Section D

Attachment D1: Exhibit 1 (F9) NNK10LB028

6.0 MECHANICAL INTERFACE
The following drawings show the mechanical interface for the Falcon 9 payload
separation system. This is a 6-point, 52.6 inch diameter separation system.

SpaceX will provide, per the Statement of Work, a test launch vehicle adapter and

separation system when required for testing and training on separation system
operations. Provision of a test adapter is a standard service in the NLS contract.

Exhibit 1 (F9) - 29


Section C J
Contract Terms and Conditions NNK10LB02B

25.8

(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.

(l) 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.

(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.

c-~40


Section D

Attachment D1: Exhibit 2 NNK10LB02B
SOW Launch Vehicle Requirements Summary
Para. #

K Provision of a payload protective cover for use after payload mate to the launch vehicle, if
the fairing is installed at the launch pad: The cover shall be. purged with conditioned air
meeting the minimum requirements stated in the SOW, paragraph 2.4.2.3(C). Provisions
shall be made for payload personnel ingress and egress.

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.

‘

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

A Payload/Vehicle Integration Environment (see SOW for description)

B Transportation Environment (see SOW for description)

Cc Fairing Environment (see SOW for description)

[e) Fairing Internal and Payload Adapter Surface Cleaning (see SOW for description)

E Reserved

F Clean Room Garments (see SOW for description)

G Materials (see SOW for description)

2.4.2.4 Operational Support Services (see SOW for description)

24.3 Range Support and Services (see SOW for description)

2.5 Safety, Reliability, and Quality Assurance

2.5.4 | Safety and Health Program (see SOW for description)

2.5.2 Reliability Program (see SOW for description) _

2.5.3 Quality Assurance Program (see SOW for description)

2.6 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.

Exhibit 2 - 8


Section D

Attachment D1: Statement of Work (F9) ; NNK10LB02B
4.0 MISSION UNIQUE REQUIREMENTS 31
44 Mission Unique Hardware . 31
4.2 Mission Unique Software... 32
4.3 Unanticipated Mission Unique Services .. 32
5.0 SPECIAL TASK ASSIGNMENTS .............cscsssssssssssseenseeesenesesseesereesseseenenses 32
6.0 INFORMATION TECHNOLOGY SECURITY..

7.0 GUIDELINE DOCUMENTS .............csssssesssesessesessseeenensseeecsseessnenenensnenenseees 33
8.0 RESERVED..

Statement of Work (F9) - 2


Section C
Contract Terms and Conditions NNK10LB02B

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.

(ii) The Government may issue a demand for payment to the
Contractor upon finding a debt is due under the contract.

(iii) Final decisions. The Contracting Officer will issue a final
decision as required by 33.211 if—

(A) The Contracting Officer and the Contractor are unable to
reach agreement on the existence or amount of a debt
within thirty (30) days;

(B) 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

(C) The Contractor requests a deferment of collection on a
debt previously demanded by the Contracting Officer
(see 32.607-2).

(iv) If 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) The date fixed under this contract.
(B) 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) The date on which the designated office receives
payment from the Contractor;


Section D
Attachment D3: Supplemental Data Requirements List

NNK10LB02B
SDRL S1-1 Data

Request B Y Q L /

(F) Temperature _

| (G) Hazardous Capability ~~ ~~

03-6


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B

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.

7.0 GUIDELINE DOCUMENTS

The following documents are to be used as guidelines to the extent specified in
this SOW. If a 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 tSO
9001:2000 to Computer Software

ISO 19011 2002 Guidelines for Quality And/Or Environmental Management
Systems Auditing

MIL-STD-1553' BB Digital Time Division Command/Response Multiplex Data
Bus

MIL-STD-1540 Borc Test Requirements for Launch, Upper-Stage, and Space
Vehicles

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- D Product Cleanliness Levels and Contamination Control

CC1246 2002 Program

Statement of Work (FQ) - 33


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

2.5

2.5.1

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.

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 the applicable launch processing site. 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
tepresentative 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

Statement of Work (F9) - 28


Section B
Table of Contents NNK10LB02B

SECTION B
STANDARD FORM 1449 CONTINUATION

TABLE OF CONTENTS

SCHEDULE OF SUPPLIES AND/OR SERVICES TO BE PROVIDED... B-1
RESCNVED... 0. cece ceeeetceeneee cee eee cee eeeeeeeeeeeeceeerenereeeeereseneeeeeseeeates
Reserved.....

Reserved..
Reserved.....

Special Task Assignment (Studies and Analyses).
IDIQ Launch Service Task Order (LSTO)....
NTE Prices - Standard Launch Services for IDIQ Missions....
NTE Prices - Non-Standard Services for IDIQ Missions

Bana wa ap
ONAOAWNA/O

2.0 TOTAL AWARD AMOUNT... B-15

3.0 RESERVED....
3.1 Reserved..
3.2 Reserved..
3.3 Reserved..

4.0 MOST FAVORED CUSTOMER... B-15

5.0 IDIQ LAUNCH SERVICE AND PRICE UPDATES... B-15



Section D

Attachment D1: Statement of Work (F1/Fie) NNK10LB02B

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
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- D Product Cleanliness Levels and Contamination Control

CC1246 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

Statement of Work (F1/F1e) - 32


Section C
Contract Terms and Conditions NNK10LB02B

32.3

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 shail 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.

c~49


Section D
Attachment D1: Exhibit 1 (F9)

NNK10LB02B

BM
Qelacked \

ts entirety |

Exhibit 1 (F9) - 34


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

3.0

4.0

41

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 shail 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.

Statement of Work (F9) - 31


Section C

Contract Terms and Conditions NNK1 OLBO2B
nfstoc.htm Homepage
http://procurement.ksc.nasa.gov/clauses.htm KSC Standard Unique

Clauses
38.0 RESERVED
39.0 SPECIAL UNDERSTANDING REGARDING DAMAGE TO GOVERNMENT

40.0

41.0

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 shail reimburse the Government for the cost of
spacecraft repairs as well as any costs associated with launch delays as set forth
in the Section C, Clause 19.0, entitled “Adjustments to Launch Schedule.” After
intentional ignition, the provisions of Contract Section C, clause 24.0 shall apply.

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 shail 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. Sucha
Government-caused delay to the subject mission shall be subject to the
contract's changes clause.

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.)

C60


Section D -
Attachment D1: Exhibit 3 (F1/Fie) NNK10LB02B

25.0

26.0
26.1

26.2

26.3

26.4

27.0
27.1

BY |

TDRSS Compatible Telemetry System
Design, build, qualify, integrate and test a TDRSS compatible telemetry
system in the Launch Vehicle. After first flight, the TDRSS compatible
telemetry system will be a standard launch service capability provided for
NASA missions.

\for IDIQ at this time but can be evaluated as a mission
unique service.

Extended Integration Periods - Order B{{ ATP

BY Extended Integration Period
This non-standard service provides for the standard launch services
beginning BU No additional services

above and beyond the standard services are covered by this non-standard
service.

Extended Integration Period
This non-standard service provides for the standard launch services

beginning a No additional services
_ above and beyond the standard services are covered by this non-standard
service. ‘
BY _.... Extended Integration Period
This non-standard service provides for the standard launch services
beginning - . “, No additional services

above and beyond the standard services are covered by this non-standard
service. :

Ry Extended Integration Period
This. non-standard service provides for the standard launch services
beginning Be . No additional

services above and beyond the standard services are covered by this non-
standard service.

Contractor Defined Non-Standard Services

SpaceX offers Falcon 1 and Falcon te launch services from
Kwajalein (a non-standard NASA launch site) as part of the standard
launch service.

Exhibit 3 (F1/F1e) - 9


Section B
Standard Form 1449 Continuation _ NNK10LB02B

proposals pursuant to Section C, Clause 14.0, and shall be subject to the written
approval of the Contracting Officer.


Section D
Attachment D1: Exhibit 1,(F9) NNK10LB028

134

Redactesl in
ts entir ety

Exhibit 1 (F9) - 30


Section D
Attachment D1: Exhibit 3 (F9) NNK10LB02B

11.7

12.0

13.0
14.0

15.0

Grade B Nitrogen spot cooling is offered with a lead time of BY
before taunch. BY
sic BiReS C Nitrogen (GN2) law MIL-PRF- -27401F Purge System

Enhanced PLF and PLA Cleaning IAW IEST-STD-CC1246D level 500A.
The internal surfaces of the payload fairing compartment (including
Payload Adapter) shall be cleaned, certified and maintained to IEST-STD-
CC1246D Level 500A 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
1$014644-1. In lieu of fEST-STD-CC 1246D Level 500A, 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 0.5% total obscuration and
<1mg/0.1m? Nonvolatile Residue (NVR). The sampling methodology for
particulate shall be per ASTM 1216 and for Angstroms molecular
contamination per ASTM 1235 with the number and locations of samples
to be determined by the integration team.

- Certified Portable Class 7 Clean Enclosure(s) for Open PLF Access Doors

BY )
Reserved

Co-Manifested Paytoad Mission Service

coment
NASA Secondary Payload Mission Service

BY
Payload Compatibility Assessment BY r)

The Contractor shall provide a document compiling all compatibility
analyses performed on the co-manifested or secondary payload to verify
the co-manifested or secondary payload does not unacceptably impact the
primary. .The specifics of the different analyses performed will vary from
mission to mission and depend greatly on the nature of both primary and
secondary payloads. Some items which are common elements of the
document are: combined coupled loads analysis, critical clearance
analysis, interface failure modes and effects analysis, safety assessment,
combined thermal analysis, and mass properties/GN&C analysis.

SpaceX offers this as a non-standard service.

Exhibit 3 (F9) - 5


Section D

Attachment D2: Contract Data Requirements List (CDRL} NNK10LB02B
ATTACHMENT D2

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.

{tem 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 minus 1W;
Review 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
iC1-4 _ |Manifest Policy Review Contract Award As Changed 5
1-5* |Operations Documentation for Review AJR in CDRL As Changed 2

Processing in NASA Provided
Payload Processing Facilities

* Required per mission

TABLE D2-A: CDRL INDEX

D2-1



Section D

NNK10LB02B

Attachment D1: Exhibit 1 (F1/F1e)

RY
Redacted ~

ts entirety

Exhibit 1 (F1/F1e) - 41


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B

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.

D2-21


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

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,
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, shail be included in the standard faunch service.

Statement of Work (F9) - 7


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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 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.

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

D2-12


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B8

(D)

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 shail provide verification of the following items at
the MSCDR:

(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 shail 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
Tesult of new flight data;

Statement of Work (F9) - 13


Section D

Attachment D3: Supplemental Data Requirements List zi NNK10L802B
SORL DESCRIPTION Number: S3-2
Reserved

D3-16


Section D

Attachment D1: Exhibit 2 NNK10L8028

EXHIBIT 2

STANDARD LAUNCH SERVICES LIST

The Contractor shall provide the following as part of their standard launch service.
These services shall be performed for each mission in accordance with the contract
terms and conditions. Each item shall include all hardware, software, analyses, and
support required to perform the service. All capabilities and conditions in Exhibit 1 that
pertain to the services listed herein shail apply.

sow Launch Vehicle Requirements Summary
Para. #
| 2.1 Launch Vehicle _ ”

A . . _ —_ —

(i) Launch periods as small as TBP days in duration (see SOW for description)

(ii) Multiple approximately twenty-four (24) hour re-launch attempts in the event of a launch scrub

(i) Instantaneous faunch window ~—
im) Inertial targeting overa BY ‘launch window utilizing multiple discrete or continuous
targeting

NIA Mission Planning for missions extending beyond 45 minutes (GTO and interplanetary)

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.

Cc A payload separation system with the following characteristics (see SOW for description)

Hl {

{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.

(iv) Redundant payload separation indications. ~

[°)

Exhibit 2 - 2



Section D -
Attachment D1: Exhibit 1 (F1/F1e) _ NNK10LB02B

RY

R od acted in |
ks onic ely -

Exhibit 4 (F1/F1e) - 33


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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

A quick look post-flight analysis or briefing will be submitted or performed no later than
L+30 days.

D2-45


Section D '
Attachment D1: Exhibit 1 (F1/Fte)

NNK10L8028

RY

Redacted (n
its a nihice fy

Exhibit 1 (F1/Fte) - 22


Section C
Contract Terms and Conditions NNK10LB02B

(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 Il (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.0.’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).

X (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).

X = (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) (314 U.S.C. 3332).

(41) 52.239-1, Privacy or Security Safeguards (Aug 1996) (5 U.S.C.
562a).

(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.

C-55


Section D

Attachrient D1: Exhibit 2 ‘et NNK10LB02B

[sow

[ Launch Vehicle Requirements Summary

| U

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

2.4.2.4

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.

Exhibit 2 - 6


Section D

Attachment D2: Contract Data Requirements List (CDRL' NNK10LB02B
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.

(DB) A llisting of all ground and mobile telemetry station locations and space based
telemetry assets.

(E) An electronic copy of respective antenna patterns with Theta, 6, having
values from zero (0) to one hundred eighty (180) degrees and Phi, 9, 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, which must capture all information presented in the sample
figure below (see Figure D2-1).

D2-40


Section B
Standard Form 1449 Continuation NNK10LB02B

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

B-15,1 Modification 002


Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
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)

}

D3-2


Section C
Contract Terms and Conditions NNK10LB028

3.3

3.4

4.0
41

4.2
43

44

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 Availablity

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 Jeast 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
Reserved
Reserved
(A) Reserved
(B) Reserved
(C) Reserved

(D) Reserved

C-12


Section D +
Attachment D1: Exhibit 1 (F9) “ NNK10LB02B

2 BY >

te eee es Peers wot woe te

3.0 INSERTION ACCURACIES

SpaceX provides the following - insertion accuracies for. the Falcon 9 vehicle
configuration. These values:have not been verified by multiplé operations at the time of
the submittal of this proposal. Per the NASA RFP, the orbital parameters | in the following
table are examples for consideration.

Required 3-Sigma Insertion Error Limit Magnitude

Variable Accuracy
Inclination Y -
Argument of Periapsis RB Uf
Right Ascension of Ascending Node q
Apogee : ‘
Perigee

Right Ascension of Launch Asymptote
Declination of Launch Asymptote
C3

Table D1- H: Falcon 9 Standard Insertion Accuracy Requirements

BY

Exhibit 1 (F9) - 24


Section D
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

2.2.3

2.2.4

2.2.5

2.3

2.3.4

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 €1-4 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.

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.

Statement of Work (F1/F1e) - 16


Section C
Contract Terms and Conditions NNK10LB028

7.4

75

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.

(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 shail 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.

C-19


Section D
Attachment D1: Exhibit 1 (F9) . 7 NNK10L802B

BY

Redacted iva\
\\s entirety

Exhibit 4 (F9) - 50


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10L802B

N
CDRL DESCRIPTION Number: C3-2 (cont)

4.2

a)

b)

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

An initial investigation by the Contractor is required for all mishaps which
have been reported 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 :
Attachment D1; Exhibit 1 (F9) ; NNK10LB02B

RY

Redacted WA

Exhibit 1 (F9) - 46


Section D “ ot
Attachment D1: Exhibit 1 (F4/F1e) sg. NNK10LB02B

BY

Redacled in
ia \ ts EN very

Exhibit 1 (F1/F1e) - 8


Section D
Attachment D3: Supplemental Data Requirements List NNK10LB02B

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

D3-13


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
3.3.2 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
3.3.3 Ascent Pressure

3.3.4 Dynamics
3.3.4.1 Sine Vibration
3.3.4.2 Acoustics
3.3.4.3 Shock
3.3.5 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 RE Transmitter/Receiver Systems EMC
3.3.5.6 Lightning

3.3.5.7 SC/LV Interface Electrical Bonding
3.3.6 Mission Satisfaction Kit

3.4 Flight Design

D2-14


Section C

Contract Terms and Conditions NNK10LB02B

(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 right 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
tesponsible for designing, fabricating, and installing a secondary payload
mass simulator.

(B) Delays

(C)

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.

29.4 NASA Secondary Payload on a Non-NASA Primary Payload

(A)

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

C45


om,

Section D
Attachment D1: Exhibit 3 (F1/F1e) . NNK10LB02B

20.5

20.6

20.7

20.8

20.9

20.10

20.11

20.12

20.13

20.14

20.15

Coupled Dynamic Loads Analysis

This can be procured at any time by the customer up until BY - ‘and
will require BY to complete. SpaceX assumes format is per the NLS
ll RFP CDRL.

Pre-Flight Controls and Stability Analysis

This can be procured at any time by the customer up until BY ‘and
will require RY ‘to complete. SpaceX assumes format is per the
NLS II RFP CDRL. .
Integrated Thermal Analysis

This can be procured at any time by the customer up until BY and
will require BY to complete. SpaceX assumes format is per the
NLS RFP CDRL.

RF Link Analysis . :

This can be procured at any time by the customer up until BY and
will require BY "to complete. SpaceX assumes format is per the
NLS Ii RFP CDRL.

Payload Fairing Clearance Analysis

This can be orocured at any time by the customer up until BY and
will require (34 to complete. SpaceX assumes format is per the
NLS If RFP CDRL.

Payload/Expended Stage Separation Analysis

This can be procured at any time by the customer up until BY ~ .and
will require BY sto complete. SpaceX assumes format is per the
NLS II RFP CDRL.

Analysis of ECS flow impingement on payload surfaces

This can be procured at any time by the customer up until BY” \and
will require BY to complete. :
RF Resonance Analysis to determine maximum RF field strengths that
payload and launch vehicle avionics would be exposed to if spacecraft RF
transmission systems where activated while encapsulated within the

fairing.

By \
Advanced mission performance analysis support (limited feasibility
assegpments in response to new mission concepts)

Launch vehicle Collision Avoidance (COLA) trajectory and covariance
data.

Launch vehicle flight software code and associated documentation.

Exhibit 3 (F1/F1e) - 7


Section D

Attachment D1: Exhibit 1 (F9) NNK10LB02B
Table D1-J2: Falcon 9 Launch Vehicle RF System Characteristics. This table does
not include path loss .39
Table D1-K: = Maximum Flight-Level Payload Acoustic Environment
Table D1-L: = Maximum Flight-Level Payload Interface Random Vibration
Environment... eceeeereeeeeeeeeseeeseeeesesceseseseteseeeneieeeneeratiseseeseee eee 43
Table D1-M: Maximum Flight-Level Payload Interface Shock Response Spectrum 44
Table D1-N: — Falcon 9 Payload Design CG Limit Load Factors... . +47
Table D1-O: Maximum Expected Sinusoidal Vibrations at the Base of the PA sane
Contractor-Provided Payload Environment Instrumentation ...............

Table 01- P:

Exhibit 1 (F9) - 4


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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.

D2-17


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

clean room rated at or above Class 8 IAW ISO14644-1. 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.

(E) Reserved

(F) 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 personne! safety operating standards
as specified in the mission specific contamination control plan.

(G) Materials. All materials used in areas in close proximity to the payload shalt
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 payioad/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 $1-1).

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

Statement of Work (FQ) - 27


Section C

Contract Terms and Conditions NNK10LB028
Launch Service Payment Schedule
Milestone/ Payment(s) Amount Cumulative Termination for
Commercial | Months Before (% of Amount of Convenience of
Interim / After Launch’ | Launch Launch the Government
Payment Service Service Repayment
No. ances {insert | CLIN Payments Schedule —
‘the left containing Price) ($) Percentage (%)
invoice submission on - of Cumulative
scoters tng | Payments Made
left containing to Date to be
individual dollar Returned to
amounts
Government
1 Lx"? L-30 10 TBD TBD (50-100) /
50
2 L-27 5 TBD 50
3 L-24 5 TBD 50
4 L-21 10 TBD 50
5 L-18 10 TBD 50
6 L-15 10 TBD 50
7 L-12 10 TBD 50
8 L-09 5 TBD 50
9 L-05 5 TBD 50
10 L-02 10 TBD 50
11 Launch * 10° TBD -
12 Launch +03 ° 10° TBD —

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 tight 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 RESP. 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 jaunch service price unless specified in the
RLSP.

> The Contracting Officer will either approve the final payment (Launch+ 03M) within
thirty (30) days after receipt of the Final Flight Report, (CORL 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.

C-15


Section C
Contract Terms and Conditions NNK10L802B

31.1

31.2

31.3

31.4

32.0
32.1

32.2

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. “Controiling
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.

Definitions:

C-48


Section D aon
Attachment D1: Exhibit 1 (F1/F1e) etl NNK10LB802B

BY

Redacted a |
its ennicety

Exhibit 1 (F1/F1e) - 34


Section D .
Attachment D2: Contract Data Requirements List (CDRt) NNK10LB02B

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
3.3.1.1 SC Thermal Environments

02-13


* Section D

Attachment D1: Exhibit 1 (F1/Fie) ; « NNK10LB02B

Exhibit 1 (F1/F1e) - 40


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
CDRL DESCRIPTION Number: C3-2 (cont)
2. NASA MISHAPS:
Classification | Property Damage Injury
Level &
{Investigation
Type
Total direct cost of mission failure and | Occupational injury and/or itlness that
property damage is $1,000,000 or resulted in:
more,
or A fatality,
Crewed aircraft hull loss has or
Type A occurred, or A permanent total oisabity,
Mishap Occurrence of an unexpected aircraft | The hospitalization for inpatient care of 3
departure from controlled flight or more people within 30 workdays of the
(except high performance jet/test mishap.
aircraft such as F-15, F-16, F/A-18, T-
38, OV-10, and T-34, when engaged
in flight test activities).
Total direct cost of mission failure and | Occupational injury and/or illness has
property damage of at least $250,000 ; resulted in permanent partial disability.
Type B but less than $1,000,000. or
Mishap The hospitalization for inpatient care of 1-
| 2 people within 30 workdays of the
| mishap.
Total direct cost of mission failure and | Nonfatal occupational injury or illness that
Type C property damage of at least $25,000 caused any workdays away from work,
Mishap but less than $250,000. restricted duty, or transfer to another job
beyond the workday or shift on which it
occurred.
| Total direct cost of mission failure and | Any nonfatal OSHA recordable
Type D property damage of at least $1,000 occupational injury and/or iliness that
Mishap but less than $25,000. does not meet the definition of a Type C
mishap.
An event in which there is no An event in which there is no injury or
equipment/property damage or minor | only minor injury requiring first aid, but
Close Cail equipment/property damage (less which possesses a potential to cause a
than $1000), but which possesses a mishap.
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

D2-23



Section D

Attachment D1: Statement of Work (F1/F1e)

(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.

(L) 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. :

(M) Manage the design, development, qualification, testing and integration of
mission unique requirements.

(N) Evaluate the capability of the launch vehicle and define any performance
and payload volume the Contractor may make available to NASA for
secondary payloads.

(O) Provide mission's tatus to NNC throughout the launch campaign from
Authority to Proceed (ATP) through mission success determination.

(P) Provide appropriate representation and participation at NASA conducted
Ground Operations Working Groups (GOWG's) approximately 2 times a

Statement of Work (F1/F1e) - 17

NNK10LB02B


* Section D

Attachment D1: Exhibit 1 (F1/F1e) ; ‘at NNK10LB02B_

R4

Reladlel oy”
bs she

Exhibit 1 (F1/F1e) - 11


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B

Provide a mechanism to incorporate new launch services, technology
upgrades, improved systems engineering processes, and advances in
manufacturing techniques.

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.

Statement of Work (F9) - 5


Section D
Attachment D1: Exhibit 2 NNK10LB02B

SECTION D
ATTACHMENT D1
EXHIBIT 2

STANDARD LAUNCH SERVICES LIST
Falcon 1, Falcon te and Falcon 9

Exhibit 2 - 1


Section C

Contract Terms and Conditions NNK10LB028

(B

(Cc

)

submission of the 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.

C-25


SECTION D
ATTACHMENT D1
STATEMENT OF WORK

FALCON 1 and FALCON 1e


Section B

Standard Form 1449 Continuation NNK10LB02B
NON-STANDARD SERVICE ITEM (Falcon 1 & 1e) NOT TO EXCEED (NTE) PRICE ($} IN CALENDAR YEAR ORDERED*
item description 2010 (Jul-Dec) 2044 2042 2043 2014 2045 2046-2022
205 Coupled Dynamic Loads Analysis TBP

206 Pre-Flight Controls and Stability Analysis

20.7 integrated Thermal Analysis
20.8 RF Link Analysis

20.9 Payload Fairing Clearance Analysis

20.10 Payload/ Expended Stage Separation Analysis

20.17 | Analysis of ECS flow impingement on payload
surfaces

20.12 RF Resonance Analysis to determine maximum RF
field strengths that payload and launch vehicle
avionics would be exposed to if spacecraft RF
transmission systems where activated while
encapsulated within the fairing

20.13 Advanced mission performance analysis support
(limited feasibility assessments in response to new

mission concepts) | ——
20.14 — | Launch Vehicle Collision Avoidance (COLA) trajectory C TSP
and covariance data >
20.15 | Launch vehicle flight software code and associated TEP
documentation |
aA Reserved
22 NASA Public Affairs Office Support B ff 2 TBP
3 Caunch Service Contractor (LSC) provided Telemetry TBP
—_—_
24 Launch Service Contractor (LSC) provided Telemetry TBP
Acquisition Assistance Message (AAM) / BY
25 | TORSS Compatible Telemetry System 5 TBP
2 Extended Integration Periods (assumes extended mis:
26.41 Three Month Extended integration Period TeP



Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B

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) Describe the models, methodology and forcing functions used.

(B) The flight events and conditions that cause the greatest loads on the payload shail
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).

(D) Worst-case payload fairing dynamic relative deflections shall 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 B
Standard Form 1449 Continuation NNK10LB02B

1.6

Table B-7: Reserved

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
Attachment D1: Exhibit 3 (F1/F1e) NNK10LB02B

147

12.0

13.0

14.0

15.0

16.0

Enhanced PLF and PLA Cleaning IAW IEST-STD-CC1246D level 500A.
The internal surfaces of the payload fairing compartment (including
Payload Adapter) shall be cleaned, certified and maintained to IEST-STD-
CC1246D Level 500A 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 [AW
1S014644-1. In lieu of IEST-STD-CC1246D Level 500A, 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 0.5% total obscuration and
<1mg/0.1m? Nonvolatile Residue (NVR). The sampling methodology for
particulate shall be per ASTM 1216 and for Angstroms molecular
contamination per ASTM 1235 with the number and locations of samples
to be on by the integration team.

i
Certified Portable Class 7 Clean Enclosure(s) for Open PLF Access Doors

BY

-Reserved

Co-Manifested Payload Mission Service

NASA Secondary Payload Mission Service
\

Payload Compatibility Assessment

The Contractor shall provide a document compiling all compatibility
analyses performed on the co-manifested or secondary payload to verify
the co-manifested or secondary payload does not unacceptably impact the
primary. The specifics of the different analyses performed will vary from
mission to mission and depend greatly on the nature of both primary and
secondary payloads. Some items which are common elements of the
document are: combined coupled loads analysis, critical clearance
analysis, interface failure modes and effects analysis, safety assessment,
combined thermal analysis, and mass properties/GN&C analysis.
SpaceX offers this as a non-standard service. Order AY :

Secondary Payload Mission Feasibility Study

A secondary payload mission feasibility study shall assess the
performance capability and payload volume available to accommodate
secondary payload missions on a non-interference basis with a given
primary mission. Separating and non-separating secondary payloads shall
be accommodated as a non-standard service.

SpaceX offers this as a non-standard service. Order BY

Exhibit 3 (F1/F1e) - 5


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

2.5.2

2.5.3

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.

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 |SO
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 shail be
notified within five (5) business days (CDRL C3-3).

The Contractor shall maintain a Software Assurance Program using [SO 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).

Statement of Work (F9) - 29


Section D
Attachment D1: Exhibit 9 NNK10LB02B

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

Exhibit 9 - 1


Section C

Contract Terms and Conditions NNK10LB02B

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

10.0 RESERVED

11.0 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

12.0

(b)

(c)

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.

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.

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)

(b)

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.

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

12 Launch Services or;

C-22


Section D
Attachment D1: Exhibit 1 (F1/F1e) NNK10LB02B

~ / EXHIBIT 1

(

ra

FALCON 1 and FALCON te CAPABILITIES, SPECIFICATIONS AND
ENVIRONMENTS
Exhibit 1 represents the capabilities, specifications, and environments of the proposed
launch services, including all standard launch service and non-standard services.

.1.0 VEHICLE CONFIGURATION

The Contractor shail define (in Table D1-C) the vehicle, Solid Rocket Motor (SRM),
upper stage, Payload Adapter (PA), and Payload Fairing (PLF) configuration options
available for each proposed vehicle class. These configurations shall inctude all
standard electrical systems, mechanical. systems, propulsion systems, ordnance
devices, and flight instrumentation.

Vehicle Falcon 1: The Falcon 1 first stage uses a single Merlin 1C
Configuration engine which burns LOX/RP-1 and generates 78,000 Ibf thrust
(sea level). The engine does not have the ability to be
throttled. The overall length of the Falcon 1 first stage
propellant tank is 402 inches.

SRM ~~ | Not Applicable (N/A)
Configuration
Upper Stage Kestrel 2 (K2)

Payload Adapter | The 38.81 inch sixty-point payload attach fitting is provided for
S/C mounting and the 38.81" motorized LightBand separation
system. Carries an electrical connector(s) that provide
separation indication through primary and redundant
breakwires. Separation initiated by electrical command to
motorized release mechanism with springs integrated to
provide delta-velocity.

5 foot (1.5m) diameter — length (11.3 feet {3.5m])

Payload Fairing

|
Z BY ~~
| ne ! '
i SRM _ | Not Applicable (N/A)
Cc. Configuration

Exhibit 1 (F1/F1e) - 5


Section C

Contract Terms and Conditions NNK10LB02B
X = (19) 52.222-3, Convict Labor (June 2003) (E.0. 11755).
X= (20) 52.222-19, Child Labor-Cooperation with Authorities and
Remedies (Aug 2009) (E.0. 13126).
X = (21) 52.222-21, Prohibition of Segregated Facilities (Feb 1999).
X = (22) 52.222-26, Equal Opportunity (Mar 2007) (E.O. 11246).
X = (23) §2.222-35, Equal Opportunity for Special Disabled Veterans,
‘ Veterans of the Vietnam Era, and Other Eligible Veterans (Sep 2006)
(38 U.S.C. 4212).
X = (24) 52.222-36, Affirmative Action for Workers with Disabilities (Jun
1998) (29 U.S.C, 793).
X = (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). .
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).


Section C
Contract Terms and Conditions NNK10LB02B

place, if benefits therefore are either payable or required to be provided under
any workmen's compensation or occupational disease law;

(vi) Shall not apply to any claim resulting from a nuclear incident occurring
outside the United States;

(vii) 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

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

(f) 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 behaif 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.

(g) 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.

(h) 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.

(i) Civil penalties. The contractor and its subcontractors and suppliers who are
indemnified under the provisions of this clause are subject to civil penalties,

C43


OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24 & 30

SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS

+, REQUISITION NUMBER = {PAGE 1 OF 1

Same as Block 9.

OP-LS

. CONTRACT NO. 3. AWARDIEFFECTIVE 4. ORDER NUMBER 5. SOLICITATION NUMBER 8 SOLICITATION ISSUE
DATE DATE
NNK10LB02B 7 RFP10-99-0021 Rev D | October 18,1999
7. FOR SOLICITATION a, NAME > TELEPHONE NUMBER (No collect calls) [8 OFFER DUE DATEMLOCAL TIME
INFORMATION CALL Steven B. Peterson 321-867-5632 10/19/2009
9 ISSUED BY q OP-LS 10 THIS ACQUISITION IS 11. DELIVERY FOR FOB DESTINATION
UNLESS
NASA John F. Kennedy Space Center 2] unrestricteo stock is marKeo [_] see
SCHEDULE
Procurement Office, Mail Code: OP-LS SET ASIDE: % FOR 12, OFFER ACCEPTANCE PERIOD
Attn: Steven B. Peterson, Room 3144C SMALL BUSINESS 180 Days from Date in Block 8
Kennedy Space Center, Florida 32899 SMALL DISADVANTAGED [| EX]134, THIS CONTRACT IS A RATED
BUSINESS ORDER
BIA) UNOER DPAS (15 CFR 700)
74, METHOD OF SOLICITATION sic: 3764 138. RATING
Clara Ors  DBdaee [Jaro SIZE STANDARD: 1000 Do.c9
15, DELIVER TO CODE 16. ADMINISTERED BY

a

Same as Block 9.

1 Rocket Road Hawthorne California 90250
[TELEPHONE NO. (310) 363-6229

7a. CONTRACTOR? PPC/STATE FACIIT 7
Wa, CONTRAG STATE | C0) ] aur 3VBL8_ |'8# PAYMENT WiLL BE MADE B or)
Space Exploration Technologies DUNS—~120406462 NASA Shared Services Center (NSSC)

Financial Management Division (FMD) — Accounts Payable
Bldg 1111, C. Road

Stennis Space Center, MS 39529

Email: NSSC-AccountsPayable@nasa,gov

Fax: 866-209-5415

17b. CHECK IF REMITTANCE IS DIFFERENT ANO PUT SUCH
ADDRESS IN OFFER

186. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a. UNLESS
BLOCK BELOW IS CHECKEO SEE ADDENDUM

19. 20.
ITEM NO. SCHEDULE OF SUPPLIES/SERVICES

24.

2 22. 23.
QUANTITY UNIT. UNIT PRICE AMOUNT

WITH SECTION B, C AND D.

(Attach Additional Sheets as Necessary)

NASA LAUNCH SERVICES IN ACCORDANCE

Ps. ACCOUNTING AND APPROPRIATION DATA

28. TOTAL AWARD AMOUNT (For Govt, Use Only}

ADJo7a_ SOLICITATION INCORPORATES IN FULL TEXT FAR 52 212-1, 52.212-4. FAR 52 212-9 & $2 212.5 ARE ATTACHED ADDENDA [XJare |_lare NOT ATTACHED

Doz». CONTRACTIPURCHASE ORDER INCORPORATES IN FULL TEXT FAR 52.252-4, FAR $2 212-5 IS ATTACHED.

aonenoa [XJare [_Jare not aTTacheo

TERMS AND CONDITIONS SPECIFIED HEREIN

[X]zs. conTRACTOR IS REQUIRED [0 SIGN THIS DOCUMENT AND RETURN 3 COPIES TO
ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND DELIVER ALL ITEMS SET FORTH
JOR OTHERWISE IDENTIFIED ABOVE AND ON ANY ADDITIONAL SHEETS SUBJECT TO THE

[Teo awaR0 OF CONTRACT: REFERENCE OFFER DATED
THE OFFER ON SOLICITATION (BLOCK 5). INCLUDING ANY ADDITIONS.
JOR CHANGES WHICH ARE SET FORTH HEREIN, [S ACCEPTED AS TO

STEMS:

30a. SIGNATURE OF OFFEROR/CONTRACTOR

\a
30D. NAME AND TITLE OF SIGNER (Type or print) 30¢ DATE Jib. NAME OF CONTRACTING OFFICER (Type
. " SIGNED pring)
Julie A. Jiru, Contracts Officer .

24 Sep 10 Michael $. McCarty rt) jO
30a, QUANTITY IN COLUMN 21 HAS BEEN 35, SHIP NUMBER "34, VOUCHER 35, AOU!
Qreceveo Cyinspectep () ACCEPTED, AND CONFORMS TO THE Cipartiat (] FINAL NUMBER VERIFIED

CONTRACT, EXCEPT AS NOTED CORRECT FOR
320. SIGNATURE OF AUTHORIZED GOVT. REPRESENTATIVE Bic DATE 36, PAYMENT 37, CHECK
Cicometere (Jeartar [J rinat NUMBER
38. SIR ACCOUNT NO. 38. SIR VOUCHER NO. 40, PAID BY

42a. RECEIVED BY (Print)

‘4ia_ 1 CERTIFY THIS ACCOUNT IS CORRECT AND PROPER FOR PAYMENT

4p. SIGNATURE AND TITLE OF CERTIFYING OFFICER 4c. DATE

426. RECEIVED AT (Location)

42c. DATE REC'D
(rv)

‘42d, TOT. CONTAINERS

"AUTHORIZED FOR LOCAL REPRODUCTION

A-2

"STANDARG FORM 1449 (10-55)
Prescaibed by GSA - FAR (48 CFR) 53.212



Section D :
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

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 real-time launch vehicle and GSE telemetry (RF and
hardwire) data to the NASA designated NASA LSP Data Center. Examples
include, but are not limited to telemetry test data during initial vehicle power-up,
flight simulation prior to payload mate, and flight simulation following payload
mate (SDRL S6-3).

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 tater than sixty (60)
days prior to !aunch. 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 shail 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.

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.

Statement of Work (F1/Fte) - 21


Section D

Attachment D1: Exhibit 1 (Fue) : NNK10LB02B
—- any
+—- OK .
MY —/
CO Cp/
—_{~.
c o> Ce
a
~ — o>
m
4 >
<

Exhibit 1 ‘"*/F1e) - 26


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B8

2.2

2.2.1

(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 shail 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.

Statement of Work (F9) - 10


O

oN

A

Section D

Attachment D1: Exhibit 1 (F1/F1e) : NNK10LB02B

Table D1-c:

Table D1- G3b:

Table D1- H:
Table D1- I:
Table D1- J:
Table D1-J1a:

Table D1-J1b:
Table D1- Ka:

Table D1- Kb:
Table D1-La:

Table D1- N:
Table D1- 0:

Table D1- P:

LIST OF TABLES

Vehicle Configurations ...........secseeeceeecsicenieeesnneeesseesseeecsneee tease 6

‘Table D1- G3a: Maximum Payload Capability for Direct Insertion into GSO for Falcon 1

Vehicle Configuration .............cccecccceicseceseetsescsecserensescseteeanseseetaeeee 19
Maximum Payload Capability for Direct Insertion into GSO for Falcon
Te Vehicle Configuration... ccc cccccceeee cece ceecenetersesetenennseesnaees
Falcon 1/1e Standard Insertion Accuracy Requirements.
Standard Payload Deployment Attitudes/Rates:................
Falcon 1/1e Electrical Interface Minimum Wire Requirements.
Falcon 1/1e Maximum Electromagnetic Radiation Levels Encountered
ON Payload, 2... eccccceeesesecestcsseneteseseseteeneranstseesesssetiensessestessssssstteeens 29
Falcon 1/1e Launch Vehicle RF System Source Characteristics ........ 30
Falcon 1 Maximum Flight-Level Payload Acoustic Environment
(derived from flight and test data) ....
Falcon 1e Maximum Flight-Level Payloa
Falcon 1 Maximum Flight-Level Payload Interface Random Vibration
Environment.

Falcon 1/1e Payload Design CG Limit Load Factors «00... 1.37
Maximum Falcon 1/1e Expected Sinusoidal Vibrations at the Base of
the PA .40

Exhibit 1 (F4/Fte) - 3


Section B

Standard Form 1449 Continuation NNK10LB02B

SECTION B

STANDARD FORM 1449 CONTINUATION

1.0 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)

Unit Total
Description of Price Amount
CLIN Supplies and Service Qty | Unit ($) ($)
10 | Special Task Assignments — Firm | A/R | Labor See See
Fixed-Price Composite Labor Hour Table Table
Hours B-6 B-6

Table B-5: Special Task Assignments (Studies and Analyses)


Section D .
Attachment D1: Exhibit 1 (F1/F1e) ; NNK10LB02B

BY

Redacted iA ES
entirety |

Exhibit 1 (F4/F te) - 35


Section D
Attachment D1: Exhibit 1 (F9) ad NNK10LB028

R4

R edactedl in
f = eutirely

Exhibit 1 (F9) - 11


Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
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 alt
phases of powered flight from two (2) minutes prior to stage ignition through 5
seconds after shutdown. The payload separation event from 40 seconds prior to and
5 seconds after separation shall also be included.

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

D3-28


Section D
Attachment D1: Statement of Work (F1/F1e) . NNK10LB02B

The Contractor shall providee 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. 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[” By .
B44. IAW NASA Policy LSP-PD-120.05. The
Contractor shall receive and record launch vehicle | 84

. ‘after payload separation IAW NASA Policy LSP-PD-
120.05. -

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 shalt poll N 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.

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

Statement of Work (Ft/Fte) -22


Section C
Contract Terms and Conditions NNK10LB02B

2.2

2.3

24

“25

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 shail
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.

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.

C-10


Section D
Attachment D1: Exhibit 1 (F9) t NNK10LB02B

Redac ed tn:
ies evr ety

Exhibit 1 (F9) - 13


Section D

Attachment D1: Statement of Work (F1/Fte) NNK10LB02B
3.0 NON-STANDARD SERVICES ...........cescscessssssceesesessescnenesenesseeeneeeneeneneaees 30
4.0 MISSION UNIQUE REQUIREMENTS..

41 Mission Unique Hardware.

4.2 Mission Unique Software ..

43 Unanticipated Mission Unique Services.

5.0 SPECIAL TASK ASSIGNMENTS

6.0 INFORMATION TECHNOLOGY SECURITY ..c.cccsssssssssssssssesssssesssssssssssseses 31
7.0 GUIDELINE. DOCUMENTS ...........sesesssssesesseressonencenteaeeansansansanesnesneaneanenes 34
8.0 RESERVED........2:sscsscssesscsscssessesscsstssesaeenesnessensnsessessenseneersnassesssassosenseseenses 33

Statement of Work (F1/F1e) - 2


Section D
Attachment D1: Exhibit 1 (F1/F1e) . NNK10LB02B

Bu

R ed acted (n
Es | enhiretY

Exhibit 1 (F1/F1e) - 43


Section C
Contract Terms and Conditions NNK10LB02B

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

(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:

C-65


Section B

NNK10LB02B

Standard Form 1449 Continuation
NON-STANDARD SERVICE ITEM (Falcon 9 Bik 1 & 2) | NOT TO EXCEED (NTE) PRICE ($) INCALENDAR YEAR ORDERED*
#from | lam description 2010 (Jul- 2017 2012 2013 2014 2015 2076-2022
Exhibit 3 Dec)
20.2 | Support for additonal mission integration working group TSP
meetings in excess of four per calendar year AY ate ie
20.3 | Reserved -- we ee ee TT
20.4 Performance and Guidance Accuracy Analysis TBP
20.5 | Coupled Dynamic Loads Analysis Ter |
206 Pre-Flight Controls and Stability Analysis TEP
20.7 Integrated Thermal Analysis. BY TBP
208 RF Link Analysis = ——> TBP
20.8 | Payload Fairing Clearance Analysis TEP
20.10 | Payload) Expended Stage Separation Analysis Te
20.11 | Analysis of ECS flow impingement on payload surfaces TEP
i 1 1 1 ———__-—_b. rf
20.12 | RF Resonance Analysis to determine maximum RF field TEP
strengths that payload and launch vehicle avionics would
be exposed to if spacecrafi RF transmission systems
where activated while encapsulated within the fairing
20.13 Advanced mission performance analysis support (limited TBP
feasibility assessments in response to new mission
concepts) —_—->
20.14} Launch Vehicle Collision Avoidance (COLA) trajectory a —TeP
and covariance data
20.15 | Launch vehicle fight sofware code and associated Ter
documentation
FD Reserved B {
7 NASA Public Affairs Office Support ] ZZ ———=» TEP
B Taunch Service Contractor (LSC) provided Telemetry , TEP
it i 1 L dot
% Launch Service Contractor (LSC) provided Telemetry Qf eS TEP
. Acquisition Assistance Message (AAM) ~ | :
2 TDRSS Compatible Telemetry System ] ~~ 7 “TBP

Ze

- BY¥———>


Section D
Attachment D1: Exhibit 1 (F9) NNK10LB02B

EXHIBIT 1
FALCON 9 CAPABILITIES, SPECIFICATIONS AND ENVIRONMENTS

Exhibit 1 represents the capabilities, specifications, and’ environments of the proposed
launch services, including all standard launch service and non-standard services.

1.0 VEHICLE CONFIGURATION

The Contractor shall define (in Table D1-C) the vehicle, Solid Rocket Motor (SRM),
upper stage, Payload Adapter (PA), and Payload Fairing (PLF) configuration options
available for each proposed vehicle class. These configurations shall include all
standard electrical systems, mechanical systems, propulsion systems, ordnance
devices, and flight instrumentation.

Vehicle | Falcon 9 Block 1: The Falcon 9 Block 1 first stage uses nine
Configuration | Merlin 1C engines. The Merlin 1C engine burns LOx/RP-1
and generates 95,000 Ibf thrust (sea level). The engine does
not have the ability to be-throttled.
SRM Not Applicable
Configuration _
Upper Stage _| Falcon 9 Stage 2 (powered by Merlin Vacuum single engine)
Payload The 56.2 inch six-point payload mounting and separation
Adapter system). Carries an electrical connector(s) that provide
separation indication through primary and redundant
breakwires. Separation initiated by electrical command to
non-explosive separation nuts; integral springs provide delta-
17 foot (5.2m) diameter — single length (45 feet [13.7m])

SRM [Not Applicable

Exhibit 1 (F9) -6


Section C
Contract Terms and Conditions NNK10LB02B

19.12

19.13

20.0

21.0

22.0

23.0

23.1

23.2

23.3

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, shail 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. ‘

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.

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, shail result in no increase in the price of this contract.

The Contractor is responsible for determining the suitability for use of ail
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.


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB028

(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.

D2-43


Section D

BY

Redacted | (A 7
its entiroty


Section D

Attachment D2: Contract Data uirements List (CDRL NNK10LB02B
Item Document Approval/ = Initial Submittal Subsequent No. of
Review Date Submittal Date {Copies
C3: Safety & Mission
Assurance
IC3-1__|Alert System Documentation Review Dispo + 1M AVR 2
\C3-2 _|Mishap Notification, Investigation |Review JVR in CDORL AIR 2
land Mishap Preparedness, and
Contingency Plan
IC3-3 {ISO 9001/2000 Certification Review Upon Recertification |Upon 4
Certificate (ISO 9001/2008 Recertification
\Certification Certificate after
November 2010)
C3-4 {Quality Management System Review Contract Award +45 |When Revised |2
(QMS) and SupplierVendor Days
Audit/Assessment 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 Approval for JA/R in CORL AVR
Processing In NASA Provided INASA owned
Facilities facilities;
Review for
NASA
procured
facilities

* Required per mission

TABLE D2-A: CDRL INDEX (Cont.)

02-3



Section D
Attachment D1: Statement of Work (F1/F 1e) : NNK10LB02B

2.2

2.2.1

(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 or such other locations
as defined by the ICD. At this facility, the Contractor shail support, with
necessary personnel and equipment, the following: a fit check of the payload
with the flight PA, environmental testing with a TPA (personnel support is
limited to one installation and one removal of TPA), payload shock testing
with a TPA, and sufficient pyrotechnics for two shock test firings.

(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)

Statement of Work (F1/Fi1e) - 9


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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.

e Launch Vehicle facility, processing, security, contamination requirements 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 facility.
o Initia) submittal date sixty (60) days prior to arrival.
« Non-hazardous Launch vehicle standalone procedures.
o Initial submittal date forty-five (45) days prior to use.
« Launch vehicle personnel badging and training requirements to include any
medical certifications.
o Initial submittal date ninety (90) days prior to arrival.

D2-11


Section D oe .
Attachment D1: Exhibit 1 (F1/F1e) : NNK10LB02B

B4

Redacted in
rhs en firety 7

"Exhibit 1 (F4/F te) - 29


Section D

Attachment D1: Exhibit 2

NNK10L602B

SOW
Para. #

Launch Vehicle Requirements Summary

12.4.1.2.2

)
|
|

Baseline and Integrated Vehicle Support

Exhibit 2 - 5



Section D
Attachment D1; Exhibit 3 (F1/F1e) NNK10LB02B

2.6

RF-transparent doors

SpaceX offers RF-transparent doors in lieu of or in addition to personnel
access doors as a standard service. The payload fairing supports a
maximum combination of three doors and/or RF windows. Order

3.0 Alternate Payload Adapters (PAs)
3.1 Different size or different payload interface PAs
8 ) at this time but could be handled on a mission-specific
basis
3.2 Low tip-off rate PAs
BY
4.0 Upper Stage Hardware — BY _
4.1 Motor — BY
4.2 .PA- BY
4.3. Spin system with enhanced capability — BY
4.4 Despin system with enhanced capability — 34
4.5 Improved insertion accuracy options — Q ¢/ )
5.0 Multiple PA, including Related Mission Integration Support
BU
6.0 Secondary PA for Non-Separating Secondary Payload
BY for IDIQ at this time but can be evaluated as a mission
unique service.
7.0 Secondary PA/Separation System for Separating Secondary Payload
7.1. Secondary Payload Adapter (with S/C-provided separation system)
BY for IDIQ at this time-but can be evaluated as a mission
unique service.
7.2 Secondary Payload Adapter (with contractor-provided separation system)
BY for IDIQ at this time but can be evaluated as a mission
unique service.
8.0 RF Through- -the-Fairing Transmission Capability
_ RY for IDIQ at this time but can be evaluated as a mission unique
service. *

Exhibit 3 (F1/F te) - 3


Section D .
Attachment D1: Exhibit 1 (F1/F1e) boa 7 -NNK10LB02B

BY

R edacted v,
ies entirety

Exhibit 1 (FA/F1e) - 14


Section D . :
Attachment D1: Exhibit 1 (F9) med NNK10LB02B

RY

Relacted (A :
| its ee entirely

Exhibit 4 (F9) - 41


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10L802B

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 C

Contract Terms and Conditions NNK10LB02B

(c) | 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.).

(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)).

(d) 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.

(2) The Contractor shall make available at its offices at all reasonable times the

records, materials, and other evidence for examination, audit, or

C-56


Section D : ‘
Attachment D1: Exhibit 1 (F9) : NNK10L802B

BY

Redacted in
its entirety

Exhibit 1 (F9) - 37


Section D
Attachment D1: Exhibit 1 (F9) NNK10LB02B

Ry
Redacted tn |
I Ls entirety

Exhibit 1 (F9) - 18


Section C
Contract Terms and Conditions NNK10LB02B

5.9

6.0

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.

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.

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(1)
“Termination for the Government's convenience” of this contract, the total
amount payable by the Government pursuant to contract Section C, Clause
1.0(!) 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(I) “Termination for the Government's convenience”
notwithstanding.

C-16


Section D
Attachment D1: Exhibit 1 (F1/Fte)

NNK10LB02B

4
Red acted (A
ts entirety

Exhibit 1 (F1/F te) - 25


Section D
Attachment D1: Exhibit 1 (F9) : NNK10LB02B

BY

Redacted Ov
its enti rofy

Exhibit 1 (F9) - 20


Section C
Contract Terms and Conditions NNK1GLB02B

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) Date of the task order
(ii) Contract number and task order number

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

(iv) Product or service to be delivered
(v) Task order price

(vi) Completion/Delivery date

(vii) Reserved

(viii) 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 commercia! 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.

C-28


Section D

Attachment D1: Statement of Work (F1/F1e)

NNK10LB02B

@ 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 wiil
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.

3.0 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.

4.0 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.

41 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
4.2 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

Statement of Work (F1/F1e) - 30


Section C
Contract Terms and Conditions NNK10L8028

19.8

19.9

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 shail be suspended for the length of the delay and then resumed with
all remaining 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 fromRange 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.

19.10 Once a specific launch date and time have been established, they may be

19.11

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. .

C-33


Section D

Attachment D1: Exhibit 1 (F9) NNK10LB02B

Figure D1- 1:

Figure D1- 2a:
Figure D1- 2b:
Figure D1- 2c:
Figure D1- 2d:
Figure D1- 2e:

Figure D1- 3:

Figure D1- 4:

Figure D1- 4a:

Figure D1- 5:

Figure D1- 5a:

LIST OF FIGURES

Falcon 9 5.2m [17ft] Maximum Payload Static Envelopes
Payload Adapters and Interfaces...
Payload Adapters and Interfaces..
Payload Adapters and Interfaces...
Payload Adapters and Interfaces..
Payload Interface Ring.
Falcon 9 Maximum Electromagnetic Levels Encountere!
on Payload
PLF Pressure Profiles and Depressurization Rates
Maximum Flight-Levei Payload Interface Shock Response Spectrum

(6-point, 52.6 inch diameter separation system) ............:e:eeeeeeee .44
Spacecraft Quasi-Static Acceleration (max) (Falcon 9 Block 1 and

BOCK 2)... .eeececeeesecceeeceesenseseseeeeeeeceeeececeeeeescseevsteseneeenaseceeverinesereeeees 45
Falcon 9 Payload Design CG Limit Load Factors... eee 46

Exhibit 1 (F9) - 5


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

2.2.5

2.3

2.3.1

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.

Mission Integration Services
Mission Integration Management

The Contractor shail 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 shail be
responsible for preparing and distributing agendas, minutes and action item
logs for each meeting (SDRL S$1-2). The Contractor shall maintain the action
item database and ensure closure of ail 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.

Statement of Work (F9) - 17


Section D
Attachment D2: Contract Data Requirements List (CDRL NNK10LB02B

CDRL DESCRIPTION Number: C3-3

ISO 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 !SO
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 C

Contract Terms and Conditions

NNK10LB02B

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.

xX

Title Number _Date Tailoring
Iso 9001/2000 2000 Third Party Certification

Aerospace QMS

AS9100
RevC

17.0 INSPECTION SYSTEM RECORDS

2009

Required (ISO 9001/2008
after November 2010)

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

IDIQ LSTOs
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

Table C-4: IDIQ LSTO Delivery Schedule

C-29


Section D :
Attachment D1: Exhibit 1 (F9) . I NNK10LB02B

RY
Redactel in
ibs onic FY

Exhibit 1 (F9) - 15


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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 \CD 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

D2-16




Section D
Attachment D2: Contract Data Requirements List (CDRL’ NNK10LB02B

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) A compliance 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

D2-50


Section D . to
Attachment D1: Exhibit 1 (F9) hoot NNK10L802B

RY

Redacted iy
iks entirety

Exhibit 1 (F9) - 16


Section C
Contract Terms and Conditions

NNK10LB02B

36.2

36.3

37.0

FAR 52.215-1(c)(3)
FAR 52.222-1

FAR 52.227-14
FAR 52.227-14

FAR 52.227-14

FAR 52.232-18
FAR 52.233-1
FAR 52.242-15
FAR 52.243-1
FAR 52.246-4
FAR 52.246-25

Instructions to Offerors-Competitive Acquisition (Jan
2004)
Notice to the Government of Labor Disputes (Feb 1997)

Rights in Data—General (Dec 2007)

Rights in Data—General (Dec 2007) Alternate || (Dec
2007) .

Rights in Data—General (Dec 2007) Alternate III (Dec
2007)

Availability of Funds (Apr 1984)

Disputes (July 2002)

Stop-Work Order (Aug 1989)

Changes—Fixed-Price (Aug 1987) Alternate | (Apr 1984)
Inspection of Services—Fixed-Price (Aug 1996)
Limitation of Liability—Services (Feb 1997)

NASA FAR SUPPLEMENT (48 CFR CHAPTER 18) CLAUSES:

NFS 1852.215-84

NFS 1852.219-74
NFS 1852.219-75

NFS 1852.219-76
NFS 1852.223-70
NFS 1852.223-75
NFS 1852.225-70
NFS 1852.228-75

NFS 1852.243-71

Ombudsman (Oct 2003) James E. Hattaway, Jr. at
(321) 867-7246

Use of Rural Area Small Businesses (Sep 1990)

Small, Small Disadvantaged, and Women-Owned Small
Business Subcontracting Reporting (May 1999)

NASA 8 Percent Goal (Jul 1997)

Safety and Health (April 2002)

Major Breach of Safety or Security (Feb 2002)

Export Licenses (Feb 2000) Alternate | (Feb 2000)
Minimum Insurance Coverage (Oct 1988)

Shared Savings (Mar 1997)

KENNEDY SPACE CENTER STANDARD CLAUSES

KSC 52.204-96

Security Controls for KSC & CCAFS (Apr 2010)

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):

htto:/Awww.arnet.gov/far/ GSA FAR Homepage

http://www.hq.nasa.gov/office/procurement/regs/_ NASA FAR Supplement

C-59


Section D

Attachment D3: Supplemental Data Requirements List NNK40LB02B
SDRL DESCRIPTION Number: $1-3

PROGRAM MASTER SCHEDULE AND LAUNCH VEHICLE PLANNING MANIFEST
DESCRIPTION/PURPOSE:

The contractor shalt develop and provide a Program Master Schedule to include sub-tier
schedules, production schedules, and faunch 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.

D3-14


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
CDRL DESCRIPTION Number: C2-4
Reserved

D2-19


Section D

Compliance Documents.

Attachment D1: Statement of Work (F4/F1e) NNK10LB028
ATTACHMENT D1
STATEMENT OF WORK
TABLE OF CONTENTS
1.0 INTRODUCTION .
1.1 Scope .....
1.2 Objectives
1.3
14

Reserved cvsssstusesissisvnsisivevisivinssisnssiisisinssinsisivisnisivassisessetinsen

STANDARD LAUNCH SERVICE
Launch Vehicle ............02..00.

Program Management
Formal Reviews...
Program Reviews
Design Reviews — Mission Specific
Readiness Reviews .
Risk Management...
Configuration Managemen
Manifest Policy
New Launch Vehicle Orientation.
Mission Integration Services ....
Mission Integration Management
Mission Analyses
Mission Success Determination..
Launch Site Support...
Pre-Launch Checkout and Launch Support.
Launch Vehicle Preparation and Launch
Telemetry Data and Launch Countdown Support..
Vehicle Telemetry .........00..000ecee
Baseline and Integrated Vehicle 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 Assurance
Safety and Health Program
Reliability Program............
Quality Assurance Program..
NASA Insight and Approval ..

Statement of Work (F4/F1e) - 1



Section C
Contract Terms and Conditions NNK10LB02B

13.0

(c)
(d)

36 Special Task Assignments or unlimited Non-Standard Services
exceeding the amount identified in (2)

(2) Any order for a combination of items in excess of $1,000,000,000; 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 |DIQ
contract portion only}

{a)

(b)

(c)

(d)

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 locations.

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 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;

C-23


Section’ D
Attachment 01: Statement of Work (F9) NNK10L802B

21

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

(iii) Instantaneous launch window

(iv) Inertial targeting overa’ 84. — launch window utilizing multiple
discrete or continuous targeting

BY

(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) Three payload access doors of sizes BY __], whose locations
shall be mission unique within the stated structural limitations of the
fairing. 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.

(ii) Thermal environments specified not to exceed’ __ B42 le,

during ascent on any launch vehicle component inside the
fairing with a view factor to the payload, with the exception of the upper

Statement of Work (F9) - 8


Section D
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

clean room rated at or above Class 8 IAW I1SO14644-1. In lieu of JIEST-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.

(E) Reserved

(F) 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.

(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.

F 24.2.4 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 shail 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 $1-1).

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

Statement of Work (F1/F1e) - 26


oo

Section D

Attachment D1: Exhibit 3 (F9)

NNK101.B02B

26

3.2

4.0
4
4.2
4.3
44
45

5.0 .

6.0

7.0

“74

7.2

8.0

9.0

9.1

9.2

RF-transparentdoors Order: BY ‘

SpaceX offers RF-transparent doors in lieu of or in addition to personnel
access doors as a standard service. The payload fairing supports a
maximum combination of three doors and/or RF windows.

Alternate Payload Adapters (PAs)
Different size or different payload interface PAs

BY ‘at this time but could be handied on a mission-specific
basis
Low tip-off rate PAs .

BY ‘at this time but could be handled on a mission-specific

basis :
Upper Staae Hardware -1 [34 ’
Motor -i BY ‘
PA- BY

Spin system with enhanced capability— B4 !
Despin system with enhanced capability B4
Improved insertion accuracy options— RY ww

Multiple PA, including Related Mission Integration Support
BY ‘for IDIQ at this time but can be evaluated as a mission
unique service.

Secondary PA for Non-Separating Secondary Payload
“BY ‘for IDIQ at this time but can be evaluated as a mission
unique service.

Secondary PA/Separation System for Separating Secondary Payload
Secondary Payload Adapter (with S/C-provided separation system)
B for IDIQ at this time but can be evaluated as a mission
unique service.
Secondary Payload Adapter (with contractor-provided separation system)
4 ‘for IDIQ at this time but can be evaluated as a mission
unique service.

RF Through-the-Fairing Transmission Capability
B ‘for IDIQ at this time but can be evaluated as a mission
unique service.

Enhanced Electrical interface
Increased capacity payload-to-GSE interface.
for IDIQ at this time but can be evaluated as a mission
unique service.
Launch vehicle command and control of payload

Exhibit 3 (F9) - 3


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B

2. 4. 1
2.4.1.1
2.4.1.2
2.4.1.2.1
2.4.1.2.2
2.4.1.2.3
2.4.1.3
2.4.2
2.4.2.1
2.4.2.2
2.4.2.3
2.4.2.4
2.4.3

2.5.1
2.5.2
2.5.3
26

3.0

ATTACHMENT D1

STATEMENT OF WORK
TABLE OF CONTENTS

INTRODUCTION...

Compliance Documents .
Reserved...

STANDARD LAUNCH SERVICE.
Launch Vehicle...........
Program Management
Formal Reviews....
Program Reviews .
Design Reviews — Mission Specific .
Readiness Reviews.
Risk Management...
Configuration Managemen
Manifest Policy ...............
New Launch Vehicle Orientation .
Mission Integration Services..
Mission Integration Management.
Mission Analyses... .
Mission Success Determination
Launch Site Support........0.00....
Pre-Launch Checkout and Launch Support..
Launch Vehicle Preparation and Launch.......
Telemetry Data and Launch Countdown Support .
Vehicle Telemetry... 20
Baseline and Integrated Vehicle 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 Assurance.
Safety and Health Program
Reliability Program .........
Quality Assurance Program
NASA Insight and Approval...

NON-STANDARD SERVICES...

Statement of Work (F9) - 1


Section D
Attachment D1: Exhibit 1 (F9) ; we NNK10LB02B

BH

Redacted 1A
vhs entirety

Exhibit 1 (F9) - 10


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

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 8715.37 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

1.4

2.0

1

2

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.

The Contractor shall support NASA’s compliance with this document.
Reserved
STANDARD LAUNCH SERVICE

The Contractor shail 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

Statement of Work (FQ) - 6


Section D .
Attachment D1: Exhibit 1 (F9) - NNK10LB02B8

BY
N ed acted A
chs ent rety

Exhibit 1 (F9) - 33


Section D :
Attachment D1: Exhibit 1 (F9) NNK10LB02B

Ralacted oO
Gs entirely

Exhibit 1(F9)-22 -


Section D
Attachment D1: Statement of Work (F9) NNK10LB802B

2.6

The Contractor shall provide for NASA attendance at any flight hardware reviews
the Contractor performs at Contractor or subcontractor facilities. The Contractor
shail 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 read-only quality information to NASA (via remote
terminal) from such Quality Assurance on-line database systems as exist and to
which the Contractor has regular and timely input. An example is an on-line
Problem/Failure Reporting (P/FR) system.

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

Statement of Work (F9) - 30


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B
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

Statement of Work (F9) - 34


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B8
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) Upper stage and payload adapter mission specific drawings showing all sub-tier
mission unique installations, including all payload mechanical interfaces.

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

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

(D) All schematics harness drawings, and assembly drawings for mission unique
electrical hardware.

(E) A drawing tree showing all mission specific drawings.

D2-51


Section B

Table of Contents. NNK10LB02B
LIST OF TABLES

Table B-1_ Reserved... eee ee B-1
Table B-2 Reserved... onsen eee eee ee B-1
Table B-3 Reserved... .eee esses eee e eee cee eee e ee eee ee ee B-1
Table.B-4 Reserved... eee eee ee B-1
Table B-5__ Special Task Assignments (Studies and Analyses)..................... B-1
Table B-6__ Hourly Labor Rate - FFP List... B-2
Table B-7___ Reserved... eee B-2
Table B-8___1DIQ Launch Service Task Order..........-.-. 1... ee ee B-3
Table B-9.1_NTE Price List - Standard Launch Services for IDIQ Missions

(25% tefund). oo. ee eee eee eee eee eee eee B-5
Table B-10a NTE Price List - Falcon 1 & te Non-Standard Services for IDIQ

Missions... 2... ss eee ee ee ee ee ee eee eee eee B-6
Table B-10b NTE Price List - Falcon 9 Bik 1.& 2 Non-Standard Services for IDIQ

Missions... eee B-10
Table B-11_ Reserved... ieee cceecce cee ee cee cee ee eee e eee eee eee eens B-16
Table B-12 Reserved oo... ois eee eee eee ee B-16



Section D
Attachment D1: Exhibit 1 (F9) . NNK10LB028

BY
| R ada ced i.
( f S ents ely :

Exhibit 1 (F9) - 49


Section D .
Attachment D1: Exhibit 2 NNK10LB02B

SOW Launch Vehicle Requirements Summary
Para. #

(i) Two (F1/1e) or three (F9) payload access doors of sizes (see SOW for description)

(ii) Thermal environments... (see SOW for description)

(iv) 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 (see SOW for description)
G Post mission maneuvers (see SOW for description)
{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 _ ee ee
(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).

rT A logo in accordance with NASA provided artwork (see SOW for description)
J Availability of a Test Payload Adapter (TPA) (see SOW for description)
K Command, control, and power signal capability from the launch control facility to the payload
umbilical Ground Support Equipment (GSE) !AW 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 |AW 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.

Exhibit 2 - 3


Section D :
Attachment D1: Exhibit 3 (F9) NNK10LB02B

This non-standard service provides for the standard launch services
beginning BY. earlier, at AY . No additional
services above and beyond the standard services are covered by this non-
standard service.

27.0 Contractor Defined Non-Standard Services

27.15 _ _ BY

Exhibit 3 (F9) - 10


Section D
Attachment D1: Statement of Work (F9) . NNK10LB028

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.

2.4.2.2 Launch Site Payload Integration Support

The Contractor shall provide ail 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, and payload communication
accommodations 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) Provision for contingency off-loading of payload propellants in accordance
with the appropriate Range Safety requirements and appropriate payload
procedures.

Statement of Work (F9) - 24


Section D’ .
Attachment D1: Statement of Work (F4/Fie) NNK10LB02B

2.4 Launch Site Support
2.4.1. 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 access to all meetings including, but not limited to, scheduling
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
2.4.1.2.1 Vehicle Telemetry

Telemetry data shail 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 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

Statement of Work (F1/F1e) - 19


Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
SDRL DESCRIPTION Number: S5-1
VEHICLE TEST PROCEDURES

DESCRIPTION/PURPOSE:

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

DATA REQUIREMENTS:

Launch Service Contractor (LSC) shall provide a list of all launch vehicle test or
processing procedures.

Provide upon request the following vehicle processing procedures:

The Falcon 1/1e Procedure List

Procedure
Number Description

1.10 ETS Open-loop checks
1.20 RF Checks
1.30 Range Interface Checks
1.40 1st stage Engine Alignment
1.50 1st stage TVC Performance

1.60 2nd stage TVC Functional

1.65 Stage Sep Bottle Fill

1.70 Main Valve Timing/Purge checks.

1.85 Recovery System Charging and Activation
1.90 Vehicle hold-down

1.100 Initial Pad Preps

1.105 Final Pad Preps

1.120 Countdown
2.10 Stage Deliveries
2.20 Kestrel Build Up
2.30 1st Stage Check-out
2.35 Recovery Ordnance Install
2.40 2nd Stage Check-out
2.45 Fairing/PLA Check-out
2.50 TEA-TEB Canister Installation
2.55 Interstage Closeout
2.60 Stage Mate
2.70 HITL

Procedure

Number Description

D3-21



Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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-0 being the time of launch vehicle lift-off from the
launch pad. T+ time is any event after T-O0. 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:
() Weather

(ii), Communication

02-7


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
item Document ‘Approval/ {Initial Submittal |Subsequent No. of
Review Date Submittal Date {Copies
C2: Mission Integration
|C2-1.1* |Interface Control Document (ICD) |Approval Preliminary ICD at |Baseline ICD at |10
ATP+ 6M L-15M and
AR
(C2-1.2* |Interface Control Document (ICD) |Approval NLT 3 months after |A/R or with each |3
Requirements Verification Matrix Preliminary ICD ICD revision
CDRL approval
IC2-2* |Mission Specific Program [Approval A/R As Changed 3
Requirements Document/
Operational Requirements
(PRD/OR)
IC2-3* Launch vehicle Detailed Mission |Approval AVR 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

TABLE D2-A: CDRL INDEX (Cont.)

D2-2



Section C
Contract Terms and Conditions NNK10LB02B

29.5

30.0
30.1

30.2

30.3

31.0

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 control 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.

DOMESTIC SOURCE CRITERIA

C-47


Section C
Contract Terms and Conditions NNK10LB028

Table C-6: NASA Postponement Fees and Grace Periods

BY

19.7 The maximum amount paid for delays (in excess of the grace period) by the
Contractor/NASA is BY 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 BY 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.

C-32


Section D .
Attachment D1: Exhibit 3 (F9) NNK10L802B

25.0

26.0
26.1

26.2

26.3

26.4

mission. These telemetry sites may be owned/operated by NASA, the
DoD, a U.S. commercial entity, or a foreign entity.

Generation of the AAMs will be treated as no greater than REQUIRED
capability for launch commit criteria purposes. Should any greater
capability be imposed, then the requirements to meet that greater
capability shall be considered outside the scope of this NSS and subject to
a separate contract action.

Format for AAMs will be in accordance with industry standard.

BS
bu

TDRSS Compatible Telemetry System

Design, build, qualify, integrate and test a TDRSS compatible telemetry
system in the Launch Vehicle. After first flight, the TDRSS compatible
telemetry system will be a standard launch service capability provided for
NASA missions. .

BY

Extended Integration Periods Order BY ~ ATP
BY Extended Integration Period

This non-standard service provides for the standard launch services

beginning B y searlier,at BY No additional services

‘

* above and beyond the standard services are covered by this non-standard

service.

RH: Extended Integration Period
This non-standard service provides for the standard launch services
beginning 4 earlier,at RU * 3. No additional services
above and beyond the standard services are covered by this non-standard
service.

By Extended Integration Period
This non-standard service provides for the standard launch services
beginning 134 earlier, at GY. | No additional services
above and beyond the standard services are covered by this non-standard
service.
&Y 1 Extended Integration Period

Exhibit 3 (F9) - 9


Section D : .
Attachment D1: Exhibit 1 (F1/F1e) pnt NNK10LB02B_ -

BY

| Redacted UN
ts entic et :

Exhibit 4 (F1/F1e) - 17


Section D

Attachment D1: Statement of Work (F1/F 1e) : NNK10L8028

(C)

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 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
teady

{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

Statement of Work (F1/F1e) - 14


Section D

Attachment D1: Exhibit 2 NNK10LB02B

SOW
Para. #

Launch Vehicle Requirements Summary

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.

tn 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 shail
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 |ines 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.

Required Insurance for Liability to Third Parties

The Contractor shail 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.

Exhibit 2 - 9



Section C

Contract Terms and Conditions NNK10LB02B

10)

(k)

(B) 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

(C) 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.

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).

{m) 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

(n)

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
shail not be liable to the Contractor for any amount for supplies or services
not accepted, including all launch service payments previously paid and alt
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.

C4


Section 0 . .
Attachment D1: Exhibit 1 (F9) te NNK10LB02B

RU

Redacted iA
( \s enwrre ty

Exhibit 1 (F9) - 28


Section D .
Attachment D1: Exhibit 1 (F9) : NNK10LB02B

RY

R cdacted iA
rhs entirety :

Exhibit 1 (F9) - 36


Section C

Contract Terms and Conditions NNK10LB02B

(c)

(d)

(e)

(f)

(9)

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 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 resoived 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;

C-2


Section D

Attachment D1: Statement of Work (F1/Fle)

NNK10LB02B

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.

CORL 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

The standard launch service shall include all analyses required to evaluate
compliance with 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.

2.3.3. 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.

Statement of Work (F1/F1e) - 18



Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
SDRL DESCRIPTION Number: S3-1
Reserved

D3-15


Section D
Attachment D1: Exhibit 4 (FA/F1e) NNK10LB02B

BY

Table D1- C: Vehicle Configurations
2.0 | PAYLOAD DELIVERY CAPABILITY

SpaceX has provided where applicable, in Tables D1-D through 01-G3, the maximum
payload capability from appropriate launch site with associated ground rules for the two
configurations; the Falcon 1 launch vehicle and the Falcon 1e Launch vehicle. The
Falcon 1 launch vehicle was part of the previous NASA Launch Services catalog, before
the contract period of performance expired. The two small Launch Vehicle
configurations are defined in paragraph 1.0, Vehicle Configuration. Performance is
expressed in terms of separated payload mass (assuming standard PAs as outlined in
paragraph 1.0, Vehicle Configuration) and shall assume a 3-sigma performance reserve
for the following orbits:

Low Earth Orbits (LEO): Data shall be provided for circular orbit altitudes from 200 to
2000 km (in increments of 100 km) for inclinations of 0, 5, 10, 20, 28.5, 38, 51.6, 60, 70
and 90 degrees.

Sun-Synchronous Orbits: Data shall be provided for circular orbit altitudes from 200 to
2000 km.

High Eneray Missions: Data shall be provided as a function of C3 from -10 km?/sec? to
200 km/sec’.

Elliptical Orbits: Data shail be provided as a function of apogee altitude and inclination
using the launch vehicle’s standard ground rules. In addition, provide performance with
a perigee altitude of 2000 km.

Geo-Synchronous Orbits (GSQ): Data shall be provided for insertion directly into Geo- .

Synchronous Orbits (GSO).

Exhibit 1 (F1/F1e) - 6


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B

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 shail be followed.

D2-24


Section B
Standard Form 1449 Continuation NNK10LB02B

2.0 TOTAL AWARD AMOUNT

The guaranteed minimum value of this contract is $20,000. The maximum
potential value of contract number NNK10LB02B is $15,000,000,000. The total
maximum potential value of all NLS contracts combined is $15,000,000,000.

2.1 Total Contract Amount

The total firm-fixed-price for all definitized work under this contract is. BY
This amount includes CLIN 10.

3.0 RESERVED

3.41. 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 iaunch 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 fower price awarded for an equivalent launch service.

5.0 HDIQLAUNCH 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 shal! be subject to the Jaunch vehicle certification requirements
of Section C, Clause 3.0. Contractor initiated changes to the launch vehicle

B-15 Modification 002


Section D..-: on
Attachment D1: Exhibit 4. (F1/Fte)

Exhibit 1 (F1/F te) - 9



Section D ve on
Attachment 01: Exhibit 1 (F1/Fte) cca NNK10LB02B

RY

Relacted (/ :
ths entirety

Exhibit 1 (F1/F1e) - 13


Section C
Contract Terms and Conditions NNK10LB02B

5.8

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 ta 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(l) and NFS 1852.232-77 Limitation of Funds (Fixed-Price Contract) (Mar 1989).

c-14


Section D

Attachment D1: Exhibit 1 (F1/F1e) NNK10LB02B

RY

R edacted ;
its enticety

Exhibit 1 (F1/F1e) - 19


Section D

Attachment D1: Exhibit 3(F9) NNK10L802B

20.12

20.13

20.14

23.0."

24.0

RF Resonance Analysis to determine maximum RF field strengths that
payload and launch vehicle avionics would be exposed to if spacecraft RF
transmission systems where activated while encapsulated within the
fairing. |

BY
Advanced mission performance analysis support (limited feasibility
assessments in response to new mission concepts)

Launch vehicle Collision Avoidance (COLA) trajectory and covariance

data. By \

Launch vehicle flight software code and associated documentation.

By

Reserved
Reserved
Reserved
Reserved

NASA Public Affairs Office Support

Accommodations for NASA guests, in units of 50, to view launch, including
local transportation, launch viewing facilities, lavatory accommodations,
food and beverage service, first aid and medical support for each
proposed launch site.

SpaceX offers this service as non-standard with R{{ i advance notice
for the Cape Canaveral launch site.

Launch Service Contractor (LSC) provided Telemetry

The LSC shail provide all telemetry data (main vehicle telemetry and
special instrumentation/wideband telemetry svstem) IAW LSP-PD-120.05,
‘Launch Telemetry Requirements."t QU )

Launch Service Contractor (LSC) provided Telemetry Acquisition
Assistance Message (AAM) Order NLS BY j

The Contractor shail provide Acquisition Assistance Messages (AAMs) to
the down-range telemetry sites utilized by the mission for antenna pointing
to acquire launch vehicle telemetry and to payload-designated control
centers/telemetry sites for acquisition of space vehicle telemetry. The
Government utilizes down-range telemetry sites to' receive record and
relay telemetry data from the Contractor's launch vehicle in accordance
with LSP-PD-120.05, “Launch Telemetry Requirements.” Mission-specific
telemetry sites are selected to acquire data from the launch vehicle during
the launch, powered-flight, and spacecraft separation phases of the

Exhibit 3 (F9) - 8



Section D
Attachment D4: SB and SDB Subcontracting Plan NNK10LB02B

ATTACHMENT D4

SMALL BUSINESS AND SMALL DISADVANTAGED BUSINESS
SUBCONTRACTING PLAN

SpaceX qualifies as a small business concern; accordingly, it is not required by law to
implement a small business and small disadvantage business subcontracting plan.

D4-1


Section D
Attachment D1: Exhibit 1 (F9) NNK10LB02B

BY
Red tee in
its entrety

Exhibit 1 (F9) - 31


Section D .
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

2.5.2

2.5.3

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.

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 [SO 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 2" 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).

Statement of Work (F1/F1e) - 28


Section B
Standard Form 1449 Continuation NNK10LB02B

proposals pursuant to Section C, Clause 14.0, and shall be subject to the written
approval of the Contracting Officer.

6.0 SPECIAL TASK ASSIGNMENTS (STUDIES AND ANALYSES) (CLIN10) -

DEFINITIZED
Task
Assignment
No. Description Hours _| Firm Fixed Price
Solar Probe Plus Launch RY
NLSII-S-001 | Vehicle Performance Analysis BY
T
Total | BY BY 7

B-16 Modification 002



Section D
Attachment 01: Exhibit 3 (F1/F1e) : NNK10L802B

17.0

18.0

19.0
19.1

19.2

19.3

19.4

20.0
20.1
20.2

20.3
20.4

Secondary Payload Accommodation Study

Asecondary payload accommodation study shall address the suitability of
and the approach for accommodating secondary payloads on a given
vehicle configuration.. The study shall develop a design, general payload
tequirements (secondary payload interface, volume, mass, environments)
and implementation scheme for implementing both separating and/or non-
separating secondary payloads. Dynamic loading analysis for generic
secondary payloads shall be performed so that mission unique analyses
are minimized.

SpaceX offers this as a non-standard service. Order | BY

Secondary Payload Mass Simulator

A mass simulator shall be designed and fabricated to match the
requirements (e.g., moment of inertia, rigidity, mass, and CG) of the
secondary payload that will be replaced. The mass simulator shall also
adhere to the requirements (e.g., contamination, cleanliness, and
interface) identified in the ICD. The Contractor shall complete any other
analyses or documentation required, for replacement of the secondary

- paviload with the mass simulator.

Payload Processing Facilities
The Contractor shall provide the capability to provide ground processing
facilities for payloads at the Eastern Range.

The Contractor shalt provide the capability to provide ground processing
facilities ti payloads at the Western Range.

The Contractor shall provide the capability to provide ground processing
fecite payloads at the Wallops Flight Facility.

The Contractor shall provide the capability to provide ground processing
facilities BY _

Additional Mission Analysis and Support

Reserved

Support for additional mission integration working group meetings in
excess of and) : .

This can be procured at any time by the customer up until BY _ with
(84 Inotice. Meetings are to be held at SpaceX facilities.

Reserved

Performance and Guidance Accuracy Analysis

This can be procured at any time by the customer up until AY and

will require {84 ‘to complete. SpaceX assumes format is per the NLS
N RFP CDRL.

Exhibit 3 (F1/Fte) -6


Section D . :
Attachment D1: Exhibit 1 (F1/F1e) . NNK10LB02B

R4

Redacted in
as entice tY

Exhibit 1 (F1/F1e) - 38


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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 rea! 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
amanner 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.

D2-55


Section D
Attachment D1: Exhibit 3 (F1/Fte) NNK10LB02B

9.0
9.1

9.2
9.3
9.4
9.5

10.0

11.3

11.4

11.6

Enhanced Electrical Interface
Increased capacity payload-to-GSE interface.
for IDIQ at this time but can be evaluated as a mission
unique service. ,
Launch vehicle command and control of payload
‘for IDIQ at this time but can be evaluated as a mission
unique service.
Launch vehicle supplied payload power capability
‘for IDIQ at this time but can be evaluated as a mission
unique service.
Enhanced telemetry capabilities including interleaving/deinterleaving of
payload telemetry data
‘for IDIQ at this time but can be evaluated as a mission
unique service.

_ Additional faunch vehicle environmental instrumentation

mgd

Launch Vehicle Mounted Cameras

Launch Vehicle Mounted Cameras including necessary lighting and the
real time transmission of the video signal to the designated NASA LSP
Data Center. Identification of potential ground coverage sites and.
coordination of video transmission between all ground sites and NASA
LSP Data Center is to be included.

L » 64 .
Special Contamination Control Options

Enhanced fairing environment

SpaceX can offer the enhanced fairing environment for Falcon 1 and
Falcon te as a non-std service. Order

Enhanced fairing internal surface cleaning (IEST-STD-CC1246D level
500A)
BY -

Optional pavload/vehicle integration environments

Additional instrument purge system(s) up to RY JEST-STD-CC1246D
leyel 100A) :

“Bq. for IDIQ (can. be accommodated on a case by case
basis).
Grade B Nitrogen (GN2) IAW MIL-PRF-27401F or conditioned air cooling
supply for spot cooling of payload components from payload mate or
encapsulation up to &
Grade B Nitrogen spot cooling is offered with a lead time of BY
before launch.
Sic see C Nitrogen (GN2) [AW MIL-PRF-27401F Purge System

)

Exhibit 3 (F1/F1e) - 4


Section D

Attachment D1: Exhibit 2 NNK10LB02B
SOW Launch Vehicle Requirements Summary
Para. #

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 fines provided for payload use.

Cc Support for the installation and checkout of the payload GSE (provided by the payload
customer) at the launch site, and payload communication accommodations 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 Provision for contingency off-loading of payload propellants in accordance with the
.| appropriate Range Safety requirements and appropriate payload procedures.

F Provision for jaunch site services to meet payload requirements such as: power, air
conditioning, GN2/GHe purges, and contamination control.

facility if necessary.

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).

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.

Exhibit 2 - 7



Section D
Attachment D1: Exhibit 3 (F9) NNK10LB02B

pd for IDIQ at this time but can be evaluated as a mission
unique service.
9.3 Launch vehicle supplied payload power capability
Y for IDIQ at this time but can be evaluated as a mission
unique service.
9.4 Enhanced telemetry capabilities including interleaving/deinterleaving of
payload telemetry data
BY ‘for ID!Q at this time but can be evaluated as a mission
unique service.
9.5 Additional launch vehicle environmental instrumentation
_..__ for IDIQ at this time but can be evaluated as a mission
unique service.

10.0 Launch Vehicle Mounted Cameras BY
Launch Vehicle Mounted Cameras including necessary lighting and the
teal time transmission of the video signal to the designated NASA LSP.
Data Center. Identification of potential ground coverage sites and
coordination of video transmission between all ground sites and NASA
LSP Data Center is to be included.

QM

11.0 Special Contamination Control Options

11.1. Enhanced fairing environment
SpaceX offers recirculated nitrogen as the conditioned gas used inside the
payload fairing once the Falcon 9 is vertical on the pad with access.doors
closed and no additional access required. Operating parameters are
provided in Exhibit 1.

11.2 Enhanced fairing internal surface cleaning (IEST-STD- ©C1246D level
500A)
SpaceX can offer the enhanced fairing internal surface cleaning for Falcon
9 as a non-std service.

11.3. Optional payload/vehicle integration environments

U

11.4 Additional instrument purge system(s) up to AY (IEST-STD-CC1246D
level 100A)
BY for IDIQ (can be accommodated on a case by case
basis).
11.5 Grade B Nitrogen (GN2) [AW MIL-PRF-27401F or conditioned air cooling
supply for spot cooling of payload components from payload mate or
encapsulation up to BY

Exhibit 3 (F9) - 4


Section D
Attachment D1: Exhibit 1 (F9) a NNK10LB02B

ane -ew

RY

Redack in
ks entirety

“ Exhibit’t (F9) - 25


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B

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

(C) Launch Management Coordination Meeting (LMCM)

{D

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
faunch. 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 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 [AW 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

Statement of Work (FQ) - 15


Section D~
Attachment D1: Exhibit 1 (F1/F1e) Lt NNK10LB02B

BY

| Redacted in
+s enrety

Exhibit 1 (F1/F1e) - 21


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
item Document Approval’ |initial Submittal {Subsequent No. of
Review Date Submittal Date {Copies
|c4: Analysis : ;
iC4-1* -|Performance and Guidance initial : a ‘ L-12M;
Accuracy Analysis (PGAA) Submittal = L-6M
Review, 8 Y y
Subsequent {7
Submittals =
Approval
(C4-2* {Final Mission Analysis (FMA) ‘Approval Update: 3
BY L-2 wks
K— >,
IC4-3* |Payload/Expended Stage Approval L-6M 3
: Separation Analysis _
\C4-4* |Payload Fairing Venting Analysis |Approval As Required {3
<—84 —
IC4-5*  |Payload Fairing Clearance (Approval é 5 L-10M; 3
Analysis BY L-6M
IC4-6* |Pre-Flight Controls and Stability {Approval AIR 3
|Analysis <— BY er,
1C4-7* iCoupled Dynamic Loads Analysis {Approval Receipt of P/L L-15M 3
Prelim Model + 4M L-26W.
IC4-8* _ {Integrated Thermal Analysis ‘Approval AIR 3
iC4-9* [RF Link Analysis Approval L-12M AJR 3
C410" |Payload/Launch Vehicle EMC, _ [Approval (B,C,D) L-12M;, | (B,C,D) L-3M; [3
IRF, and EED Compatibility (A&E) AR in CDRL! (A&E) AVR in
Analysis CORL
IC4-11* |Mission Unique Software [Approval R y Final=L-6M 13
IC4-42" [Quick Look Flight Report Review , ~ NIA 3
IC4-13* |Final Flight Report Review RY AIR 3

* Required per mission

TABLE D2-A: CDRL INDEX (Cont.)

02-4



Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
CDRL DESCRIPTION Number: C6-1(cont)

(C)

(D)

(E)

(F)

(G)

(vii) Type of measurement
(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

(xiii) 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 nominai 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.

D2-54


Section 0

Attachment D3: Supplemental Data Requirements List NNK10LB02B
SDRL DESCRIPTION : Number: S4-2
Reserved

D3-20


Section C
Contract Terms and Conditions NNK10LB02B

25.0
25.1

25.2

25.3

25.4

25.5

25.6

25.7

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 resuit 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 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:

C-39


Section D

Attachment D1: Statement of Work (F1/Fie) ~ NNK10LB02B
(A) Payload/Vehicle Integration Environment. For all Contractor provided

(B)

(C)

(D)

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 BY jand

BY 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. If the Contractor provides a payload protective cover as identified in
paragraph 2.4.2.2(K) of the SOW, and purge air has been established, the
facility environment may be exceeded. Prior to removal of the payload
protective cover, the facility shall be returned to a Class 8 IAW ISO 14644-1
clean room environment. 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 and
the payload environment shall be maintained within a temperature and
humidity range of BY . respectively. ,
The Contractor shall identify periods or configurations where the temperature
and humidity requirements cannot be met. 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.

Fairing Environment. Following fairing installation and payload mate to the
launch vehicle, the PLF environment shall be purged with conditioned filtered
air and shall maintain a temperature set point range, selectable by the
payload, of BY cose ee through T-
0.. Relative humidity shall be maintained within 30% to 50%, controllable to
5%. The Contractor shall identify periods or configurations where the
temperature and humidity requirements cannot be met. 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, GNz (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 (including Payload Adapter)

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

Statement of Work (F1/F1e) - 25


Section C

Contract Terms and Conditions NNK10LB02B

(3)

(e)
(1)

teproduction, 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 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.

(iii) 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).

C-57


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B

CDRL DESCRIPTION Number: C3-4

QUALITY MANAGEMENT S YSTEM (QMS) AND SUPPLIER/VENDOR
AUDIT/AS SESS MENT 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 C
Contract Terms and Conditions. NNK10L802B

(9) Other documents, exhibits, and attachments.
(10) The specification.
(t) 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.

(2)

(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

Cc-8


Section D

Attachment D3: Supplemental Data Requirements List

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. 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
1S 1-1 Launch Service User's Guide and Facility
Information :
S1-2 Mission Integration Meeting Documentation
S1-3 Program Master Schedule and Launch Vehicle
Planning Manifest
$3: Safety & Mission Assurance
S3-1 Reserved
S3-2 Reserved
S3-3 As-Built Configuration List
IS3-4 Safety Data Package
$4: Analysis
S4-4 Mission Battery Budget Analysis
S4-2 Reserved
I $5: Engineering
S5-1 [Vehicle Test Procedures
S6: 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

NNK10LB02B



Section D
Attachment 01: Statement of Work (F1/Fle) NNK10LB028

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.

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.

21 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

(iti) Instantaneous launch window

°* (iv) Inertial targeting overa’ = =4 — 3 launch window utilizing multiple
discrete or continuous targeting. [ Ba
continuous targeting. Muitiple dis: { ceesee

BY |
voy

(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.

Statement of Work (F1/Fte) - 7



Section D
Attachment D3: Supplemental Data Requirements List

NNK10LB02B

SDRL S1-1 Data
Request BY

BY

(L) Grounding Provisions

BY

D3-10



Section B

Standard Form 1449 Continuation NNK10LB028
NON-STANDARD SERVICE ITEM (Falcon 1 & te} NOT TO EXCEED (NTE) PRICE ($) INCALENDAR YEAR ORDERED*
# from ttem description 2010 | 2011 ] 2012 2013 2014 2015 2016-2022
Exhibit 3 |
262 | Six Month Extended integration Period . Ter
263 | Nine Month Extended Integration Period ; Te
26.4 | Twelve Month Extended integration Period << — 8 > TEP
7 Contractor Defined Non-Standard Services
B7A_| Rewajalein launch Tee

* Pricing may be offered for any or all of the order years remaining on the NLS contract, ie. order years 2010 (Jul-Dec) through 2020, At minimum, the Contractor shail provide
pricing through 2015. 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-10a: NTE Price List — Falcon 1 & 1e Non-Standard Services for IDIQ Missions

Launch Vehicle Confi

uration Falcon 9 Bik 1 & 2 From Table B-9

NON-STANDARD SERVICE ITEM (Falcon 9 Bik 1 & 2}

NOT TO EXCEED (NTE) PRICE ($) IN CALENDAR YEAR ORDERED*

#from | Item description 2010 (Jule 2017 2012 2013 2018 2015 2016-2022
Exhibit 3 Dec)
7 ‘Alternate Vehicle configurations or Performance
Enhancements
2 Alternate Fairing Configurations and/or Modifications:
21 Alternate Configurations _ TBP
22 ‘Additional access doors in excess of 3 included in ~ — > TBP
standard service ——
23 ‘Access doars of non-standard size, TBP
2a Mounting provisions, cabling and antenna systems for TBP
reradiating signals from the payload to remote sites
26 S, G, X, and Ku-band Reradiating equipment TeP
26 RF Transparent Ooors _ 4 Ss TBP
3 ‘Alternate Payload Adapters _S :



Section C

Contract Terms and Conditions NNK10LB02B

(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, ef 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).

(2) 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.

35.0 RESERVED

36.0 LISTING OF CLAUSES INCORPORATED BY REFERENCE

36.1

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

FEDERAL ACQUISITION REGULATION (48 CFR CHAPTER 1) CLAUSES

FAR §2.202-1 Definitions (Jul 2004)

FAR §2.211-14 Notice of Priority Rating for National Defense, Emergency

Preparedness, and Energy Program Use (Apr 2008)

C-58


Section C .
Contract Terms and Conditions NNK10LB02B

pursuant to 234A of the Act, for violations of applicable DOE nuclear-safety
related rules, regulations, or orders.

(j) 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.

(k) 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.

(l) Effective date. This indemnity agreement shall be applicable with respect to

nuclear incidents occurring on or after August 20, 1988.

2 :
42.0 NFS 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; SN

(ii) Damage to, loss of, or loss of use of any property;

{iii) Loss of revenue or profits; or

C64


Section D .
Attachment D1: Exhibit 1 (F9) * NNK10LB02B

(34

R cdactedl 7 An
( $5 emntiy ety

Exhibit 1 (F9) - 27


Section D

Attachment D3: Supplemental Data Requirements List

SDRL S1-1 Data

NNK10LB02B

Request

BY

(B) Crane Size and Hook
Height

\

Ru

(C) Electrical Service

w

RY

D3-4


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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.

02-33


Section B

Standard Form 1449 Continuation

NNK10LB028

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. For non-standard services which have non-recurring costs the
offeror shall also propose “Subsequent purchase” pricing. “Subsequent purchase’ pricing shall apply in the event
the Government orders a non-standard service more than once from a provider, regardless of the mission specific

implementation and/or repetitive nature of the mission.

Launch Vehicle Configuration Falcon 1 & Falcon 1e From Table B-9

NON-STANDARD SERVICE ITEM (Falcon 1 & 1e)

NOT TO EXCEED (NTE) PRICE ($) IN CALENDAR YEAR ORDERED*

# from

item description

2040 (Jul-Dec) 2017 2012 2013 2014 2015 2016-2022
Exhibit 3
7 Altemate Vehicle configurations or Performance 7 TSP
Enhancements
z Alternate Fairing Configurations and/or Modifications
a Altemate Configurations i Ter |
22 ‘Additional access doors in excess of 2 included in “TSP
standard service
2.3 Access doors of non-standard size TBP
aa Mounting provisions, cabling and antenna systems for TEP
reradiating signals from the payload to remote sites
[25 S.C. x, and Ku-band Reradiating equipment B Y “Tap
26 RF Transparent Ooors TBP
3 Alternate Payload Adapters:
at Different size or different payload interface Pas A TEP
32 Cow tip-off rate Pas TeP |
4 Upper stage hardware
at Motor of TBP
42 PA Ter
a3 Spin system with enhanced capability TEP



Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10L802B

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 anaiysis shail 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.

(D) Expended stage/payload relative motion analysis following payload deployment


Section D
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

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

(F) Provision for launch site services to meet payload requirements 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.

(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) Provision of a payload protective cover for use after payload mate to the
launch vehicle, if the fairing is installed at the launch pad. The cover shail be
purged with conditioned air meeting the minimum requirements stated in the
SOW, paragraph 2.4.2.3(C). Provisions shall be made for payload personnel
ingress and egress.

(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.

(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 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:

Statement of Work (F1/Fte) - 24


Section D
Attachment D3: Supplemental Data Requirements List

NNK10LB02B

Enclosed are the Falcon 1 and Falcon 9 launch vehicle Payload User's Guides for reference only. Please note that
content may change.

The following information is provided to supplement the Launch Vehicle User’s Guides.

Request
(A) Payload GSE Space |-—

and Capabilities (S . BY

A

SDRL S1-1 Data 4 U - ‘

D3-3


Section C
Contract Terms and Conditions NNK10LB02B

(A) 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:

1. Negligence;
2. Contributory negligence;
3. Assumption of risk; or

4. Unforeseeable intervening causes, whether involving the conduct of a third
person or an act of God;

(B) Any issue or defense as to charitable or governmental immunity; and

(C) 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 issue or defense 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. The waiver shall be judicially enforceable in accordance
with its terms by the claimant against the person indemnified.

(v) 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.

(vi) 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.

(3) The waivers set forth above:

(i) 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;

(ii) Shall be judicially enforceable in accordance with its terms by the claimant
against the person indemnified;

(iii) Shall not preclude a defense based upon a failure to take reasonable steps
to mitigate damages;

(iv) Shail 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;

(v) 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

C42


Section D 2
Attachment D1: Exhibit 1 (F1/F1e) : NNK10LB02B

Frequency Falcon 1 Payload
(Hz) Acoustic MPE*

Frequency Falcon 1 Payload

Acoustic MPE*

“Empty Fairing (133 dB OASPL)

Table D1- Ka: Falcon 1 Maximum Flight-Level Payload Acoustic Environment
(derived from flight and test data) -.

Exhibit 1 (F1/F1e) - 32


Section D
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

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 guidarice’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 hardwire) 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 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.

Statement of Work (F1/F1e) - 20


Section D
Attachment D1: Statement of Work (F1/F1e)

NNK10L802B

« Provide flexible manifesting policy that recognizes the national priorities of

NASA missions.

e Provide a capability to optimize cost, schedule, and performance to satisfy

mission objectives.

e Provide for clear Government visibility into program schedule, technical

performance, and risk.

« Foster competition and create opportunities for new, emerging launch service

providers.

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

The Contractor shall comply with the requirements contained in the following

Document Title

1.3 Compliance Documents
documents.

Document No. Revision
Applicable Range Safety
Requirements
1SO 9001/2000' 2000
AS9100 “2009
KNPR 8715.3?
LSP-PD-120.05 BASIC
NPR 8715.6° A

NASA-STD-8719.97

1

2

3

(e.g., EWR-127-1, AFSPCMAN 91-710, RSM-
2002)

International Organization of Standardization
Aerospace Quality Management System

KSC Safety Practices Procedural Requirements
Launch Telemetry Requirements

NASA Procedural Requirements for Limiting
Orbital Debris

NASA Safety Standard for Lifting Devices and
Equipment

(SO 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.

The Contractor shall support NASA's compliance with this document.

Statement of Work (F1/Fte) - 5



Section D! :
Attachment D1: Exhibit 1 (F 1/F1e) . ‘ NNK10L802B

BY

Redacted in
its entirety

‘Exhibit 1 (F1/F te) - 24


Section D o,
Attachment D1: Exhibit 1 (F1/F1e) on NNK10LB028

BY

Re acted in
its enbiceky

Exhibit 1 (F4/F1e) - 27


Section C
Contract Terms and Conditions NNK10LB02B

25.9

26.0

(D) Critical flight hardware pedigree.

(£) Safety and Mission Assurance compliance evaluations (prime and
subcontractors).

(F) Pre-ship reviews.

(G) Design and qualification reviews.

(H) Major/critical problems.

(!) 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.

(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

C-41


Section C
Contract Terms and Conditions NNK10LB02B

24.3

(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.

(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.

(C) 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 Jaunch 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 faunch service a

Partial Mission Success, the Government will pay no portion of the final
payment in accordance with Table C-8.

C-36


Section C :
Contract Terms and Conditions NNK10LB028

17.0___ INSPECTION SYSTEM RECORDS. .......sssssssssssssccsssesscosssessessssesesssssccesaes C-29

18.0 REQUIRED TIME OF DELIVERY FOR LAUNCH SERVICES...

19.0 _ ADJUSTMENTS TO LAUNCH SCHEDULE ..........s:ssssesrssesesesserensetscsotts C-30
20.0 __ PLACE OF PERFORMANCE ..............:..:s:sscsssssssscssesssssesssessesssesssssssoetsses, C-34
21.0 _ RESERVED. .............-..scssssssssssssssssssatssessssrerssssssecescossesnesssesesssssneseneceessaeaees C-34
22.0 __ RESERVED.............ssscssssssssssssesesececssssssssoasscasassecessessscasacssesseserscesseserscesese C-34
23.0 __ USE OF GOVERNMENT PROPERTY, FACILITIES, AND ASSETS....... C-34
24.0 _ MISSION SUCCESS DETERMINATION, INVESTIGATION, AND
CORRECTIVE ACTIONG ..........-scssssssscsssessesssessessessessscssosssssesscsessesecestes C-35
25.0 _ GOVERNMENT _INSIGHT AND APPROVAL .........-...:s:s:ssssssssssssssesesersess C-39
26.0 _ _ GOVERNMENT LAUNCH READINESS ASSESSMENT...............-.... C-41

27.0 _ LICENSES AND PERMITS FOR A LAUNCH SERVICE OPERATOR... C-42
28.0 _ ADVANCE UNDERSTANDING REGARDING TERMINATION SETTLEMENT

UNDER FAR 52.212-A(L) ......sscessessssessssesersssssssnseseessceeseceeseceerensesessesseness: C-42

© 29.0 CO-MANIFESTED PAYLOADS wssscsssssssssssssesssnssestieseessessecestsssesssssuses C-43
30.0__ EXPORT CONTROL AND FOREIGN NATIONALG..............::::s:sscssereseeee C-47
31.0__ DOMESTIC SOURCE CRITERIA...............:s.:.:ssssosssssserssssseseseseessecneoesersres C-47
32.0__ LIABILITY FOR THIRD PARTY CLAIMS ..........::e:sscccssssssssssssssessesessseees C-48

33.0 __ FAR 52.212-3 OFFEROR REPRESENTATIONS AND CERTIFICATIONS --
COMMERCIAL ITEMS {AUG 2009) ALT | (APRIL 2002)...............:::04 C-54

34.0 ___ FAR 52.212-5 CONTRACT TERMS AND CONDITIONS REQUIRED TO
IMPLEMENT STATUTES OR EXECUTIVE ORDERS--COMMERCIAL ITEMS

(APR 2010)........-:sscssossscsrssesosasserssesescesssstecasssscsssssssssssseecasssesssstssessesessses C-51

35.0___ RESERVED .............ssscsssssssssssssnrscssesessessssesseseesessapeccnceesesssasssesssseseeseesses C-58

36.0 __ LISTING OF CLAUSES INCORPORATED BY REFERENCE....
37.0__ FAR 52.252-2 CLAUSES INCORPORATED BY REFERENCE (FEB



Section D
Attachment D1: Exhibit 1 (F9) : -_ NNK10LB02B

BY
R alacted | iN
ifs entrety

Exhibit 1 (F9) - 35


Section C

Contract Terms and Conditions NNK10LB02B

(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.

1. 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.

2. 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 253j(d)).

3. 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).

(iii) Launch service task order mission solutions will be attached to the
contract (Exhibit 9) upon award of task order(s).

(F) Modifications to LSTOs. After an LSTO is issued, it may be necessary to

(G

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.

Task Order Authorization and Content. The only persons authorized to issue
task orders under this contract are the KSC Contracting Officers. Task

C-27


Section D Lo

Attachment 01: Exhibit 3 (F9) NNK10LB02B
C
SECTION D
ATTACHMENT D1
EXHIBIT 3
FALCON 9

Non-Standard Launch Services List .

Exhibit 3 (F9) - 4


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B

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 shail 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

(K) Input file

02-32


Section C
Contract Terms and Conditions NNK10LB02B

19.4

19.5

196

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, Ciause 1.0(m), Termination

BY

Table C-5: Contractor Liquidated Damages and Grace Periods

BY |



Section 0
Attachment D1: Exhibit 3 (F1/F1e) NNK10LB02B

EXHIBIT 3
NON STANDARD-LAUNCH SERVICES LIST for Falcon 1 and Falcon 1e

SpaceX shall provide the capability to perform the following non-standard
services. This information is provided in response to the instructions in the NLS
Il RFP.’ These services shall be performed for each mission, as requested and
authorized by the NASA Contracting Officer, in accordance with the contract
terms and conditions. Each non-standard item listed shall include all hardware,
software, analyses, and support required to provide the service. Any impacts to
the capabilities or conditions defined in Exhibit 1 introduced by the non-standard
service shall be explained in detail. The Contractor shall not be required to
design and develop a non-standard service in support of this contract.

The Contractor shall list all non-standard services provided for each proposed
launch vehicle configuration, which will be negotiated and incorporated into the
contract. All non-standard services provided shall be fully compliant with the
SOW. Any non-standard services provided that are not fully compliant shall be
designated as such in the proposal with details supplied. as to the impact of
making the service compliant. All proposed non-standard services shall have an
associated, no-later-than ordering date. with respect to the launch date. In
addition, the Contractor shall provide any non-standard services deemed useful
for future NASA missions based on past experience.

If authorized, the Contractor shall implement the following services:

1.0 Alternate Vehicle Configurations or Performance Enhancements (i:e.,
Extended Nozzles, Additional Motors/Thrust Augmentation) —

2.0 Alternate Fairing Configuragons and/or Modifications

2.1 Alternate configurations — '

2.2 Additional access doors in excess of two included in standard service.
Limitations on location can be provided (for example, doors cannot be
located in proximity to the fairing separation split line). This option must
beorder BY ° ifrom launch.

2.3. Access daors of non-standard size
SpaceX can offer doors smaller than the standard size. Limitations on
location can be provided (for example, doors cannot be located in
proximity to the fairing separation split.ine). This option must be order

BY ~~ ~ 3 from launch.

2.4 Mounting provisions, cabling and antenna systems for re-radiating signals
from the payload to remote sites — R ‘ :

2.5 S,C, X, and Ku-band re-radiation equipment - BY

Exhibit 3 (F1/F1e) - 2


Section C
Contract Terms and Conditions NNK10LB02B

(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.

(2) 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.

(e)(1) 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.

(2) In the event of an extraordinary nuclear occurrence which:
(i) Arises out of, results from, or occurs in the course of the construction,
possession, or operation of a production or utilization facility; or

(ii) 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

(iil) 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

(iv) 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:

C61


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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.

02-18


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10L802B
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:
e Safety Data Package (Missile System Prelaunch Safety Package - MSPSP)
System Descriptions
Hazards Analyses/Hazard Reports
Single Failure Point (SFP) Analyses (where applicable)
Test Plans and Nondestructive Examination Plans
Material Compatibility
Material Safety Data Sheets (MSDS's)
e 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
e Radiation control and use authorization for ail 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

oa0g000

ie}

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
safety documentation. The 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 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 D
Attachment D1: Statement of Work (F9) NNK10LB02B

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 shail 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
$6-1).

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 hardwire) 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 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.

Statement of Work (F9) - 21


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B

(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;

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)

(B)

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.

Statement of Work (FQ) - 14


Section B

Standard Form 1449 Continuation NNK10LB028
NON-STANDARD SERVICE ITEM (Falcon 9 Bik 1 & 2) NOT TO EXCEED (NTE) PRICE ($) INCALENDAR YEAR ORDERED*
# from Item description 2010 (Jul- 2011 2012 2013 204 2015 2016-2022
Exhibit 3 Dec)
26 Extended Intagration Perlods (assumes extended
mission integration period as noted, not extended
payload processing integration period)
26.4 Three Month Extended Integration Period Yer
26.2 ‘Six Month Extended Integration Period TeP
26.3 Nine Month Extended Integration Period | TS TBP
26.4 Twelve Month Extended Integration Period ° TeP

a Contractor Defined Non-Standard Services ~ L i >
27.1 Kwajalein launch TBP

* 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 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-10b: NTE Price List — Falcon 9 Blk 1 & 2 Non-Standard Services for IDIQ Missions



Section.D
Attachment D1: Exhibit 4 NNK10LB02B

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.

SpaceX 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/US Government Launch Authority foresees no national resource
protection or Range Safety issues which would preclude launch.

; (TBD) Space Wing//US Government Launch Authority

Date

Exhibit 4 - 2


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B°

2.2.2

2.2.3

2.2.4

(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

{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

Statement of Work (F9) - 16


Section C
Contract Terms and Conditions NNK10LB02B

24.0

24.1

MISSION SUCCESS DETERMINATION, INVESTIGATION, AND CORRECTIVE
ACTIONS

Mission Success Criteria

(A) A mission will be determined a Mission Success, if:

10)
(ii)

(iii

(iv)

The payload is placed into the required orbit by the launch vehicle, and

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

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

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) A mission will be determined a Failed Mission when the payload:

10)
(ii)
(iii)

ls destroyed during launch/flight, or
Cannot be separated from the launch vehicle, or

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.

24.2 Mission Success Determination

C-35


Section B

Standard Form 1449 Continuation

NNK10L.B02B

CLIN

Description of
Supplies and Services

Contract
Mod*

Qty

Unit

Unit
Price

(8)

Total
Amount

(8)

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

x'A

x'B

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

Lot

Lot

See
Table B-
9

See
Table B-
10

TBD

" The Contracting Officer shall determine the CLIN number to be assigned.
2 The actual number of LSTOs to be awarded is TBD.
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.

Table B-8: IDIQ Launch Service Task Order



Section D

NNK10LB02B

Attachment D1: Exhibit 41 (F4/Fte)

RU
Rellacked Un

AS e nh roby

Exhibit 1 (F1/F1e).- 18


Section D . fo :
Attachment 01: Exhibit 1 (F1/F1e) . NNK10LB02B

BY

Red acted ia
ibs entir ety

Exhibit 1 (F1/F te) - 42


Section D
Attachment D1: Exhibit.1 (F9) te NNK10LB02B

RY

Redacted tr -
its entirety

Exhibit 1 (F9) - 21


NNK10LB02B



Section C

Contract Terms and Conditions NNK10LB02B

(iii) Alternate | (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 | (Oct 1995) of 52.219-7.
(iii) Alternate Il (Mar 2004) of 52.219-7.

(10) 52.219-8, Utilization of Small Business Concerns (May 2004) (15
U.S.C. 637(d)(2) and (3)).

(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.
(iii) Alternate || (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)).

C-53


Section C

Contract Terms and Conditions NNK10LB02B

(0)

(p)

(a)

()

(s)

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 Goverment 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 benefit; 40 U.S.C. 3701, ef 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.


Section C
Contract Terms and Conditions NNK10LB02B

32.5

33.0

34.0

(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

(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.

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.

FAR 52.212-3 OFFEROR REPRESENTATIONS AND CERTIFICATIONS--
COMMERCIAL ITEMS (AUG 2009) ALT I (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.

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:


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

(F) Provision for launch site services to meet payload requirements 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.

(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 contro! 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) Provision of a payload protective cover for use after payload mate to the
launch vehicle, if the fairing is installed at the launch pad. The cover shall be
purged with conditioned air meeting the minimum requirements stated in the
SOW, paragraph 2.4.2.3(C). Provisions shall be made for payload personnel
ingress and egress.

(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.

(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 Environmenta! 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, integration facilities, or facilities at the launch pad), a
Class 8 clean room environment IAW ISO 14644-1 shall be provided. In

Statement of Work (F9) - 25


Section C

Contract Terms ani nditions NNK10LB02B

(B

(C)

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.

!n 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, Ciause 1.0(\),
“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:

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

C-44


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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) A description 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 (EQs)

(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.

D2-47


Section C

Contract Terms and Conditions NNK10LB02B

LIST OF TABLES
Table C-1: Launch Service Payment Schedule ...........s:ssseseesete teeters C-15
Table C-2:  RESCrVed oo. secs cee ee eee cece ee eee reeset eats eeetaeaneeeeeeeteatateteeeeeseeteeeeees C-29
Table C-3: RES@rVed asics esee cesses eett tee ee sees sees eeeeeonseeesesscesssesseespeatoee epee C-29
Table C-4: _iDIQ LSTO Delivery Schedule .

Table C-5: Contractor Liquidated Damages and Grace Periods

Table C-6: _ NASA Postponement Fees and Grace Periods ............ cee C-32
Table C-7:  ReS@rved sss sssssses sce ccseececsseceesececesseesccssesesesesenpeeepecaeseesteseeeseenenenee C-34
Table C-8: Mission Success Payment Schedule ............-...-csesseeeeseeeeessenesteeees C-37
Table C-9: RESCrVed eee eee cess tetesec ts ssee ee teteesesececeseeseeesesesectseseeeeeeeeteeeeesoes C-43

C-iv


Section C
Contract Terms and Conditions NNK10LB02B

(c) (1) {tis 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(I) 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 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”.

(d) 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.

(e) 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
shail be made in the price(s) (including appropriate target, billing, and ceiling

C-17


Section D

Attachment D1: Exhibit 1 (F1/F1e) NNK10L802B

SECTION D
ATTACHMENT D1
Exhibit 1

FALCON 1 and FALCON 1e Capabilities,
Specifications and Environments

Exhibit 1 (F1/Fte) - 1


Section D . .
Attachment D1: Exhibit 1 (F9) NNK10LB02B

IR U

Reda cheoh tA
( fs enhy ety

Exhibit 1 (F9) - 44


Section C
Contract Terms and Conditions NNK10LB02B

24.6

24.7

(C)

(D)

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 related 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
tequire corrective action before return to flight shall also apply.

Finality of Contracting Officer's Determination

(A)

(B)
(C)

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

Reserved

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 shail 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.

C-38


Section D
Attachment 01: Exhibit 1 (F9) NNK10L802B

BY

Redacted ( rn
ity ent rety

Exhibit 1 (F9) - 43


Section C

Contract Terms and Conditions NNK10LB02B

(h)

(v)

(vi)
wii)

(viii)

(i)

(x)

Shipping number and date of shipment including the bill of

_ lading number and weight of shipment if shipped on Government

bill of lading;
Terms of any discount for prompt payment offered;
Name and address of official to whom payment is to be sent;

Name, title, and phone number of person to notify in event of
defective invoice; and

Taxpayer Identification Number (TIN). The Contractor shall include
its TIN on the invoice only if required elsewhere in this contract.

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-3


Section D :
Attachment D1: Statement of Work (F9) NNK10LB02B

The Contractor shall provide BYNASA 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. The Contractor shall implement the NASA
provided console communications configuration for those consoles occupied by
the NASA team within the Contractor's faunch 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 shail 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 faunch 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 igo en)

4 __ IAW NASA Policy LSP- PD- 120, 08. The
Contractor shall receive and record launch vehicle ~ Ba

BY | after payload separation, JAW NASA Policy LSP-' PD-
120.05.

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 [AW 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 shail 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.

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

Statement of Work (F9) - 23


Section D
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

LIST OF TABLES

Table D1-A: Mission Analyses to Support Payload Integration
Table D1-B: Mission Unique Hardware Factors of Safety

Statement of Work (F1/F1e) - 3


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB028
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 D
Attachment D1: Exhibit 7 (F9) NNK10LB02B

Section D
ATTACHMENT D1
EXHIBIT 7

FALCON 9
Certification Plan

RY
‘2 edacted i
+s enticety

Exhibit 7 (F9) - 1


RY

Redacted fn -


Section C
Contract Terms and Conditions. NNK10L802B

14.0

14.1

14.2

14.3

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 postion 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 aunch 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

C-24


Section C
Contract Terms and Conditions NNK10LB02B

(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 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

C-66


Section 0

Attachment D1: Exhibit 2 : NNK10LB02B

SOW © Launch Vehicle Requirements Summary

Para. #

N All other hardware equipment, software, infrastructure, and logistics necessary to perform
the contracted launch services.

2.2 Program Management (see SOW for description)

2.3 Mission Integration Services

2.3.1 Mission integration Management (see SOW for description)

2.3.2 Mission Analyses (see SOW for description)

2.3.3 Mission Success Determination (see SOW for description)

24° Launch Site Support (see SOW for description),

2.4.1 | Pre-Launch Checkout and Launch Support _ _

2.4.1.4 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.

Cc Provide NASA access to all meetings including, but not limited to, scheduling 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

2.4.1.2.1_ | Vehicle Telemetry

Exhibit 2 - 4



Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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
Attachment D1: Statement of Work NNK10LB02B

EXHIBIT 8

MISSION INTERFACE CONTROL DOCUMENTS (ICD)

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.

For each mission, the final Interface Control-Document (CDRL C2-1.1) shall be attached
to the contract.

Exhibit 8 - 1


Section D
Attachment D1: Exhibit 1 (F1/F1e)

NNK10LB02B

RY

R od G of col (7
its ent rely

Exhibit 1 (F4/F te) - 20


Section D ra
Attachment D1: Exhibit 1 (F9) . a NNK10LB02B

RY
Redacted in
( Ls entir ety

Exhibit 1 (F9) - 12


Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
2.80 Merlin Engine Closeout
2.90 FTS System Level Checkout
2.95 FTS Pad Checkout
2.100 Tunnel Cover install
2.120 Encapsulation
2.125 Avionics Bay Closeout
2.130 Payload to Vehicle Mate
2.140 Ordnance Install
2.145 1st Stage TEA-TEB Install
2.150 Rollout and Connect
2.160 Erect
2.165 QD Mechanical Connect
2.170 Vehicle QD Leak Check
2.175 2nd Stage Lanyard and Tether Connect
2.180 Vehicle Align to Local Vertical
2.200 Optical Azimuth Alignment
3.10 LV Power Up/Down
3.20 Vehicle Pneumatics
3.30 RP-1 Drainback
3.40 Tank Purge
3,50 Post Static Fire Inspection
3.60 2nd Stage TVC Performance Check
3.70 2nd Stage TVC Polarity Check
3.80 Stage 2 TVC alignment
3.90 Bring down vehicle and roll into hangar
3.100 FTS Battery Charging
3.120 QD Disconnect
3.125 Merlin Purge Test
3.130 1st Stage Corrosion Inspections
3.140 Falcon Integrated Vehicle Checkouts
3.150 Terminal Count Dry Run
3.170 1st Stage TEA-TEB Changeout
3.180 TEA-TEB Flush
3.190 Firmware Update and Verify
3.200 1st Stage Polarity Check
3.210 Falcon 4 Ignition Inhibit Test
3.220 Vehicle Short-Term Storage
3.230 Orag On Instrumentation Installation and Removal
3.240 Hangar RF Receiving Equipment Setup
3.250 Stage 2 Combined Offload
3.260 Long Term Storage
Procedure
Number Description

D3-22



Section D
Attachment D1: Exhibit 1 (F9)

(~ LIST OF TABLES

Table D1-C: Vehicle Configurations oo. cceceeceereeeeeene

/

Table D1-H: Falcon 9 Standard Insertion Accuracy Requirements...
Table D1- I: Standard Payload Deployment -Attitudes/Rates
Table D1- J: Electrical Interface Minimum Wire Requirement:

NNK10L.802B

7 Table D1- J1: Falcon 9 Maximum Electromagnetic Radiation Levels Encountered on

(. Payload... eeeecccceceseseseecceeteees bessesteceeaneansesiens

Exhibit 1 (F9) - 3

ceseeeeeseenentenesesseneeness 38


Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
Procedure
Number Description
2.120 Interstage to 1st Stage Mate
2.125 Stage Mate
2.130 Hardware-In-The-Loop
2.140 ist Stage Aft Closeout
2.170 Tunnel Cover Install
2.175 1st Stage Avionics Bay Closeout
2.180 2nd Stage Aft Closeout
2.185 2nd Stage Forward Section Closeout
2.195 Separation System Checkout _
2.XxX Payload Fairing Delivery, Unpack, Inspect
2.XXX Fairing/Payload Adapter Checkout
2.200 Encapsulated Payload to Vehicle Mate
2.210 ist Stage Recovery System Install
2.213 Recovery System Charging and Activation
2.220 Falcon 9 Tank Purges
2.230 Vehicle to TE Installation
2.235 2nd Stage QD Install
2.240 Vehicle QD Install
2.245 Vehicle QD Leak Checks
2.917 FTS L-28 Day Pre-Flight Battery Test
2.930 FTS L-10 Day Pre-Flight Ordnance Interrupter Test and Installation
2.935 FTS L-10 Day Pre-Flight Safe and Arm Device Test and Installation
2.950 FTS Antenna System, DTB, CRD and Battery Installation
2.953 FTS Flexible Contained Detonable Cord Installation
2.955 FTS Linear Shaped Charge Installation
2.970 FTS RF System Check
2.973 LPI Pull Test and Installation
2.975 FTS Open Loop Test
2.980 Final Ordnance Connect and Pin Pull
3.015 Vehicle Weight and CG
3.020 Vehicle Power Up / Down
3.030 Vehicle Pneumatics
3.040 Post Static Fire Inspection
3.045 Falcon 9 TVC Bleed In
3.050 2nd Stage TVC Performance Check
3.060 Stage 2 TVC Alignment
3.075 1st & 2nd Stage Engine Fuel Drain & IPA Flush
3.085 Ast Stage TVC Single Engine Functional
3.090 Ignition Inhibit Test
3.160 Vehicle De-erect and Recycle
3.120 FTS Battery Charging
Procedure Description

D3-24



Section C
Contract Terms and Conditions NNK101L.B02B

28.2

28.3

28.4

29.0

29.1

(A)

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

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

29.2

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.

NASA Secondary Payload with NASA Primary Payload ~

(A) Procedures

C43


—_

Section D

Attachment D1: Exhibit 3 (F9) NNK10LB02B
19.3. The Contractor shall provide the capability.to provide ground processing
facilities for pavioads at the Wallops Flight Facility.
| |
_19.4 The Contractor shall provide the capability to provide ground processing
. facilities for Falcon 9 payloads at the Reagan Test Site (USAKA -
Kwajalein). Order BY. . ‘ ;
20.0 Additional Mission Analysis and Support
20.1 Reserved
20.2 Support for additional mission integration working group meetings in
excessofi BY - |
This can be procured at any time by the customer up until BY swith
° BY notice. Meetings are to be held at SpaceX facilities.
20.3 Reserved :
20.4 Performance and Guidance Accuracy Analysis
This can be procured at any time by the customer up until BY and
will require BY. to complete. SpaceX assumes format is per the NLS
{RFP CDRL.
20.5 Coupled Dynamic Loads Analysis
This can be procured at any time by the customer up until BY and
will require B{ to complete. SpaceX assumes format is per the NLS
» I}RFP CDRL. y
20.6 Pre-Flight Controls and Stability Analysis
This can be procured at any time by the customer up until BY and
will require : BY ‘to complete. SpaceX assumes format is per the NLS
<I RFP CDRL.
20.7. - Integrated Thermal Analysis .
This can be procured at any time by the customer up until BY’ land
will require RY ‘to complete. SpaceX assumes format is per the NLS
l)} RFP CDRL.
20.8 RF Link Analysis
This can be procured at any time by the customer up until Bd/ and
will require ®4  ,tocomplete. SpaceX assumes format is per the
NLS fl RFP CDRL.
20.9 Payload Fairing Clearance Analysis ;
This can be procured at any time by the customer up until BY \and
will require BY ... to complete. SpaceX assumes format is per the NLS
IT RFP CDRL.
20.10 Payload/Expended Stage Separation Analysis
This can be procured at any time by the customer up until BY and
will require BU to complete. SpaceX assumes format is per the NLS
. WRFPCDRL.
20.11 Analysis of ECS flow impingement on payload surfaces

This can be procured at any time by the customer up until 2 4 sand
will require RY to complete.

Exhibit 3 (F9) - 7


Section C
Contract Terms and Conditions NNK10LB02B

other impairment of health, or death of such person;

(iii) Claims for Damage caused by willful misconduct;

{iv) Intellectual property claims;

(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 shail 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.

C47


Section D

Review

Date

. Attachment D2: Contract Data Requirements List (CDRL) NNK40L802B
{tem Document Approval/ initial Submittal {Subsequent No. of

: CS: Engineering

Submittal Date {Copies

Vehicle Data Package

i
As Changed

C5-1* Review Bo"
IC5-2* {Mission Unique Hardware Test {Approval BY As Changed [4
Plan _ |
IC5-3* {Mission Unique Hardware Test Review RY AsChanged |4
Report 2
IC5-4* |Mission Specific Drawings Review As Generated per | As Changed /|4
" design review
criteria, but not
fater 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’ |initial Submittal |Subsequent No. of
Review

Date

Submittal Date |Copies

. |C6: Telemetry and

Communications

Vehicle and GSE Telemetry Review L-3M [As Changed with |2
Formats Configuration
IC6-2" {Vehicle and GSE Telemetry (Test, (Review Test + 1D; N/A 4
Pre-Launch, and Launch) Pre-Launch + 4D;
Launch + 4W.

* Required per mission

TABLE D2-A: CDRL INDEX (Cont.)

D2-5


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B

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.
1

(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

Attachment D3: Supplemental Data Requirements List NNK10L.B02B
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.

D3-18


SECTION D
ATTACHMENT D1
STATEMENT OF WORK

FALCON 9 Block 1 and Block 2


Section D .
Attachment D1: Exhibit 1 (F1/F1e)

NNK10LB02B

Bi
Redacked in

bs entirety.

Exhibit 1 (F1/F1e) - 39


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

LIST OF TABLES

Table D1-A: Mission Analyses to Support Payload Integration
Table D1-B: Mission Unique Hardware Factors of Safety......

Statement of Work (F9) - 3


Section C

Contract Terms and Conditions NNK10L.802B

3.0 LAUNCH VEHICLE CERTIFICATION

3.1. 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.

3.2 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.

(D) 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).

(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, regardiess 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


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK40LB02B

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

D249


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B

NASA RP-1124

NPR 2810.A

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

8.0 RESERVED

4
1997

2006

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

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

Statement of Work (F9) - 35


Section B
Table of Contents NNK10LB02B

SECTION B

STANDARD FORM 1449 CONTINUATION

TABLE OF CONTENTS
1.0 SCHEDULE OF SUPPLIES AND/OR SERVICES TO BE PROVIDED... B-1
11 Reserved.. B-1
1.2 Reserved... B-1
1.3 Reserved B-1
1.4 Reserved.. B-1
1.6 Special Task Assignment (Studies and Analyses) B-1.
1.6 IDIQ Launch Service Task Order (LSTO)......... B-2
1.7 NTE Prices - Standard Launch Services for IDIQ Missions. B-4
1.8 NTE Prices - Non-Standard Services for IDIQ Missions. .... . B7
2.0 TOTAL AWARD AMOUNT...
21 Total Contract Amount
3.0 RESERVED.. a. B-15

3.1 Reserved
3.2 Reserved.
3.3 Reserved..

4.0 MOST FAVORED CUSTOMER. ooo ceeccststteecse es severe BAS

5.0 IDIQ LAUNCH SERVICE AND PRICE UPDATES...

6.0 SPECIAL TASK ASSIGNMENTS (STUDIES AND ANALYSES
(CLIN 10) — DEFINITIZED... ee teeter B-16

B-i Modification 002


Section D
Attachment D1: Exhibit 1 (F1/F1e)

-___ NNK10LB02B

BY
Redacted 10

\ fs en f cel

Exhibit 1 (F1/F1e) - 23


Section B

Standard Form 1449 Continuation

NNK10LB02B

NON-STANDARD SERVICE ITEM (Falcon 1 & 1e)

NOT TO EXCEED (NTE) PRICE ($) IN CALENDAR YEAR ORDERED*

# irom Item description 2010 (Jul-Dec) 2017 2012 2013 2074 2015 2016-2022
Exhibit 3
encapsulation up to 1-0 |
118 SIC Grade C Nitrogen (GN2) IAW MIL-PRF-27401F A
Purge System
41.7 ‘Enhanced PLF and PLA Cleaning IAW IEST-STD-
CC1246D level 500A
18 Certified Portable Class 7 Clean Enclosure(s) for Open TEP
PLF Access Doors
42 Reserved
or) Go manifested Payload mission service TBP
14 NASA Secondary Payload Mission Service TSP
8 Payload Compatibility Assessment . TEP
16 Secondary Payload Mission Feasibility Study TEP
7 Secondary Payload accommodation study q TEP
418 Secondary Payload Mass simulator TBP
oT) Payload Processing facilities
19.7 Contractor shall provide capability to provide ground TSP
processing facilities for payloads at the Eastem Range
19.2 Contractor shall provide capability to provide ground TaP
processing facilities for payloads al the Westem
Range —
19.3 Contractor shall provide capability to provide ground TBP
processing facilities for payloads at the Wallops Flight
Facility
194 Contractor shall provide capability to provide ground TSP
processing facilities for payloads at the Reagan Test
Site (USAKA- Kwajatein)
20 Additional Mission Analysis and Support
20.1 Reserved ‘TBP
20.2 Support for additional mission integration working TeP
group meetings in excess of four per calendar year
20.3 Reserved ¥ :
20.4 Performance and Guidance Accuracy Analysis TBP



Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
4.10 EGSE Checkout
4.30 Hydraulic GSE Proof, Leak, functional
4.31 Hydraulic Accumulator Check and Fill
4.35 Launch Mount Maintenance Erection
4.40 LOX Proof and Leak
4.41 RP-1 Proof and Leak
4.42 Helium System Proof and Leak
4.45 GN2 Proof and Leak
4.46 Water Proof and Leak
4.47 TVC Proof and Leak
4.50 Launch Site Consumables Management
4.51 Fluid GSE Pre-connect Flush
4.60 Launch Site Setup/Shutdown
4.61 RP-1 Filtering and Heating
462 RP-1 Steam Heating
4.70 GCS System Setup
4.80 Payload Environment Monitoring
4.90 Launch Camera Setup
4.95 Facility Vehicle Hold Down Test
§.20 PAA Integration
The Falcon 9 Block 1/Block 2 Procedure List
Procedure
Number Description
1.030 Optical Azimuth Alignment
1.080 1st Stage Engine Alignment
1.090 1st Stage TVC Polarity Check
1.110 2nd stage TVC Functional
1.140 Vehicle Rollout and Launch Preparations
1.150 Final Preps for Launch (Vehicle and Pad)
1.160 Countdown
2.010 Stage Delivery, Unpack & Inspect
2.015 MVac Skirt Delivery, Unpack & Inspect
2.040 1st Stage Avionics Check-out
2.050 ist Stage Propulsion Check-out
2.060 2nd Stage Avionics Check-out
2.070 2nd Stage Propulsion Check-out
2.080 2nd Stage Polarity
2.100 TEA-TEB Canister Installation
2.110 interstage Closeout
2.115 MVac Skirt Install

D3-23



Section D
Attachment D1; Exhibit 1 (F9) . NNK10LB02B

Qu |

Configuration |

Table D1-C: Vehicle Configurations

2.0 PAYLOAD DELIVERY CAPABILITY

* SpaceX has provided where applicable, in Tables D1-D through D1-G3, the maximum
payload capability from appropriate launch site with associated ground rules for the two
configurations of the Falcon 9 launch vehicle (Block 1 and Block 2). The Block 1 launch
vehicle was part of the previous NASA Launch Services catalog, before the contract
period of performance expired. The configurations are defined in paragraph 1.0, Vehicle
Configuration. Performance is expressed in terms of payload mass plus payload
separation system — see Performance Ground Rule #1 on page ‘Exhibit 1 (F9)-9 and
shall assume a 3-sigma performance reserve for the following orbits:

Low Earth Orbits (LEO): Data shall be provided for circular orbit altitudes from 200 to
2000 km (in increments of 100 km) for inclinations of 0, 5, 10, 20, 28.5, 38, 51.6, 60, 70
and 90 degrees.

Sun-Synchronous Orbits: Data shall be provided for circular orbit altitudes from 200 to
2000 km.

High Energy Missions: Data shall be provided as a function of C3 from —10 km/sec? to
200 km*/sec*.

Elliptical Orbits: Data shall be provided as a function of apogee altitude and inclination
using the launch vehicle's standard ground rules. In addition, provide performance with
a perigee altitude of 2000 km. :

Geo-Synchronous Orbits (GSO): Data shall be provided for.insertion directly into Geo-
Synchronous Orbits (GSO).

BY - =: --

Exhibit 1 (F9) -7


Section D

Attachment D1: Statement of Work (F9) ; NNK10LB02B

(G)
(H)
()

(J)
(K)

(L)

(M)

(N)

(0)

(P)

Coordinate interface and support requirements for the mission.
Plan/coordinate mission specific flight operations.

Manage integration activities at the launch site.

Manage and coordinate the launch vehicle safety approval process.

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.

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.

Evaluate 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 (GOWG’s) approximately 2 times a
year from L-27 months to spacecraft arrival at the launch site and at the

NASA Ground Operations Review (GOR).

Statement of Work (F9) - 18


AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT TCONTRAGTID CODE PACE eo
2. AMENDMENT/MODIFICATION NO. ‘3. EFFECTIVE DATE 4. REQUISITION/PURCHASE NO. 5. PROJECT NO. (!f applicable)
002 See Block 16C 4200369828 NLSIL-S
6. ISSUED BY , CODE OP-LS 7. ADMINISTERED BY (ifother than item 6) CODE
John F. Kennedy Space Center, NASA
Procurement Office/Expendable Launch Services Support Office Same as Block 6
Attn: OP-LS/Helena Wilkas “
Kennedy Space Center, Florida 32899

@. NAME AND ADDRESS OF CONTRACTOR (No., sireet, county, State and Zip Code) (LJ [84 AMENDMENT OF SOLICITATION NO.
Space Exploration Technologies ‘9B. DATED (SEE ITEM 11)
1 Rocket Road DX) ica MODIFICATION OF CONTRACTIORDER NO,
Hawthome, CA 90250 " NNK10LB02B .
(310) 363-6229 . HOB. DATED (SEE ITEM 13)

CODE 3VBL8 [racury cope September 24, 2010

41. THIS [TEM ONLY APPLIES TO AMENOMENTS OF SOLICITATIONS

(1 The above numbered solicitation is amended es set forth in Item 14, ‘The hour and date specified for receipt of Offers [_]is extended, [_]s not extended,
Offers must acknowledge receipt of this amendment prior to the hour and date specified in the sollcliation or as amended, by one of the following methods:

(a) By completing Items 8 and 15, and retuming __ copies of the amandment; {b) By acknowledging receipt of this amendment on each copy of the offer submitted; or
(©) By separate letter or telegram which includes a reference to the solicitation and amendment numbers, FAILURE OF YOUR ACKNOWLEDGEMENT TO BE
RECEIVED AT THE PLACE DESIGNATED FOR THE RECEIPT OF OFFERS PRIOR TO THE HOUR AND DATE SPECIFIED MAY RESULT IN REJECTION OF YOUR
OFFER. iby virtue of this amendment you desire to change an offer already submitted, auch change may be made by telegram or letter, provided each telegram or latter
makes reference to the solicitation and this amendment, and Is recelved prior to the opening hour and date specified.

12. ACCOUNTING AND APPROPRIATION DATA (If required)

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

[| 4 _ [THIS CHANGE ORDER IS ISSUED PURSUANT TO (Speoty authority)
Cl [THEABOVE NUMBERED CONTRACT/ORDER IS MODIFIED TO REFLECT THE ADMINISTRATIVE CHANGES (Such as changes in peying

office, appropriation data, etc.) SET FORTH IN ITEM 14, PURSUANT TO THE AUTHORITY OF FAR 43.103(b).

[THIS SUPPLEMENTAL AGREEMENT IS ENTERED tNTO PURSUANT TO AUTHORITY OF: NFS 1852.232-77 Limitation of Funds (Fixed- Price
 [Contract)(Mar 1989) and FAR 52.243-1 Changes-Fixed Price (Aug 1987) Alt 1 (Apr 1989)

D IOTHER (Specify type of modification and authority)

E. IMPORTANT: Contractor <1 is not, [_] is required to sign this document and retum 4. copies to the Issuing office.
74. DESCRIPTION OF AMENDMENTIMODIFICATION (Organized by UGF section headings, Including sollcitalion/contract subject matter where feasible.)

See Page 2

Except a3 provided herein, ail terms and conditions of the document referenced in Item @A or 104, as heretofore changed. remains ut 2nd wn full force at fect.

15a. NAME AND TITLE OF SIGNER (Type or print) 6a. NAME AND TITLE OF CONTRACTING OFFICER (Type or print)
John Vondenhueve!
Contracting Officer

168. CONTRACTOR/OFFEROR 15C. DATE SIGNED —_|4@B. UNITED STATES OF AMERICA 16C. DATE SIGNED.

BY. IBY.

(Signature of person authorized to sign} {Signature of Contracting Officer}
ISN 7540-01-162-8070
PREVIOUS EDITION NOT USABLE soos STANDARD FORM 30 (Rev. 1945

ssenbad by’
FAR (48 CFR] $3 243,



Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B

CDRL DESCRIPTION Number: C1-2 (cont)

(C)

(iii) Range requirements
(iv) Collision avoidance (COLA)
(v) 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 shail 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.

02-8


Section D
Attachment D3: Supplemental Data Requirements List NNK10LB02B

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.

D3-27


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B

(B

(C

0)

addition, the temperature and humidity environment shall have the ability to
be controlled and maintained within a range of BY Jand
30% to 60%, 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 !AW 2.4.2.3(B) or (C),
herein. If the Contractor provides a payload protective cover as identified in
paragraph 2.4.2.2(K) of the SOW, and purge air has been established, the
facility environment may be exceeded. Prior to removal of the payload
protective cover, the facility shall be returned to a Class 8 JAW ISO 14644-1
clean room environment. 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. Fottowing payload encapsulation,
the transportation container shall be purged with conditioned filtered air and
the payload environment shall be maintained within a temperature and
humidity range of “B44 ) and 30% to 60%, respectively.
The Contractor shall identify periods or configurations where the temperature
and humidity requirements cannot be met. 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.

Fairing Environment. Following fairing installation and payload mate to the
launch vehiclé, the PLF environment shall be purged with conditioned filtered
air and shall maintain a temperature set point range, selectable by the
payload,of ~  B4 ), controllable to B84 ., through T-
0. Relative humidity shall be maintained within 30% to 50%, controllable to
5%. The Contractor shall identify periods or configurations where the
temperature and humidity requirements cannot be met. 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, GNz (or better) IAW MIL-PRF-27401F, may be used for purging the
fairing environment. Fairing GN2 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 (including Payload Adapter)
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

Statement of Work (F9) - 26


Section D
Attachment D1: Exhibit 1 (F9) oa NNK10LB02B

BY

Rede cled i)
| its entirety

Exhibit 1 (F9) - 45


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
CDRL DESCRIPTION Number: C3-5

QMS AND SUPPLIER/VENDOR AUDIT/AS SESSMENT 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/assessment, 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 D

Attachment D1: Statement of Work (F9) NNK10LB02B
Application Test Analysis (No Test)
Yield Ultimate Yield Ultimate
Non-Man Rated 1.10 1.25 1.60 2.0

4.2

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

Statement of Work (F9) - 32


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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 1CD 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 Controi 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) A Lightning 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.

02-42


Section C
Contract Terms and Conditions NNK10LB02B

(D) LSTO Proposal Evaluation/_STO 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:

{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.

(iii) 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.

C-26


Section D
Attachment D1: Exhibit 1 (F9) NNK10LB02B

BY
Redacted A
( {. entirety

Exhibit 4 (F9) - 47


Section D “
Attachment D1: Exhibit 1 (F9) NNK10LB02B

BH

R edacked |
\ Ls sa cy

Exhibit 1 (F9) - 9


Section D :
Attachment D1: Exhibit 1 (F9) NNK10LB02B

BU

R odackedk on
its entirety

Exhibit 1 (F9) - 26


Section B

Standard Form 1449 Continuation NNK10LB02B

NON-STANDARD SERVICE ITEM (Falcon 1 & 1e) NOT TO EXCEED (NTE) PRICE ($) IN CALENDAR YEAR ORDERED* 7
# from Tiom description 2016 (Jul-Dec) 2077 012 2013 2018 2018 2016-2022
Exhibit 3 -

44 Bespin system with enhanced capability | TBP

45 Improved insertion accuracy options TBP
5 Multiple PA, including Related Mission Integration TBP

Support
6 ‘Secondary PA for Non-Separaling Secondary Payload Tap |
7 Secondary PA/Sep systems for Separating Secondary Payload
TA ‘Secondary Payload Adapter (with S/C-provided ~~ TSP
‘separation system)
72 Secondary Payload Adapter (with contractor-provided Te
‘separation system)
Ey | RF Through-the-Fairing Transmission Capability TBP
g Enhanced electrical interface

a4 increased capacity payload-to-GSE interface TSP

o2 (V command and contral of payload TBP

93 LV supplied payload power capability TEP

94 Enhanced (iMbps) Telemetry capabilities including TEP

interleaving/deinterteaving of payload telemetry data ,

95 ‘Additional LV environmental instrumentation ~TeP
40 LW mounted cameras (see Exhibit 3, paragraph 10.0) TBP
44 ‘Special contamination control options ~

14 Enhanced Fairing environment TEP

1.2 Enhanced fairing internal surface cleaning (IEST-STD- TBP

CC1246D Sevel 500A)
13 “Optional payload/venidle integration environments TEP
114 Additional instrument purge systems up to 1-0 (IEST- TEP
STD-CC1246D level 100A)
115 Grade B Nitrogen (GN2) IAW MIL-PRF-27401F of TBP

conditioned air cooling supply for spot caoling of
| payload components from payload mate or



Section D :
Attachment D1: Exhibit 1 (F9) : NNK10LB02B

BM

R e Sa CO ed. m
its entir et Y

Exhibit 1 (F9) - 40


Section C
Contract Terms and Conditions NNK10LB802B

8.0

8.1

8.2
8.3

8.4

85

9.0

9.1

92

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

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:

(i) Statement of Work

(ii) Required Completion Date
(iii) Government Point of Contact

c-20


Section D

Attachment D2: Contract Data Requirements List

CDRL DESCRIPTION

Power Received Above Noise (48) .

(G) Descriptive contractor recommendations to mitigate any risks identified by this
analysis.

DRL

NNK10LB02B

Number: C4-9 (cont)

[MISSION] [VEHICLE SYSTEM] LINK ANALYSIS
[LAUNCH DATE] [GROUND STATION] [ANTENNA]

RHC
7

LHC.
VERT or HORIZ

Show Significant Events

LINK DATA

Vehicle Transmitter Power (W)

Ground Antenna Location (HT, LAT, LON):
Vehicle Losses (dB): [TM]

Noise Bandwidth (kHz): {TM]

Ground Station G/T (4B): [TM)

Vehicle Transmitter Frequency (MHz): [TM]
Bit Rate (kBits/Second): [TM]

| Ground Station Loss (dB): [CRD]

Ground Antenna Gain (48): [CRD}
Vehicle Losses, CRO (48): (CRD}

CRD Threshold {:V): [CRD]

Frequency (MHz): {CRD]

Uplink Frequency (MHz): [C-band]
Reply Frequency (MHz): [C-band]
Radar EIRP (dBm): [C-band]
Transponder Sensitivity (dBm): [C-band

Show Significant Events

200 300 400 500 600 700 800 S00 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200
Time from fiftoff (2ec)

Figure D2-1: Power -Vs- Plus Count Time

D241



Section D . .
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

NASA RP-1124 4 . Outgassing Data for Selecting Spacecraft Materials r )
: 1997

NPR 2810.A ° 2006 Security of Information Technology

NASA-STD- . Planning, Developing and Managing an Effective Reliability

8729.1 - and Maintainability (R&M) Program

NPD 8610.23 Launch Vehicle Technical Oversight Policy

NPD 8610.24 Launch Services Program (LSP) Pre-Launch Readiness
Reviews :

NPD 8610.7 Launch Services Risk Mitigation Policy for NASA-Owned
and/or NASA-Sponsored Payloads/Missions

LSP-PLN-324.01 Expendable Launch Vehicle Certification

NPR 8621.1 : NASA Procedural Requirements for Mishap and Close Call
Reporting, Investigating, and Recordkeeping

LSP-PLN-353.01* “Launch Services Program Risk Management Plan

NPD 1280.1 NASA Management System Policy @

NPR 7120.5 NASA Space Flight Program and Project Management
. Requirements

NPR 8715.3 NASA General Safety Program Requirements

' MIL-STD-1773 may be substituted

8.0 RESERVED

Statement of Work (F1/F 1e) - 33



NNK10LB02B



Section C

Contract Terms and Conditions NNK10LB02B
38.0 __ RESERVED... . C-60
39.0 _ SPECIAL UNDERSTANDING REGARDING DAMAGE TO GOVERNMENT
PAYLOADS ............sssesescssssessssssssssesenesssssesssesesssssarecseneesssacospssssnessscseneess C-60
40.0 SPECIAL UNDERSTANDING REGARDING LIABILITY FOR THIRD PARTY
CLAIMS FOR NUCLEAR INCIDENTS. ...........:esescssssstsssssssesssssssssesescnensstes C-60
41.0 DEPARTMENT OF ENERGY (DOE) 952.250-70 NUCLEAR HAZARDS
INDEMNITY AGREEMENT (JUN 1996).. .. C-60
42.0 _1852.228-78 CROSS-WAIVER OF LIABILITY FOR SCIENCE OR SPACE

EXPLORATION ACTIVITIES UNRELATED TO THE INTERNATIONAL
SPACE STATION (DEVIATION) (OCT 2009) .......css.sssssscsessessessseseesteeees C-64

C-iii


Section D
Attachment D3: Supplemental Data Requirements List

NNK10LB02B

SDRL S1-1 Data . ~
Request

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

AS

BY

(E) Environmental
Monitoring Equipment

D3-5



Section B
Standard Form 1449 Continuation NNK10LB02B

2.0

3.0
3.1

3.2

3.3

4.0

5.0

TOTAL AWARD AMOUNT

The guaranteed minimum value of this contract is $20,000. The maximum
potential value of contract number NNK10LB02B is $15,000,000,000. The total
maximum potential value of all NLS contracts combined is $15,000,000,000.

RESERVED
Reserved
Reserved

Table B-11: Reserved
Reserved

Table B-12: Reserved
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.

IDIQ LAUNCH 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 faunch 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


Section B
Standard Form 1449 Continuation NNK140LB02B

1.7

NTE Prices - Standard Launch Services for IDIQ Missions

The Government shail 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.


Section D

Attachment D1: Statement of Work {F9) NNK10LB02B

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. Ail 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,

(ix)

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

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

Statement of Work (FQ) - 11


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
CDRL DESCRIPTION Number: C5-1 (cont)

(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

D2-48


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
CDRL DESCRIPTION Number: C1-3
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:

(A) Terminal or abbreviated countdown procedure
(B) Flight sequence of events

(C) Range, paytoad, launch vehicle mandatory items
(D) Communication channel matrix

(E) Down-range telemetry coverage plan

(F) Launch window for all possible attempts

(G) Launch decision flowchart

(H) Control center seating

(1) Call sign matrix

(J) Protocol for cailing holds

(K) Day of launch winds plan

D2-9


Section D
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

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.

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, and payload communication
accommodations 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.

Statement of Work (F1/F1e) - 23


Section C

Contract Terms and Conditions NNK10L802B

(B)

(C)

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 Officer. Once reviewed, the policy or policies may not be
modified or canceled without the prior, written approval of the Contracting
Officer.

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)

(B)

(C)

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.

C-50


Section D
Attachment D1: Exhibit 1 (F9) ! NNK10LB02B

R olacted cn

its eatir oty :

Exhibit 1 (F9) - 8


Section C
Contract Terms an nditions NNK10LB02B

(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 shail 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

C-4


Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
Number

3.140 Terminal Count Dry Run

3.145 Software Dry Runs

3.150 LC-40 Fluid Systems Hurricane Preparations

3.160 LC-40 Vehicle and Hangar GSE Hurricane Preparations

3.180 Aft Thermal Shield Installation

3.190 Integrated Vehicle Removal From TE

3.200 1st Stage / 2nd Stage De-Mate

3.2xx Encapsulated Payload De-Mate

3.310 2nd Stage IMU to Porro Prism Alignment -

4.010 GCS Startup

4.020 Stage Support Rack Checkout

4.040 Launch Camera Setup

4.060 LC-40 Safety System Inspections

4.210 Hangar Grounding Systems Checkout

4.220 Complex 40 Catenary System Inspection

4.230 Hangar Crane Inspection, Testing and Maintenance

4.310 Hangar Leak Check Cart Checkouts

4.413 Payload Environments Monitoring

4.420 General Site Operations

4.450 TE Hydraulics Operations

4.500 Launch Site Setup

4.513 RP-1 System Storage Tank Replenish

4.514 RP-1 System Storage Recirculation/Conditioning

4.583 LN2 Storage Tank Replenish

4.593 TEA-TEB Run Tank Replenish

4.900 Ordnance Handling Instructions

D3-25



Section D
Attachment D1: Statement of Work (F9) NNK10L802B

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 real-time launch vehicle and GSE telemetry (RF and
hardwire) data to the NASA designated NASA LSP Data Center. Examples
include, but are not limited to telemetry test data during initial vehicle power-up,
flight simulation prior to payload mate, and flight simulation following payload
mate (SDRL S6-3).

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 S$5-1).

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 shail 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 contro! 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.

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.

Statement of Work (F9) - 22


Section D :
Attachment D1: Exhibit 1 (F9) wo NNK10LB02B

BY

Red, hed in ’
its entirely

Exhibit 1 (F9) - 39


Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
SDRL 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 to NLT fifteen (15)
calendar days prior to launch and at the Flight Readiness Review.

D3-29


Page 2 of 2
NNKIOLB02B
Mod. No. 002

({tem 14 Continued)

The purpose of this modification is to definitize Task Assignment NLSII-S-00), increase Contract
value, and provide funding for the Task Assignment. j

Accordingly,

A. Section B, Clause 2.1 Total Contract Amount is added to reflect a total firm-fixed-
price of! GY _!for all definitized work under this contract.

B. Section B, Clause 6.0 SPECIAL TASK ASSIGNMENTS (STUDIES AND
ANALYSES) (CLIN 10) - DEFINITIZED is added to reflect definitized Task
Assignment NLSII-S-001. The total hours are increased from 84 | and the total
firm-fixed-price for CLIN 10 is increased from ! By '

C. Section B, TABLE OF CONTENTS, is revised to add Section 2.1 Total Contract
Amount and Section 6.0 SPECIAL TASK ASSIGNMENTS (STUDIES AND
ANALYSES) (CLIN 10) - DEFINITIZED.

D. The following contract change pages are provided and incorporated herein:
Section B: pages B-i, B-15.1, B-16, and B-16.1

E. Except as provided herein, all other terms and conditions of Contract NNK10LB02B
remain unchanged and in full force and effect.

The parties hereto agree that this supplemental agreement represents a complete and equitable
adjustment for the definitization of Task Assignment NLSII-S-001 listed in this contract
modification, including all revisions, authorized under CLIN 10 of this contract. The Contractor
hereby releases the Government from any and all liability under this contract for further
equitable adjustments attributable to such facts or circumstances giving rise to Task Assignment
NLSII-S-001 fisted in this contract modification, that were agreed to as written,

(End of Modification 002)


Section B

Standard Form 1449 Continuation NNK10LB02B
NON-STANDARD SERVICE ITEM (Falcon 9 Bik 1 & 2) NOT TO EXCEED (NTE) PRICE ($) IN CALENDAR YEAR ORDERED*
from | item description 2010 (Jur 201% 2012 2073 204 2015 2016-2022
Exhibit 3 Dec)
3A Different size or different payload interface Pas - = 7 ° TEP
32 Tow tip-off rate PAs “TBP |
[3 ip
4 Upper stage hardware
44 Motor ] 7 TBP
| 42 PA + ( TP]
43 ‘Spin system with enhanced capability — ~ wa TEP
a4 Bespin system with enhanced capability TBP
—_ |
45 improved insertion accuracy options TeP
E Multiple PA, including Related Mission Integration TBP
Support
6 ‘Secondary PA for Non-Separating Secondary Payload j : __e
1
7 Secondary PAlSep systems for Separating Secondary Payload
TA Secondary Payload Adapter (with S/C-provided ee TBP
separation system)
72 ‘Secondary Payload Adapter (with contractor-provided TBP
separation system)
8 RF Through-the-Faiing Transmission Capability TBP
9 Enhanced electrical interface an 7 :
oF increased capacily payload-to-GSE interface _ ———__ TEP
92 LV command and control af payload i Tap
EX) LV supplied payload power capability
o4 Enhanced (IMbps) Telemetry capabilities including
interleaving/deinterleaving of payload telemetry data
95 ‘Additional LV environmental instrumentation
10 LV mounted cameras (see Exhibit 3, paragraph 10.0)
7 Special contamination control options
T14 Enhanced Fairing environment
112 Enhanced fairing intemal surface cleaning (lEST-STO-
C1246D level 500A)
1713 Optional payload/vehide integration environments
14 ‘Additional instrument purge systems up to T-0 (IEST-
STD-CC1246D level 100A)



Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

2.4 Launch Site Support

2.4.1 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 access to all meetings including, but not limited to, scheduling
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

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 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

Statement of Work (F9) - 20


Section D
Attachment D3: Supplemental Data Requirements List NNK10LB02B

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.

D3-19


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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. !t 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

D2-53


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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/launch 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

(G) A list of all procedures used for vehicle and integrated processing with brief
description of their purpose.

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 procedures, ready for NASA approval, must be provided
to NASA 1 week prior to use.

D2-52


Section D

Attachment 03: Supplementat Data Requirements List : NNK10LB02B
[ SDRL S1-1 Data RQ B ai ;
Request . Y . :

(K) Support Space

03-9


Section D
Attachment D1: Exhibit 1 (F1/F te) ; NNK10LB028

8.0 PAYLOAD ENVIRONMENT

The Contractor shall provide data for the maximum payload acoustic, vibration, shock,
and acceleration, and thermal environment levels during launch and ascent. The
maximum electromagnetic radiation levels encountered by. the payload shall be
depicted in Figure D1-3. The Contractor shall illustrate the pressure profiles and
depressurization rates for each PLF in Figure D1-4. The maximum expected payload
flight environments: due to acoustics (50% fill), vibration; and. shock shall be shown in
Tables D1-K, D1-L, and D1-M, respectively. The maximum expected total acceleration
(limit load factors), including uncertainty factors, shall be shown in Table D1-N (key
dynamic events may be broken out as appropriate). The maximum expected sinusoidal
vibrations at the base of the PA shall be shown in Table D1-O. The maximum quasi-
steady acceleration as a function of payload separated mass shall be shown in Figure
01-5. The Contractor shall provide the maximum thermal environment during ascent for
every launch component (i.e., upper stage, unblanketed skin, thermal/acoustic blankets,
etc.) inside the fairing with a view factor to the payload in Figure D1-5A.

Falcon 1/1e Launch Vehicle RF System Characteristics

Payload customers must ensure that spacecraft materials or components. sensitive to
an RF environment are compatible’ with both the launch pad ¢ environment and the RF
environment during flight. oo.

S

Exhibit 1 (F1/F1e) - 28

ty,


Section D
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B

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. Ata 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.

D2-44


Section C
Contract Terms and Conditions NNK10LB02B

2.0
2.1

“Suspension of Payment” paragraph of the electronic funds
transfer (EFT) clause of this contract.

(3) 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
tecord 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.

(4) Offerors and Contractors may obtain information on registration and
annual confirmation requirements via the Internet at http:/Avww.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 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 {SO 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.


Exhibit 1 (F1/Fte)-10



Section D
Attachment D1: Exhibit 3 (F9) . NNKi0LB028

16.0 Secondary Payload Mission Feasibility Study Order . BY

A secondary payload mission feasibility study shall assess the
performance capability and payload volume available to accommodate
secondary payload missions on a non-interference basis with a given
primary mission. Separating and non-separating secondary payloads shall
be accommodated as a non-standard service.

SpaceX offers this as a non-standard service.

17.0 Secondary Payload Accommodation Study Order BY ;
i
A secondary payload accommodation study shall address the suitability of
_ and the approach for accommodating secondary payloads on a given
vehicle configuration. The study shall develop a design, general payload
requirements (secondary payload interface, volume, mass, environments)
and implementation scheme for implementing both separating and/or non-
separating secondary payloads. Dynamic loading analysis for generic
secondary payloads shall be performed so that mission unique analyses
are minimized.
GY

18.0 Secondary Payload Mass Simulator

A mass simulator shall be designed and fabricated to match the
requirements (e.g., moment of inertia, rigidity, mass, and CG) of the
secondary payload that will be replaced. The mass simulator shall also
adhere to the requirements (e.g., contamination, cleanliness, and
interface) identified in the ICD. The Contractor shall complete any other
analyses or documentation required, for replacement of the secondary

payload with the mass simulator.
BY

19.0 Payload Processing Facilities

19.1. The Contractor shall provide the capability to provide ground processing
facilities for payloads at the Eastern Range.
SpaceX shall provide the capability to provide non hazardous ground
pracessing facilities for payloads at the Eastern Range in excess of the
BY. included in the By service. SpaceX requires that this be
procured with atleast BY ~ < notice.

19.2 The Contractor shall provide the capability to provide ground processing
facilities for payloads at the Western Range.
SpaceX shall provide the capability to provide nonhazardous ground
processing facilities for payloads at the Western Range in excess of the

BY included in the standard service. SpaceX requires that this be

procured with atleast BY . notice. :

Exhibit 3 (F9) - 6


Section D :
Attachment D1: Exhibit 1 (F1/F1e)

NNK10LB02B ©

134

B ed act el | cn
ts ontivety

Exhibit 1 (F1/F1e) - 30


Section D
Attachment D3: Supplemental Data Requirements List

NNK10LB02B

SDRL S1-1 Data 4

Request
(l) Processing Space
Floor Capability i

RE

BY

TS,

(J) Processing Space
Size

D3-8



Section D
Attachment D1: Exhibit 3 (F9) NNK10LB02B

EXHIBIT 3

NON STANDARD LAUNCH SERVICES LIST for Falcon 9

SpaceX shall provide the capability to perform the following non-standard
services. This information is provided in response to the instructions in the NLS
I) RFP. These services shall be performed for each mission, as requested and
authorized by the NASA Contracting Officer, in accordance with the contract
terms and conditions. Each non-standard item listed shall include. all hardware,
software, analyses, and support required to provide the service. Any impacts to
the capabilities or conditions defined in Exhibit 1 introduced by the non-standard
service shall be explained in detail. The Contractor shall not be required to
design and develop a non-standard service in support of this contract.

The Contractor shall list all non-standard services provided for each proposed
launch vehicle configuration, which will be negotiated and incorporated into the
contract. All non-standard services provided shail be fully compliant with the
SOW. Any non-standard services provided that are not fully compliant shall be
designated as such in the proposal with details supplied as to the impact of
making the service.compliant. All proposed non-standard services shall have an
associated, no-later-than ordering date with respect to the launch date. In
addition, the Contractor shall provide any non-standard services deemed useful
for future NASA missions based on past experience. :

If authorized, the Contractor shall implement the following services:

1.0 Alternate Vehicle Configurations or Performance Enhancements (i.e.,

Extenda Nozzles, Additional Motors/Thrust Augmentation) — B4/
RU :

2.0 Alternate Fairing Configurations and/or Modifications

2.1 Alternate configurations

2.2 Additional access doors in excess of three included in standard service.
SpaceX offers up to three doors/RF windows in the payload fairing as a
standard service. Limitations on location can be provided (for example,
doors cannot be located in proximity to the fairing separation split line).
This option must be order RY from launch.

2.3. Access doors of non-standard size
SpaceX offers a non-standard size door of 36 inches by 24 inches.
Limitations on location can be provided (for example, doors cannot be
located in proximity to the fairing separation split line). This option must
be order BY from launch.

2.4 Mounting provisions, cabling and antenna systems for re-radiating signals
from the. payload to remote sites— &

2.5 §,C, X; and Ku-band re-radiation equipment - Y

Exhibit 3 (F9) - 2


Section D

Attachment D1: Exhibit 3 (F1/F1e) NNK10LB02B

21.0 Reserved

21.1 Reserved

21.2 Reserved

21.3 Reserved

22.0 NASA Public Affairs Office Support
Accommodations for NASA guests, 84 ~~, to view launch, including
local transportation, launch viewing facilities, lavatory accommodations,
food and beverage service, first aid and medical support for each
proposed launch site.

23.0 Launch Service Contractor (LSC) provided Telemetry
The LSC shall provide all telemetry data (main vehicle telemetry and
special instrumentation/wideband telemetry system) [AW LSP-PD-120.05,
“Launch Telemetry Requirements.”

BU
24.0 Launch Service Contractor (LSC) provided Telemetry Acquisition

Assistance Message (AAM) Order! 8&4

The Contractor shall provide Acquisition Assistance Messages (AAMs) to
the down-range telemetry sites utilized by the mission for antenna pointing
to acquire launch vehicle telemetry and to payload-designated control
centers/telemetry sites for acquisition of space vehicle telemetry. The
Government utilizes down-range telemetry sites to receive record and
relay telemetry data from the Contractor's launch vehicle in accordance
with LSP-PD-120.05, “Launch Telemetry Requirements.” Mission-specific
telemetry sites are selected to acquire data from the launch vehicle during
the launch, powered-flight, and spacecraft separation phases of the
mission. These telemetry sites may be owned/operated by NASA, the
DoD, a U.S. commercial entity, or a foreign entity.

Generation of the AAMs will be treated as no greater than REQUIRED
capability for launch commit criteria purposes. Should any greater
capability be imposed, then the requirements to meet that greater

_ capability shall be considered outside the scope of this NSS and subject to

a separate contract action.

Format for AAMs will bein accordance with industry standard.

RY

Exhibit 3 (F1/F te) - 8


Section D

Attachment D1: Statement of Work (F1/F1e) NNK10LB028

8),

(vii) Mass properties.

(viii) Environmental requirements (e.g., thermal, contamination, vibration,
pressure, Electromagnetic Compatibility (EMC), shock, launch complex
RF, and lightning).

(ix) Orbital requirements, launch vehicle performance, launch window
injection, and deployment attitudes and rates.

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

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 shail 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 unproved
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.

Statement of Work (F1/F te) - 14



Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

2.3.2

2.3.3

Mission Analyses

Ail 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 Therma! 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 Repost

C4-13 | Final Flight Report

Table D1-A: Mission Analyses to Support Payload Integration

The standard launch service shall include all analyses required to evaluate
compliance with 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.

Statement of Work (F9) - 19



Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10L802B
CDRL 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 shail
include:

(i) Due Date

(ii) Subject

(iit) 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

D2-6


Section D :
Attachment D1: Statement of Work (F1/F1e). NNK10LB02B

e@ Statement of work
1.0 INTRODUCTION

1.1 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°. [NOTE: The information contained in this SOW pertains to
_both the Falcon 1 and Falcon 1e Launch Vehicle configurations.]

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 to safely and reliably launch payloads in accordance
with NASA-defined mission objectives. The Contractor shall support advance
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.

1.2 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.

« . 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.

@ e Provide risk mitigation while utilizing commercial practices.

Statement of Work (F1/F1e) - 4


Section D
hment D2: Contract Data Requirements List (CDRL NNK10LB02B

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
tisks as an integral part of the Contractor's management and decision process.

e information that illustrates the functional relationships and lines of communication,
including the involvement of sub-contractors and major vendors.

e 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.

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

B. Risk reports shall be delivered quarterly (at a minimum) to the COTR. The reports
shall include allt 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.

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

D2-30


Section D ”
Attachment D1: Exhibit 1 (F9) i” NNK10LB02B

BY

R cduact el oy
its entirety

Exhibit 1 (F9) - 19


Attachment D1: Exhibit 1 (F1/F1e) a NNK10LB02B

Exhibit 1 (F1/F1e)-37


Section D
Attachment D3: Supplemental Data Requirements List NNK10LB02B

| SOR S#-4 Data RY Bef
BY

(N)} Security Systems |

=

(O) Mechanical Support

Equipment (Lifts, etc) pu

D3-12


Section B

Standard Form 1449 Continuation NNK10LB02B

NON-STANDARD SERVICE ITEM (Falcon 9 Blk 1 & 2) NOT TO EXCEED (NTE) PRICE ($) INCALENDAR YEAR ORDERED -

# from Item description 2010 (Jur 201 | 2012 2013 2014 2015 2016-2022

Exhibit 3 Dec)

15 Grade B Nitrogen (GN2) IAW MIL-PRF-27401F or TBP

conditioned air cooling supply far spot cooling of payfoad a ge Y¥ SS
components from payload mate or encapsulation up to T- | \ r wpe
0 dt.

16 ‘SIC Grade C Nitrogen (GN2) IAW MIL-PRP-27401F TBP
Purge System

11.7 Enhanced PLF and PLA Cleaning {AW IEST-STD- ££ —> TBP

CC1246D {evel 5004

11.8 Certified Portable Class 7 Clean Enclosure(s) for Open TBP
PLF Access Doors ! | l \ | i aa

42 Reserved
43 Co manifested Payload mission service | BY TBP
14 NASA Secondary Payload Mission Service TBP
1S Payload Compatibilly Assessment | Ter
6 ‘Secondary Payload Mission Feasibilfy Study Z BY Tee
7 ‘Secondary Payload accommodation study ] TEP
18 ‘Secondary Payload Mass simulator ~ i TAP
19 Payload Processing facilities

79.1 ~~ Contractor shall provide capability to provide ground TEP

processing facilities for payloads af the Eastem Range —————D

39.2] Contractor shall provide capability to provide ground —Ta |

processing facilities for payloads at the Westem Range

78:3 [Contractor shall provide capability fo provide ground nC

processing faclities for payloads at the Wallops Flight

Facllity

19.4 Contractor shall provide capability to provide ground
processing faciities for payloads at the Reagan Test Site

(USAKA- Kwajalein) :

20 ‘Additional Mission Analysis and Support

20.1 Reserved

a BY —



Section D
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

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.

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

(ii) Design restrictions, limitations, and known violations.

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

(iv) 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).

(v) Functional interfaces (e.g., structures, structural loads, and vibration).

(vi) Avionics systems and interfaces (e.g., payload avionics interfaces with

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

Statement of Work (F1/F1e) - 10


Section D

Attachment D3: Supplemental Data Requirements List NNK10LB02B
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.

D3-26


Section D . .
Attachment D1: Exhibit 1 (F1/F1e) tas - NNK10LB02B

Falcon 1/1e Acoustic Environment

During flight, the payload(s) will be subjected to a varying acoustic environment.
Levels are highest at lift off and during transonic flight due to aerodynamic excitation.
Falcon 1/1e will make use of acoustic blanketing to reduce the acoustic environment
and a nominal (minimal) 2” thick blanket configuration is assumed for all predicted
environments. Spectral energy methods were used to predict an acoustic Maximum

Predicted Environment (MPE) as shown in Table D1-Ka and D1-Kb below.

Exhibit 1 (F1/F1e) - 31


Section D

Attachment D1: Statement of Work (F1/F1e) ; NNK10LB02B

(E)

(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
teleased

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

(iii) Open ‘corrective actions/problems reports
(iv) Mission Unique and First flight items
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.

2.2.2 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). ‘ :

Statement of Work (F1/F1e) - 15


Section D '
. Attachment D1: Exhibit 1 (F9) : “ NNK10LB02B

BY

Redacted (Nn |
ibs ontirety |

Exhibit 1 (F9) - 23


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
CDRL DESCRIPTION Number: C3-2 (cont)

4. MISHAPS OCCURRING ON CONTRACTOR PROPERTY, THIRD PARTY
PROPERTY OR OTHER NON-NASA GOVERNMENT PROPERTY:

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

a. 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.

b. 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, shail 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.

c. 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.

D2-25


Section D .
Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B

3.4.1 Contract Orbit Requirements
3.4.1.1 Mission Orbit Specification
3.4.1.2 Reference Mission
3.4.2 Launch Window
3.4.3, SC Separation
3.4.4 Sun Angle Constraint
3.4.5 Thermal Roll
3.46 LV Telemetry Data
3.4.6.1_SC Separation State Vector
3.4.6.2 SC Provided Post Separation Data
3.5 Ground Operations
3.5.1 Spacecraft Contractor Supplied Ground Support Equipment
3.5.2 Payload Processing Facility
3.5.3 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
3.5.4 SC Transport

3.5.4.1 Processing Facility to Launch Complex Transport
3.5.4.2 SC Hoist and Mate Loads

3.5.5 Environmental Control System
3.5.5.1 PLF Environmental Controi System
3.5.6 Fluids And Gases Requirements
3.6 Safety Requirements

D2-15


Section D
‘Attachment D1; Exhibit + (F9) NNK10LB02B

1.0
2.0
3.0
4.0
5.0
6.0
7.0
8.0
9.0
10.0

TABLE OF CONTENTS

VEHICLE CONFIGURATION .........csccsessseessesseesssteseeeneanseeeeesnssessansnateaneassansenseneeee 6
PAYLOAD DELIVERY CAPABILITY .........scssssesssscsssesnsssssessnsesenseneecsnsnsasnensnenseee 7
INSERTION ACCURACIES
PAYLOAD SEPARATION ATTITUDE ACCURACY AND RATES. .
PAYLOAD FAIRING (PLE) ........sccsscssssessssssensaracsesesssnscenessnearsesnsanararasensseaeaenenene 26
MECHANICAL INTERFACE .
ELECTRICAL INTERFACE

PAYLOAD ENVIRONMENT... .
PAYLOAD ENVIRONMENT INSTRUMENTATION .........csssssssessqseessesseesecenseetees 50
GENERIC SECONDARY PAYLOAD CHARACTERISTICS/INTERFACE......... 50

Exhibit 1 (F9) - 2


Section B
Standard Form 1449 Continuation NNK101802B8

This Page Intentionally Left Blank

B-16.4 Modification 002


Section D :
Attachment D1: Exhibit 1 (F1/Fte) 7 NNK10LB02B"

BY

Red ached ia
ie onti coly

Exhibit 1 (F1/F te) - 36


* Section D

Attachment D1: Statement of Work (F1/F1e) ; NNK10LB02B

4.3

5.0

6.0

7.0

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.

GUIDELINE DOCUMENTS

The following documents are to be used as guidelines to the extent specified in this
SOW. If a 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.

Statement of Work (F1/F1e) - 31°


Section C

Contract Terms and Conditions NNK10LB02B

(B)

(C)

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(1),
“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

Mission success determination for the NASA secondary payload shail be
made in accordance with contract Section C, Clause 24.0, Mission Success

C46


Section D
Attachment D1: Exhibit 1 (F9) i NNK10LB02B

Reda hed ( /\
ct S ontivety

Exhibit 1 (F9) - 42


Section C

Contract Terms and Conditions NNK10LB02B

(b)

(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).

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:

[Contracting Officer shall check as appropriate]
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) §2.203-13, 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.

C-52


Section D
Attachment D1: Exhibit 1 (F9)

5

NNK10LB02B

SECTION D
ATTACHMENT D1
EXHIBIT 1

FALCON 9 Capabilities,
Specifications and Environments

Exhibit 1 (F9) - 1


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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.

D2-20


Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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
tequirements 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.

02-46


Section B
Standard Form 1449 Continuation. NNK10LB02B

This Page Intentionally Left Blank


Section D

Attachment D1: Exhibit 1 (F1/F1e) NNK10LB02B

Figure D1- 1:
Figure D1- 1b:

Figure D1- 2a:

Figure D1- 2b:

Figure D1-2c:
Figure D1-3:

Figure D1- 4:
Figure D1-M:

Figure D1- 5:

Figure D1-5A:
Figure D1-P1:

LIST OF FIGURES

Falcon 1 1.5m [5ft] Maximum Payload Static Envelopes...
Falcon 1e 1.7m [5.6ft] Maximum Payload Static Envelopes ..
Falcon 1/1e 38.81” Diameter LightBand Separation System coordinate
system (View looking aft). .
Falcon 1/1e Payload Adap| or interface showing

Falcon tite Payload Adapters and Interfaces
Falcon 1/1e Maximum Electromagnetic Radiation Levels Encountered
at Payload Interface (Does not include Range emitters)
Falcon 1/1e PLF Pressure Profiles and Depressurization Rates ........
Falcon 1/1e Maximum Predicted Payload Interface Shock Response

Spectrum Environment for various payload MasseS.............. eee 36
Falcon 1/1e Payload Maximum Steady State Axial Acceleration as a

function of Separated S/C MaSS. ..........cccccececseeeeeretetterteees
Falcon 1 Thermal environment as experienced during ascent..
Example of accelerometers and microphones on the Falcon 1 launch

VOICE... cece ce cscs cate cecsessactenseesessestsneessecseneieesistsesteaetseseretees 42

Exhibit 1 (F1/F te) - 4

ss


Section D . .
Attachment D1: Exhibit 1 (F9) NNK10LB028

BY

| Redact ed in |
its entirety

Exhibit 1 (F9) - 32


Section D

Attachment D3: Supplemental Data Reauirements List

NNK10LB02B

SDRL S1-1 Data
Request

BY
BY

(H) Power

D3-7



Section D.

Attachment D1: Statement of Work (F1/F1e) vo NNK10LB028

(C)

(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. Asa
minimum, the Contractor shall provide verification of the following items at
the MSCDR:

(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 shail 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

Statement of Work (F1/F1e) - 12


Section C

Contract Terms and Conditions _ NNK10LB02B

CONTRACT TERMS AND CONDITIONS

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

(a)

(b)

Inspection/Acceptance. Pursuant to FAR Subpart 12.402(b), FAR clause
§2.246-11 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 Governmentwide
commercial purchase card), the Contractor may not assign its rights to
receive payment under this contract.


Section C
Contract Terms and Conditions NNK10LB02B

18.2
19.0
19.1

19.2

19.3

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 [AW 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 shall 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 Settiement Under FAR
52.212-4(1), 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.

\f 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

C-30


Section D
Attachment D1: Statement of Work (F 1/Fle) NNK10LB02B

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

(i) Two payload access doors of sizes *_ B4 _\whose locations
shall be mission unique within the stated structural limitations of the
fairing. Additional or different size doors shail 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.

(ii), Thermal environments specified not to exceed _ BY :
By __ 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 which shall not exceed
BY

By Maximum thermal environments shall
be specified in the mission specific ICD (CDRL C2-1.1).

(iit), 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} ream | with an accuracy Ry
By : per second. :

(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).

(lt) A logo in accordance with NASA provided artwork. The size of the logo shall

be a maximum of * By! | dimensions.
The logo installation shall be appropriately documented in the mission
r Interface Control Document (ICD) (CDRL C2-1.1).

Statement of Work (F1/Fte) - 8


Section D a
Attachment D1: Exhibit 1 (F9) a NNK10LB02B

Bt

Reda cledl tn |
ds entirety

_ Exhibit 1 (F9) - 38


Section C
Contract Terms and Conditions NNK10LB02B

5.0

5.1

5.2

5.3

5.4

5.5

5.6

5.7

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
failing 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 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


Section D ‘
Attachment D1: Exhibit 1 (F1/F1e) : ‘is NNK10LB02B

Bu

Red acted (7 ;
ks en ceby

Exhibit 1 (F1/F1e) - 12


Section D
Attachment D3: Supplemental Data Requirements List NNK10LB02B

SDRL DESCRIPTION Number: S$3-3
AS BUILT CONFIGURATION LIST
DESCRIPTION/PURPOSE:

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

DATA REQUIREMENTS:

Bill of Materials identifying assemblies (as designed, as built, effectivity)

Part Fabrication Record — this includes the completed Work Order as well as the Work
Order status report. The completed Work Order is the record of accomplishment for
fabrication and test of the part/assembly including dates of accomplishment, quality
inspections, completion of configuration management review. The Work Order status
teport is the details — showing material and operations status, including the revision of
hardware issued for the work order and the desired revision.

Flight software and firmware: current versions and releases are identified.

Note — SpaceX maintains Bill of Materials/ Work Order status report information in
electronic format through its Visual Resource Planning and TeamCenter program
lifecycle management tools. Completed work orders are stored at SpaceX !n the online
“Quality Records’ filing system. Software and firmware, as well as vehicle build, are
stored in online at SpaceX. Special consideration will be made to provide electronic
(e.g. shared drive, etc) access to the ABCL information.

D3-17


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

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

(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 unproved
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.

(C) 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

Statement of Work (F9) - 12


Section C
Contract Terms and Conditions NNK10LB02B

SECTION C
CONTRACT TERMS AND CONDITIONS

TABLE OF CONTENTS
4.0 FAR 52.212-4 CONTRACT TERMS AND CONDITIONS--COMMERCIAL

ITEMS (MAR_2009) (TAILORED)............:.::s:s:sssssssssessssssssssessesssssersesssezes C-1
2.0 ON-RAMP AND TECHNOLOGY INSERTION ............:.2:s:ssssseressssessoesersees C-9
3.0 LAUNCH VEHICLE CERTIFICATION............:.sssssssssssssssssscosscssseresossesetss C-11

4.0 OFF-RAMP CLAUSE...

5.0 LAUNCH SERVICE PAYMENTS, MILESTONE EVENTS AND

COMPLETION CRITERIA ..........s:sssssssssssscssssssssssscarsssccssecesscscessssececesseass C-13
6.0 NFS 1852.232-77 LIMITATION OF FUNDS (FIXED-PRICE CONTRACT
(MAR 19839) . .C-16

7.0 SECURITY FOR LAUNCH SERVICE PAYMENT FINANCING............... C-18

8.0 SCOPE OF WORK — SPECIAL TASK ASSIGNMENTS (STUDIES AND
ANALYSES) (CLIN 10) .......::cssssssssssssssssssscsssssrsssesssesssssassasscssessssesessnesess C-20

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

10.0 _ RESERVED .........-scsssscsssssssosssssessesessssscessosssnesssossecossesesesssssessesessessesssesse C-22

11.0__ FAR 52.216-18 ORDERING (OCT 1995) [NOTE: APPLICABLE TO IDIQ
CONTRACT PORTION ONLY].

12.0__ FAR 52.216-19 ORDER LIMITATIONS (OCT 1995) [NOTE: APPLICABLE TO
IDIQ CONTRACT PORTION ONLY].........2.::s:sssscssessssssecesssesersesssepersssetes C-22

13.0 __ FAR 52.216-22 INDEFINITE QUANTITY (OCT 1995) [NOTE: APPLICABLE
. TO IDIQ CONTRACT PORTION ONLY}.

14.0__ LAUNCH SERVICE TASK ORDERING PROCEDURES [NOTE:
. APPLICABLE TO IDIQ CONTRACT PORTION ONLY].........:::::::::20000 C-24

15.0___ PRESERVATION, PACKING, PACKAGING, AND MARKING FOR
DOCUMENTATION...

16.0 __ FAR 52.246-11 HIGHER LEVEL CONTRACT QUALITY REQUIREMENT



Section D

Attachment D2: Contract Data Requirements List (CDRL) NNK10LB02B
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.

D2-10


Section C
Contract Terms and Conditions NNK40LB02B

26.1. The Contractor shail participate ina NASA-chaired Launch Readiness Review
(LRR) (reference 2.2.1.3(E) of the SOW). At the LRR, the Contractor shalt

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.

26.2 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.

26.3 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.

27.0 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 are included in the standard launch service price. Approvals required

by the payload are the responsibility of NASA.

28.0 ADVANCE UNDERSTANDING REGARDING TERMINATION SETTLEMENT
UNDER FAR 82.212-4(I)

28.1 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(!), Termination for the Government's
convenience, when the Contractor has refunded that portion of the milestone-

C42


Section D a
Attachment D1: Exhibit 1 (F9) NNK10LB02B

RY

Redacteel br
‘bs a wrety

Exhibit 1 (F9) - 17


Section D

Attachment D1: Statement of Work (F9) NNK10LB02B

(E)

(F)

(G)

(H

(1)

)

(K)

stage motor which shall not exceed | |
| ee BI
a “Maximum thermal environments shall be specified in
the mission specific 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.

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.

Capability to spin payloads, when applicable. orior to deployment over a
minimum range of zero (0)" BY with an accuracy Ry
“"Q4 per second.

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.

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).

A logo in accordance with NASA provided artwork. The size of the logo shall
be a maximum of ~ } BY | dimensions.
The logo installation shall be appropriately documented in the mission
Interface Control Document (ICD) (CDRL C2-1.1).

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 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, environmental testing with a TPA (personnel support is
limited to one installation and one removal of TPA), payload shock testing
with a TPA, and sufficient pyrotechnics for two shock test firings.

Command, control, and power signal capability from the launch control

facility to the payload umbilical Ground Support Equipment (GSE) IAW the
mission specific ICD.

Statement of Work (F9) - 9


Section D :
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

2.5

2.5.1

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.

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., |AW safety
requirements of the applicable launch processing site. 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), ete.) 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

Statement of Work (F1/F1e) - 27


Section D

NNK10LB02B

Attachment D1: Exhibit 3 (F1/Fie)

SECTION D
ATTACHMENT D1
EXHIBIT 3

FALCON 1 and FALCON te

Non-Standard Launch Services List-

Exhibit 3 (F1/F1e) - 1


Section D
Attachment D3: Supplemental Data Requirements List

NNK10LB02B

SDRL S1-1 Data ~ - —_
Request

(M) Communications
Capabilities

b

on

03-11



Section D
Attachment D1: Exhibit 4 NNK10LB02B

SAMPLE CERTIFICATE OF FLIGHT READINESS

FLIGHT CERTIFICATION DOCUMENT
FOR THE (TBD) MISSION

Note: The sample Certificate of Flight Readiness is modified from the suggested
format in the NLS-Il Request For Proposal. The signature block “(TBD) Space
Wing” has been amended to include “US Government Launch Authority”. US Air
Force Space Command 30" and 45" Space Wings do not have SpaceLift
Commander authority for launches from US Army Kwajalein Atoll.

Exhibit 4 - 3


Section D
Attachment D1: Statement of Work (F1/F1e) NNK10LB02B

2.6

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 read-only quality information to NASA (via remote
terminal) from such Quality Assurance on-line database systems as exist and to
which the Contractor has regular and timely input. An example is an on-line
Problem/Failure Reporting (P/FR) system.

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

Statement of Work (F1/F1e) - 29


Section D
Attachment D1: Exhibit 4 NNK10LB02B

SECTION D
ATTACHMENT D1
EXHIBIT 4
FALCON 1, FALCON ‘te, FALCON 9

Sample Certificate of Flight Readiness

Exhibit 4 - 1


Section D : Q :
Attachment D1: Exhibit 1 (FQ) - . NNK10LB02B

RY

R eda bed a ;
ts enh re ty

Exhibit 1 (F9)- 48


Section D

Attachment D2: Contract Data Requirements List (CDRL NNK10LB02B
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
pian 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.

D2-22


Section B
Standard Form 1449 Continuation - 2 NNK10L802B



Section D

of,

Attachment D1: Statement of Work (F1/Fte) . NNK10LB02B
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 shail 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/vehicie
processing, launch; and launch site maintenance and modifications. NASA
teserves 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 ail 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
teleases 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 faunch commentary for NASA Television.by furnishing faunch
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

Statement of Work (F1/Fte) - 6


Section C
Contract Terms and Conditions NNK10LB028

7.0
71

7.2

7.3

prices where applicable) of the items to be delivered, or in the time of
delivery, or both.

(f) 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.

(g) 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.

(h) 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.

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 shail be required in the form of a preferred creditor's
lien. The Contractor shall grant the Government a preferred creditor's lien ie., 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
tesponsible 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

C-18


Section D
Attachment D1: Exhibit 1 (F1/F1e) NNK10LB02B

1.0
2.0
3.0
4.0
5.0
6.0
7.0
8.0
9.0

10.0 GENERIC SECONDARY PAYLOAD CHARACTERISTICS/INTERFACE.

Table of Contents
VEHICLE CONFIGURATION ‘
PAYLOAD DELIVERY CAPABILITY...
INSERTION ACCURACIES
PAYLOAD SEPARATION ATTITUDE ACCURACY AND RATES ...sssssscsssssee 20
PAYLOAD FAIRING (PLF) ....
MECHANICAL INTERFACE .. .
ELECTRICAL INTERFACE..c.sscsscssssssssssssssssssssssesnsssseasresesessesasennevsensnenses 27
PAYLOAD ENVIRONMENT...

PAYLOAD ENVIRONMENT INSTRUMENTATION .

42

Exhibit 1 (F4/F1e) - 2


Section D
Attachment D1: Statement of Work (F9) NNK10LB02B

STATEMENT OF WORK

1.0 INTRODUCTION
1.1. 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 250 kg payload to orbit at an altitude of 200 km and a launch
inclination of 28.5°. This SOW pertains to SpaceX launch services utilizing both
the Falcon 9 Block 1 and Falcon 9 Block 2 launch vehicles.

This SOW defines the overail launch service requirements for ‘NASA or NASA-
sponsored payloads’ (hereinafter referred to as ‘payloads’). The Contractor shall
perform ail tasks necessary to safely and reliably launch payloads in accordance
with NASA-defined mission objectives. The Contractor shall support advance
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.

1.2 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.

Statement of Work (F9) - 4


Section D
Attachment D1: Exhibit 7 (F1/F1e) NNK10LB02B

Section D
ATTACHMENT D1
EXHIBIT 7

FALCON 1 and te
Certification Plan

li
\,

Exhibit 7 (F1/Fte) - 1


Section D
Attachment D1: Statement of Work (F1/F1e) . NNK10LB02B

‘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;
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

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:

20) 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

(B) 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

Statement of Work (F1/F1e) - 13


Section C
Contract Terms and Conditions NNK10LB02B

9.3

9.4

(iv)

Due date for Contractor's Task Plan

(B) The Contractor's Task Plan shail include:

(i) Discussion of the technical approach for performing the work and
rationale for any proposed changes to the Statement of Work and
tequired completion date.

(ii) Required authorization to proceed date.

(iii) 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.

(C) The Contracting Officer shail 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.

(D) 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

(E) The Special Task Assignments may be revised in the same manner as they
are executed via formal revisions.

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.

C-21