actual number of missions to be included in each LSTO is TBD.
As various Contract Modifications are issued for services ordered, their respective number will be listed in this

Table B-8: IDIQ Launch Service Task Order


Section D

NASA Launch Services II (NLS II)

Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

(B) Mission Specific Preliminary Design Review (MSPDR)

The Contractor shall conduct a preliminary detailed design review prior to major
commitment to drawings and design. Mission unique trade studies shall be
completed prior to the MSPDR. The Contractor shall discuss analyses performed
and their results along with comparisons to any similar proven designs. The
Contractor shall evaluate the safety of the design and its ability to meet safety
requirements. The preliminary mission unique design shall be subject to NASA's
approval. NASA reserves the right to withhold approval until all action items have
been closed. As a minimum, the Contractor shall provide verification of the
following items at the MSPDR

(i) All system requirements have been allocated to the subsystem and
component level and the flow down is adequate to verify system performance.

(ii) The design solutions being proposed are expected to meet the performance
and functional requirements.

(iii) The design does not pose major problems that may cause schedule delays.

(iv) Overall system architecture has been established and all launch vehicle to
payload interfaces have been identified and are verifiable

(v) The design solution can be produced based on existing processes and
techniques; if not, risk areas, which require unique and unproven processes,
are identified and risk mitigation plans are established.

(vi) An acceptable operations concept has been developed.

(vii) Preliminary launch vehicle interfaces have been defined.

(viii) Preliminary plans are established for end-to-end testing methodologies.
(ix) 30% mission unique drawings released.

Mission Specific Critical Design Review (MSCDR)

The Contractor shall conduct an MSCDR prior to design freeze and before
significant fabrication activity begins. The Contractor shall present a final detailed
design using drawings, analyses, and evaluation testing that shows the design
meets final performance and interface specifications, safety requirements, and
mission objectives. The Contractor shall provide selection criteria for the evaluation
tests performed to prove validity. The mission unique critical design shall be subject
to NASA's approval. NASA reserves the right to withhold approval until all action
items have been closed. As a minimum, the Contractor shall provide verification of
the following items at the MSCDR:

D1A-12


Section C NASA Launch Services II (NLS II)
Contract Terms and Conditions Contract NNK10LB01B

(i) Technical capability/risk, including the following:

(a) Contractor's ability to meet SOW and specific payload requirements,
including launch period and launch date

(b) Launch vehicle certification or reasonableness of the Offeror's plan to
obtain certification prior to mission launch

(c) Information gained through Government insight and approval activities
(d) Status of significant baseline vehicle changes and resolution of anomalies

(e) Unique terms and conditions contained in a contract, which may impact
price, performance or risk

(f) Proposed launch vehicle’s demonstrated flight experience
(ii) Reasonableness of proposed price, including any proposed quantity discounts.

(iil) Past performance, with emphasis given to the most recent and more relevant
experience, including small business achievements.

The Requests for Launch Service Proposals shall state, whether all evaluation
factors other than cost or price, when combined, are—

(i) Significantly more important than cost or price;

(ii) Approximately equal to cost or price; or

(iii) Significantly less important than cost or price.

The Government reserves the right to modify the evaluation criteria for individual
LSTOs. The final evaluation criteria will be defined in the request for LSTO
proposal. In any event, the Government intends to award an LSTO to the
Contractor who provides the best value in launch services that meet the
Government's requirements

(E) Award of an LSTO.

(i) The Contracting Officer will notify the Contractor of ATP of the launch service
via award of the task order.

(ii) Each of the IDIQ Contractors will be notified of the Government's award of an
LSTO.

C-29


Section D NASA Launch Services II (NLS 1!)
Exhibit 3A: Pegasus Non-Standard Services List Contract NNK10LB01B

EXHIBIT 3A

PEGASUS NON-STANDARD SERVICES LIST

E3A-1


Section D NASA Launch Services II (NLS I!)
Attachment D1B: Taurus Statement of Work (SOW) Contract NNK10LB01B

2.2

2.2.1

(K) Command, control, and power signal capability from the launch control facility to the
payload umbilical Ground Support Equipment (GSE) IAW the mission specific ICD.

(L) All mechanical GSE required to interface with the payload mechanical adapters and
accomplish the payload to launch vehicle mating operation IAW the mission ICD.

(M) Both halves of the electrical connector at each spacecraft-to-launch vehicle
interface. The Contractor shall provide three (3) sets for each electrical connector
interface: a flight set, a flight spare set, and a set for spacecraft testing.

(N) All other hardware equipment, software, infrastructure, and logistics necessary to
perform the contracted launch services.

Program Management

The Contractor shall provide all program management functions required to provide the
launch services and to satisfy the mission requirements for each NASA mission. The
program management function of this contract shall provide insight to NASA for all
technical and programmatic activities performed under this contract.

The Contractor shall coordinate all program management functions and issues directly
with the KSC LSP designated representative(s). The NASA Contracting Officer is the
only NASA representative authorized to provide formal contract direction

Formal Reviews

The Contractor shall conduct program reviews, design reviews, and readiness reviews,
and shall provide for the participation of NNC. The Contractor shall provide minutes and
action items resulting from each review to NASA within one week after the review. A
copy of the presentation material shall be available at the review for all NNC attendees
(CDRL C1-1).

2.2.1.1 Program Reviews

During the contract performance period, the Contractor shall conduct Program Reviews
with NASA at least once per year to: report development and production status, ensure
schedules support program objectives, review action items, review program schedules,
and discuss any issues. The intent of the program review is to provide a forum for open
dialog between NASA and the Contractor with respect to launch services. NASA will
provide status of Agency direction at the reviews. The review location shall alternate
between NASA and Contractor facilities unless mutually agreed upon to do otherwise

D1B-10


Section D

Attachment D10: Acronyms and Abbreviations

NASA Launch Services II (NLS II)
Contract NNK10LB01B

KHB
km
KSC

LAT
LAT
Ibm
LEO
LEV
LHC.
LMCM
LON
LOS
LPO
LRR
LSC
LSE
LSG
LSP
LSTO
LSV
LTM

LVDC

MACH
MARS
MDL
MIL-PRF
MIL-STD
MIS
MIWG

MPCP
MRB
MSCDR
MSDS
MSPDR
MSPSP
MSRR
MSSAR

Kilogram

Kennedy Handbook
Kilometer

Kennedy Space Center

Launch

Latitude

Lot Acceptance Test
Pounds Mass

Low Earth Orbit

Launch Equipment Van
Left Hand Circular

Launch Management Coordination Meeting
Longitude

Loss of Signal

Launch Panel Operator
Launch Readiness Review
Launch Service Contractor
Launch Support Equipment
Launch Systems Group
Launch Service Program
Launch Service Task Order
Launch Support Van

Load Transformation Matrix
Launch Vehicle

Launch Vehicle Data Center

Month

Modular Avionics Control Hardware
Mid-Atlantic Regional Spaceport

Mission Data Load

Military Performance Specification

Military Standard

Mission Integration Start

Mission Integration Working Group

Month

Mishap Preparedness and Contingency Plan
Material Review Board

Mission Specific Critical Design Review
Material Safety Data Sheets

Mission Specific Preliminary Design Review
Missile System Prelaunch Safety Package
Mission Specific Requirements Review
Mission Specific System Acceptance Review

D104


Section D NASA Launch Services II (NLS 11)
Attachment D1A: Pegasus Statement of Work (SOW) Contract NNK10LB01B

2.3.3

24

2.4.1

The standard launch service shall include all analyses required to support NASA's
assessment of compliance to NPR 8715.6A, NASA Procedural Requirements for
Limiting Orbital Debris. The number of submittals for the Standard Mission Analyses
are identified in Table D2-A.

Mission Success Determination

Mission success will be based on the criteria set forth in Section C, paragraph 24.1,
Mission Success Criteria. Mission success determination requirements are detailed in
Section C, paragraph 24.2, Mission Success Determination

The Contractor shall prepare and submit a Quick Look Flight Report (CDRL C4-12) and
a Final Flight Report (CDRL C4-13). Within thirty (30) days of receipt of the Final Flight
Report, the Contracting Officer will either determine the launch a Mission Success or
inform the Contractor of the Government's intent to withhold determination for payload
evaluation

Launch Site Support

Pre-Launch Checkout and Launch Support

2.4.1.1. Launch Vehicle Preparation and Launch

For launch services provided under this contract, the Contractor shall, as a minimum;

(A) Perform ail launch vehicle preparations and launch site operations necessary to
safely and successfully deliver the payload to the desired orbit.

(B) Generate the required documents (CDRL C3-7) and obtain all required safety
approvals for the launch vehicle system and integrated payload/launch vehicle
system operations including payload/launch vehicle system integration and launch
operations.

(C) Provide NASA insight as defined in Article C25, to schedule meetings, test
briefings, and technical meetings. Upon request, the Contractor shall provide
copies of schedules, test briefings, and other material presented at technical
meetings

(D) Conduct launch vehicle/launch site walk-downs with NNC participation
(E) Comply with the submittal and operational requirements for all NASA provided

facilities occupied during launch vehicle processing (CDRL C1-5). Failure to
comply may result in denied access to the NASA provided facility.

2.4.1.2 Telemetry Data and Launch Countdown Support

D1A-19


Section C NASA Launch Services II (NLS II)

Contract Terms and Conditions Contract NNK10LB801B
IDIQLSTOs
Limited Launch
CLIN Mission Quantity Launch Date/Launch
Period* Period
TBD TBD TBD TBD TBD

Indicates whether or not the mission has a limited launch period due to specific Planetary, Lunar, Scientific,

and/or Lunar Exclusion requirements

18.2

19.0

19.1

19.2

Table C-4: IDIQ LSTO Delivery Schedule
Reserved
ADJUSTMENTS TO LAUNCH SCHEDULE

NASA/Contractor will give written notice of any desired change in the launch schedule
as soon as possible. In the case of a request for postponement of the launch date by
NASA/Contractor, NASA/Contractor will propose a new launch date. Within two weeks
of receipt of the written request of a launch schedule adjustment, the Contractor/NASA
will inform NASA/Contractor whether a launch opportunity exists as requested or will
propose an alternatively available launch date. NASA/Contractor will work to provide
written agreement within thirty (30) days following receipt of the Contractor's/NASA’s
proposition, and will work together to deconflict and resolve any possible Range
conflicts. If mutual agreement on the revised launch date cannot be reached due to
launch vehicle or payload readiness, resolution between the parties shall be handled
IAW the Contracts Disputes Clause.

The postponement periods for both NASA and the Contractor shall include the
applicable grace period plus any excusable delay (e.g. a “No Fault” delay as described
in section 19.9) plus an additional eighteen (18) months each. Postponements during
this period shall be subject to the postponement fees pursuant to sections 19.3 through
19.6 and will be paid by the postponing party. In the event of a single postponement, or
cumulative postponements for each launch service by NASA/Contractor exceeds
eighteen (18) months in addition to any applicable grace period or excusable delay, the
contract shal! be subject to equitable adjustment for that portion of delay exceeding
eighteen (18) months. Any amounts owed by the postponing party as equitable
adjustment shall be in addition to the maximum postponement fees for the eighteen (18)
month delay, and/or other available remedies provided for under contract Section C,
Clause 28.0, Advance Understanding Regarding Termination Settlement Under FAR
52.212-4(l), and contract Section C, Clause 1.0(m), Termination for Cause.
Alternatively any delay declared by NASA, which results in a launch date later than the
contract period of performance shall be subject to an equitable adjustment.

C-32