80KSC020R0003 - CAPSTONE - Draft RFP.pdf

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SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS

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

1. REQUISITION NUMBER PAGE 1 OF

2. CONTRACT NO. 3. AWARD/EFFECTIVE

DATE

4. ORDER NUMBER 5. SOLICITATION NUMBER 6. SOLICITATION ISSUE

DATE

7. FOR SOLICITATION

INFORMATION CALL:

a. NAME b. TELEPHONE NUMBER (No collect calls)

8. OFFER DUE DATE/

LOCAL TIME

9. ISSUED BY

13b. RATING

14. METHOD OF SOLICITATION

CODE

15. DELIVER TO 16. ADMINISTERED BY CODE

18a. PAYMENT WILL BE MADE BY CODE17a. CONTRACTOR/

OFFEROR

FACILITY

TELEPHONE NO.

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

OFFER

18b. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a UNLESS BLOCK

BELOW IS CHECKED

RFQ IFB RFP

SEE ADDENDUM

19.

ITEM NO.

20.

SCHEDULE OF SUPPLIES/SERVICES

21.

QUANTITY

22.

UNIT

23.

UNIT PRICE

24.

AMOUNT

(Use Reverse and/or Attach Additional Sheets as Necessary)

25. ACCOUNTING AND APPROPRIATION DATA 26. TOTAL AWARD AMOUNT (For Govt. Use Only)

28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN

COPIES TO ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND

DELIVER ALL ITEMS SET FORTH OR OTHERWISE IDENTIFIED ABOVE AND ON ANY

ADDITIONAL SHEETS SUBJECT TO THE TERMS AND CONDITIONS SPECIFIED

29. AWARD OF CONTRACT: REF. OFFER

DATED . . YOUR OFFER ON SOLICITATION

(BLOCK 5), INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE

SET FORTH HEREIN, IS ACCEPTED AS TO ITEMS:

30a. SIGNATURE OF OFFEROR/CONTRACTOR

30b. NAME AND TITLE OF SIGNER (Type or print) 30c. DATE SIGNED

31a. UNITED STATES OF AMERICA (SIGNATURE OF CONTRACTING OFFICER)

31b. NAME OF CONTRACTING OFFICER (Type or print) 31c. DATE SIGNED

AUTHORIZED FOR LOCAL REPRODUCTION

PREVIOUS EDITION IS NOT USABLE

STANDARD FORM 1449 (REV. 2/2012)

Prescribed by GSA - FAR (48 CFR) 53.212

10. THIS ACQUISITION IS UNRESTRICTED OR

NAICS:

SIZE STANDARD:

13a. THIS CONTRACT IS A

RATED ORDER UNDER

DPAS (15 CFR 700)

SET ASIDE: % FOR:

11. DELIVERY FOR FOB DESTINA-

TION UNLESS BLOCK IS

MARKED

SEE SCHEDULE

12. DISCOUNT TERMS

ARE ARE NOT ATTACHED

ARE ARE NOT ATTACHED

27a. SOLICITATION INCORPORATES BY REFERENCE FAR 52.212-1, 52.212-4. FAR 52.212-3 AND 52.212-5 ARE ATTACHED. ADDENDA

27b. CONTRACT/PURCHASE ORDER INCORPORATES BY REFERENCE FAR 52.212-4. FAR 52.212-5 IS ATTACHED. ADDENDA

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41a. I CERTIFY THIS ACCOUNT IS CORRECT AND PROPER FOR PAYMENT

32b. SIGNATURE OF AUTHORIZED GOVERNMENT

REPRESENTATIVE

32c. DATE

41b. SIGNATURE AND TITLE OF CERTIFYING OFFICER 41c. DATE

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40. PAID BY

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REPRESENTATIVE

32e. MAILING ADDRESS OF AUTHORIZED GOVERNMENT REPRESENTATIVE 32f. TELPHONE NUMBER OF AUTHORZED GOVERNMENT REPRESENTATIVE

32g. E-MAIL OF AUTHORIZED GOVERNMENT REPRESENTATIVE

33. SHIP NUMBER 34. VOUCHER NUMBER 35. AMOUNT VERIFIED

CORRECT FOR

PARTIAL FINAL

37. CHECK NUMBER

38. S/R ACCOUNT NO. 39. S/R VOUCHER NUMBER

36. PAYMENT

COMPLETE PARTIAL FINAL

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

1. REQUISITION NUMBER

PAGE 1 OF

2. CONTRACT NO.

3. AWARD/EFFECTIVE

DATE

4. ORDER NUMBER

5. SOLICITATION NUMBER

6. SOLICITATION ISSUE

DATE

7. FOR SOLICITATION

INFORMATION CALL:

a. NAME

b. TELEPHONE NUMBER (No collect calls)

8. OFFER DUE DATE/

LOCAL TIME

9. ISSUED BY

13b. RATING

14. METHOD OF SOLICITATION

CODE

15. DELIVER TO

16. ADMINISTERED BY

CODE

18a. PAYMENT WILL BE MADE BY

CODE

17a. CONTRACTOR/

OFFEROR

CODE

FACILITY

CODE

CODE

TELEPHONE NO.

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

OFFER

18b. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a UNLESS BLOCK

BELOW IS CHECKED

RFQ

IFB

RFP

SEE ADDENDUM

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ITEM NO.

20.

SCHEDULE OF SUPPLIES/SERVICES

21.

QUANTITY

22.

UNIT

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UNIT PRICE

24.

AMOUNT

(Use Reverse and/or Attach Additional Sheets as Necessary)

25. ACCOUNTING AND APPROPRIATION DATA

26. TOTAL AWARD AMOUNT (For Govt. Use Only)

28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN

COPIES TO ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND

DELIVER ALL ITEMS SET FORTH OR OTHERWISE IDENTIFIED ABOVE AND ON ANY

ADDITIONAL SHEETS SUBJECT TO THE TERMS AND CONDITIONS SPECIFIED

29. AWARD OF CONTRACT: REF. OFFER

DATED . . YOUR OFFER ON SOLICITATION

(BLOCK 5), INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE

SET FORTH HEREIN, IS ACCEPTED AS TO ITEMS:

30a. SIGNATURE OF OFFEROR/CONTRACTOR

30b. NAME AND TITLE OF SIGNER (Type or print)

30c. DATE SIGNED

31a. UNITED STATES OF AMERICA (SIGNATURE OF CONTRACTING OFFICER)

31b. NAME OF CONTRACTING OFFICER (Type or print)

31c. DATE SIGNED

AUTHORIZED FOR LOCAL REPRODUCTION

PREVIOUS EDITION IS NOT USABLE

STANDARD FORM 1449 (REV. 2/2012)

Prescribed by GSA - FAR (48 CFR) 53.212

10. THIS ACQUISITION IS

UNRESTRICTED OR

NAICS:

SIZE STANDARD:

13a. THIS CONTRACT IS A

RATED ORDER UNDER

DPAS (15 CFR 700)

SET ASIDE:

% FOR:

11. DELIVERY FOR FOB DESTINA-

TION UNLESS BLOCK IS

MARKED

SEE SCHEDULE

12. DISCOUNT TERMS

ARE

ARE NOT ATTACHED

ARE

ARE NOT ATTACHED

27a. SOLICITATION INCORPORATES BY REFERENCE FAR 52.212-1, 52.212-4. FAR 52.212-3 AND 52.212-5 ARE ATTACHED. ADDENDA

27b. CONTRACT/PURCHASE ORDER INCORPORATES BY REFERENCE FAR 52.212-4. FAR 52.212-5 IS ATTACHED. ADDENDA

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8 (A)

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SMALL BUSINESS

WOMEN-OWNED SMALL BUSINESS

(WOSB) ELIGIBLE UNDER THE WOMEN-OWNED

SMALL BUSINESS PROGRAM

SMALL BUSINESS

SERVICE-DISABLED

VETERAN-OWNED

SMALL BUSINESS

HUBZONE SMALL

BUSINESS

SMALL BUSINESS

SMALL BUSINESS

STANDARD FORM 1449 (REV. 2/2012)

BACK

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32a. QUANTITY IN COLUMN 21 HAS BEEN

RECEIVED

INSPECTED

ACCEPTED, AND CONFORMS TO THE CONTRACT, EXCEPT AS NOTED:

41a. I CERTIFY THIS ACCOUNT IS CORRECT AND PROPER FOR PAYMENT

32b. SIGNATURE OF AUTHORIZED GOVERNMENT

REPRESENTATIVE

32c. DATE

41b. SIGNATURE AND TITLE OF CERTIFYING OFFICER

41c. DATE

42a. RECEIVED BY (Print)

42b. RECEIVED AT (Location)

42c. DATE REC'D (YY/MM/DD)

42d. TOTAL CONTAINERS

40. PAID BY

32d. PRINTED NAME AND TITLE OF AUTHORIZED GOVERNMENT

REPRESENTATIVE

32e. MAILING ADDRESS OF AUTHORIZED GOVERNMENT REPRESENTATIVE

32f. TELPHONE NUMBER OF AUTHORZED GOVERNMENT REPRESENTATIVE

32g. E-MAIL OF AUTHORIZED GOVERNMENT REPRESENTATIVE

33. SHIP NUMBER

34. VOUCHER NUMBER

35. AMOUNT VERIFIED

CORRECT FOR

PARTIAL

FINAL

37. CHECK NUMBER

38. S/R ACCOUNT NO.

39. S/R VOUCHER NUMBER

36. PAYMENT

COMPLETE

PARTIAL

FINAL

1. REQUISITION NUMBER: TBD

PAGE 1 OF:

2. CONTRACT NUMBER: TBD

4. ORDER NUMBER:

5. SOLICITATION NUMBER: 80KSC020R0003

7. FOR SOLICITATION INFORMATION CALL: a. NAME:

7. FOR SOLICITATION INFORMATION CALL: b. TELEPHONE NUMBER (No collect calls):

9. ISSUED BY CODE:

% For :

12. DISCOUNT TERMS:

13b. RATING:

15. DELIVER TO:

16. ADMINISTERED BY CODE:

16. ADMINISTERED BY:

17a. CONTRACTOR/ OFFEROR CODE:

17a. CONTRACTOR/ OFFEROR:

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

18a. PAYMENT WILL BE MADE BY:

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20. SCHEDULE OF SUPPLIES/ SERVICES: Integration & Launch of CAPSTONE

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28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN COPIES TO ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND DELIVER ALL ITEMS SET FORTH OR OTHERWISE IDENTIFIED ABOVE AND ON ANY

ADDITIONAL SHEETS SUBJECT TO THE TERMS AND CONDITIONS SPECIFIED. INITIALS :

29. AWARD OF CONTRACT: REFERENCE OFFER:

DATE. YOUR OFFER ON SOLICITATION

(BLOCK 5), INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE

SET FORTH HEREIN, IS ACCEPTED AS TO ITEMS.:

30b. NAME OF SIGNER (Type or print):

30b. TITLE OF SIGNER (Type or print):

31b. NAME OF CONTRACTING OFFICER (Type or print):

10. THIS ACQUISITION IS UNRESTRICTED: 1

10. THIS ACQUISITION IS SET ASIDE:: 0

11. DELIVERY FOR FOB DESTINATION UNLESS BLOCK IS MARKED SEE SCHEDULE: 0

13a. THIS CONTRACT IS A RATED ORDER UNDER DPAS (15 CFR 700): 0

14. METHOD OF SOLICITATION RFQ: 0

10. THIS ACQUISITION IS NAICS::

10. THIS ACQUISITION IS SIZE STANDARD::

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32B SIGNATURE OF AUTHORIZED GOVERNMENT REPRESENTATIVE. THIS IS A PRTECTED FIELD.:

18b. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a UNLESS BLOCK IS CHECKED SEE ADDENDUM: 0

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

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DRAFT REQUEST FOR PROPOSAL

for

CAPSTONE

CAPSTONE ATTACHMENT A – Statement of Work 80KSC020R0003

Draft Statement of Work

1.0 Scope and Requirements

1.1 Scope

The NASA Launch Services Program (LSP) is seeking a launch service for the CAPSTONE mission, a 12U-Class satellite, to a Trans Lunar Injection orbit. This contract will consist of a single launch. The launch shall occur at a Contractor-specified launch date, which shall be between December 1, 2020 and March 31, 2021. This Statement of Work (SOW) defines the Contractor requirements to provide NASA a launch service for the CAPSTONE mission.

The Contractor shall provide a launch vehicle system for the CAPSTONE mission that shall be capable of delivering a total nominal payload mass of 25 kg plus the payload provided dispenser to a C3 of -0.6 km2/s2. The maximum mass of the payload and dispenser shall not exceed 37 kg. The Contractor shall determine and account for the dispenser mounting, required trajectory, and mass reserves such that the launch vehicle will be able to accommodate CAPSTONE.

The Contractor shall perform launch vehicle planning, analysis, design, development, production, integration, and testing required to provide the launch service appropriate to transport the payload to the desired orbit.

2.0 Planning

The Contractor shall furnish all services to meet CAPSTONE requirements 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 CAPSTONE to the required orbit conditions within required launch period.

The Contractor shall be responsible for initiating and ultimately obtaining the necessary approval/licensing (i.e., Federal Aviation Administration) to successfully deliver the procured launch service. The Contractor shall be responsible for all integration and Range services in order to successfully deliver the launch service. 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 if required.

The Contractor shall include all Contract Data Requirements List (CDRL) items as part of the launch service.

The Contractor shall provide logistical supplies, services, and hardware support to the post-production, transportation, and launch base operations of the vehicle system. The Contractor shall provide all necessary services and mission specific elements, including vehicle test and flight hardware and software, required to integrate the payload to the launch vehicle system. Such support should include, but is not limited to, provision of spares; provision of propellants, liquids, and gases for launch and test; packaging and transportation of the vehicle system; and warehousing and storage.

Limited Government program management will be required in order to assess completion of the defined Attachment C, Milestone Deliverable Descriptions and Requirements, which shall be satisfied in order to progress towards the targeted launch date. NASA's seeks to enable the use of commercially accepted practices while still understanding the schedule risks of the launch service used for the mission.

2.1 Program Management

The Contractor shall perform the program management tasks required to provide the launch service and satisfy the mission requirements. These tasks shall include as a minimum:

A. Conduct launch vehicle program reviews that provide evidence of launch vehicle maturity towards the contracted launch date and to provide the Government with appropriate evidence needed to satisfy milestone payments to the Contractor (as defined in Attachment C).

B. Develop and maintain a master schedule and sub-tier schedules.

C. Obtain all applicable licenses, permits, and approvals required by federal, state, and local regulatory agencies; and prepare (or support the Government in preparing, if necessary, for the payload) and submit any environmental impact statements that may be necessary for the provisioning of the launch service. Approvals required by the payload will be the responsibility of the Government. The Contractor and the Government shall provide reasonable cooperation and support to each other in the process of obtaining, maintaining, and renewing permits and licenses as set forth above.

D. Provide resolution of critical problem areas to minimize or eliminate schedule impacts.

E. Manage all subcontracts and monitor subcontractor activities to a sufficient level of detail to ensure timely delivery of acceptable components. A report on the performance of subcontractors shall be included as part of any program reviews.

F. Provide the recommended payload success criteria prior to the launch, the post-launch supporting data, and the Final Flight Report (CDRL CAPSTONE-6) to enable determination of payload success as defined in the Interface Control Document (ICD) (CDRL CAPSTONE- 2). The Government shall determine whether the mission is a success or failure based on the application of the payload success criteria as defined in the ICD (CDRL CAPSTONE-2).

G. Make provision for insurance to cover liability for possible damage to Government property and third parties in accordance with necessary approval/licensing (i.e., Federal Aviation Administration).

H. Pay any taxes and transfer costs required for delivery of the launch service.

2.2 Compliance Documents

The Contractor shall comply with the following documents:

A. Applicable Range Safety Documentation for the selected launch site as determined by the

FAA.

B. NPR 8715.6, NASA Procedural Requirement for Limiting Orbital Debris (in order to assist the Government for payload compliance).

C. NPR 8621.1, NASA Procedural Requirements for Mishap and Close Call Reporting, Investigating, and Recordkeeping (only in order to assist the Government in the event of a mishap involving NASA personnel or property).

D. Certification Regarding United States Commercial Provider of Space Transportation

Services (Public Law 105-303, Title II, Section 201)

3.0 Launch Vehicle Analysis, Design

The Contractor shall provide the design of the launch vehicle, including but not limited to the following subsystems: structures, mechanisms, fluids/propulsion, electrical/electronics, guidance/navigation/control, flight termination, and software.

The Contractor shall meet the following requirements for the launch service:

A. Environments:

a. During launch, the payload vibration and shock environment shall be at or below the NASA Goddard General Environmental Verification Standard (GEVS).

b. The LV Free Molecular Heating (FMH) rate shall be a maximum of 1135 Watts per square meter (W/m2), three sigma, from payload fairing jettison through RSV separation.

c. There are currently no spacecraft derived environmental requirements regarding contamination, purges, pressure decay rate, structural loads, acoustics, or electro-magnetic compatibility.

d. All environments are defined at the interface between the LV and the payload dispenser.

e. The Contractor shall include sufficient flight instrumentation to establish that the vehicle launch environments meet the requirements of the ICD (CDRL CAPSTONE-3).

B. The trajectory requirements provided in Attachment A.1.

C. The mechanical interface between the payload dispenser and the LV, as referenced in Attachment

A.2. The Contractor shall supply any fasteners required to mount the dispenser to LV interface.

D. The electrical interface between the payload dispenser and the LV, as referenced in Attachment A.2.

The payload dispenser has thermostatically controlled heaters that must be powered by the LV during flight, prior to separation.

Analysis required to validate the launch vehicle design shall be documented to the launch vehicle Contractor’s standards.

4.0 Development and Production

The Contractor shall implement a test program for development and qualification of any new systems required for the launch vehicle and shall include existing systems that are modified, launch vehicle components not yet qualified, and ground support equipment. Qualification shall be to the Contractor’s standards. Risks, as defined by the Contractor's risk plan, shall be reported to the Government.

The Contractor shall manufacture, assemble, test and transport the launch vehicle and all mission hardware required to provide the launch service and shall provide all materials and equipment necessary for these tasks.

5.0 Mission Integration

The Contractor shall provide the necessary services and hardware to integrate the payload and dispenser to the launch vehicle. The Contractor shall coordinate with the Government to develop the ICD (CDRL

CAPSTONE-2) during integration. The ICD (CDRL CAPSTONE-2) assures the launch vehicle system is ready to accept satellite integration at the launch site, as well as on-orbit deployment upon completion of the launch service.

The Contractor shall conduct periodic mission integration coordination teleconferences with the Government on at least a bi-weekly basis from award through launch.

6.0 Launch Operations

The Contractor shall identify and secure a launch site to meet the requirements of the launch service.

6.1 Checkout and Launch

The Contractor shall perform the following:

A. Assemble, transport, maintain, checkout, and launch a vehicle that delivers the satellites into the desired orbit.

B. Provide and make arrangements for all facilities, supplies, and services required for preparation and launch of the vehicle.

C. Identify launch vehicle ground and flight safety launch constraints. The Government will be responsible for providing all satellite checkout procedures and for obtaining the requisite satellite safety approvals (with the assistance of the Contractor). If necessary, integrate the satellite procedures with the launch vehicle checkout effort where appropriate and coordinate launch site and safety approvals.

D. Integrate the CAPSTONE payload/dispenser assembly onto the launch vehicle, encapsulate, transport, and perform spacecraft to launch vehicle integrated checkout activities necessary to assure launch readiness.

E. Provide and schedule the necessary support services at the launch Range that are required for launch preparation of the launch vehicle, integrated testing with the payload, and launch.

6.2 Launch Support

The Contractor shall provide access for up to three Government personnel at the launch site for familiarization and communication of launch status. The Contractor shall also provide access for Government payload personnel at the launch site for integrated activities and communication of launch status. Support should be consistent with the Contractor’s commercial practices for integrated spacecraft to launch vehicle operations and on day of launch using commercial practices with available information, which may include access to real-time telemetry (RF and hardwire), voice communication channels with listen capabilities, video and telephones. As determined by the ICD (CDRL CAPSTONE-2), a notification of the achieved orbit characteristics shall be provided to the Government as soon as possible.

The Contractor shall poll the Government during the launch terminal countdown for the payload status.

The launch shall not occur unless the Government states the payload is ready.

7.0 Payload Processing Support

The Contractor shall provide notification at the Launch Vehicle Readiness Review (LVRR) (reference Attachment C, Milestone Deliverable Descriptions and Requirements) to coordinate the payload delivery to the launch site.

The Contractor shall provide a certified ISO 8 cleanliness level (Class 100K) cleanroom and any other necessary facility resources required to support Government performed pre-flight servicing of the spacecraft propellant tanks with hydrogen peroxide, integration of the spacecraft into its dispenser, and flight closeouts of the spacecraft/dispenser assembly. The CAPSTONE team will provide safety approved spacecraft propellant servicing Ground Support Equipment and the propellant and conduct all activities associated with processing of the satellite prior to integration with the launch vehicle and for all operational activities related to the satellite immediately following its separation from the launch vehicle on-orbit.

8.0 Safety and Quality

The Contractor shall establish, implement, and maintain risk management, safety, reliability, and quality assurance programs with AS9100, Aerospace Quality Management System, or equivalent as a guideline.

9.0 Contract Documentation Requirements List (CDRL)

The CDRL identifies critical elements of the Contractor’s efforts.

The Contractor shall produce and make the appropriate distribution of all items on the CDRL that require review or approval by the Government. The CDRL list is included in Attachment B (Contract Data Requirements List).

CAPSTONE ATTACHMENT A.1 TRAJECTORY REQUIREMENTS 80KSC020R0003

Launch Opportunities The launch vehicle (LV) shall support a launch attempt on any day of the year.

Reference Mass The reference mass of the spacecraft (SC) is 37 kg. This consists of the 25 kg separating SC, a

9.3 kg dispenser, and 8% margin.

Reference Mission Target Orbit Requirements The LV shall place the spacecraft into an orbit at the Target Interface Point (TIP) with the parameters shown in Table 1.

Table 1: Injection Target Orbit Parameters at TIP

Parameter Value 3-Sigma Dispersion

TIP Time(1) Daily Varying (UTC Time) N/A

Characteristic Energy (C3)(1) <= -0.6 km2/s2 ± 0.1 km2/s2

Argument of Perigee(1) Daily Varying (-20/+20 deg or 160/200 deg)

± 1.0 deg

Right Ascension of the Ascending Node (RAAN) (1)

Daily Varying (0/360 deg)

± 1.0 deg

Inclination >8 deg ± 1.0 deg

Notes:

(1) The targets and TIP time will vary depending on the result of the LV solution. The values and ranges provided reflect a 160 km x 1,330,000 km injection orbit at an inclination of 30 deg.

(2) These targets and dispersion values are preliminary. The final analyses and interfaces shall be developed with the LV.

(3) The LV target orbit parameters shall be defined using the constants defined by the World Geodetic System 1984 (WGS-84).

Mission Thermal Requirements The SC has no thermal requirements that impact the LV mission design nor are there any Sun angle constraints imposed on the LV by the SC mission design.

CAPSTONE ATTACHMENT A.1 TRAJECTORY REQUIREMENTS 80KSC020R0003

Separation Attitude The SC has no requirement on the orientation of the LV for separation of the SC.

Tipoff Rates At loss of contact between the LV and the SC, the total SC body rate shall not exceed 10 deg/sec.

Note: Total SC body rate is defined as the RSS of the Xsc, Ysc, and Zsc body rates.

Mission Duration The SC has no requirement on the LV mission duration.

Post SC Separation Following SC separation, the LV hardware shall not recontact the spacecraft.

Tyvak Proprietary Information CAPSTONE – Attachment A – 80KSC020R0003

CAPSTONE Spacecraft Envelope/Mass Properties, Mechanical Interface Requirements, and Electrical Interface Requirements

Tyvak Proprietary Information CAPSTONE – Attachment A – 80KSC020R0003

• The payload dispenser has thermostatically controlled 20W heaters that must be powered by the LV during flight, prior to separation.

• Spacecraft will terminate the LV end of the dispenser harness with LV defined connector

• LV to define length of the dispenser harness

• LV to provide prime and redundant separation commands

• Separation signal characteristics can be found in the Tyvak 12U dispenser Users Guide

Electrical Interface Requirements

CAPSTONE ATTACHMENT B – Contract Data Requirements List 80KSC020R0003

ATTACHMENT B

CONTRACT DATA REQUIREMENTS LIST

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CDRL DESCRIPTION Number: CAPSTONE-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 for the review for NASA attendees due 3 days prior to the Review. The presentation package for the QDR is due 1 week prior to the QDR or the QDR will be rescheduled.

i. Reviews as documented in Attachment C, Milestones.

B. Minutes from each formal review

C. List of attendees

D. 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 with key points/details and timeline identified/planned, closed, or deleted)

vi. Closure rationale

CDRL DESCRIPTION Number: CAPSTONE-2

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, as well as the mission success criteria.

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 as appropriate to meet payload requirements. The outline below is meant to assure all potential requirements are addressed regardless of payload complexity or risk posture; however any deemed unnecessary requirements based upon manifested payload requirements (upon mutual Government/Contractor agreement) may be listed as not applicable (NA) in the approved ICD:

1.0 INTRODUCTION

1.1 Purpose

1.2 Scope

1.3 Definitions

1.4 Interface Change Control

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

3.2 Electrical Interfaces

CDRL DESCRIPTION Number: Continuation of CAPSTONE-2

3.3 Environmental Interfaces

3.4 Flight Design

3.5 Ground Operations

3.6 Safety Requirements

4.0 MISSION SUCCESS CRITERIA

The Contractor’s proposed criteria to be used to determine the success of the mission. These criteria shall be based on applicable flight related ICD requirements.

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.

CDRL DESCRIPTION Number: CAPSTONE-3

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 Contractor engineer. NASA does not intend to conduct its own verification of the interface requirements.

DATA REQUIREMENTS:

The verification matrix shall be released no later than CDR 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

CDRL DESCRIPTION Number: CAPSTONE-4

PERFORMANCE AND GUIDANCE ACCURACY ANALYSIS (PGAA)

DESCRIPTION/PURPOSE:

This analysis is prepared using the provider-defined trajectory requirements to help provide confidence in meeting the CAPSTONE requirement.

DATA REQUIREMENTS:

The analysis shall include, as a minimum:

A. The nominal and 3-sigma limits for orbit elements and associated covariance matrix.

B. Performance impacts as a function of launch date and time.

C. Performance capability, margins and reserves, including description of how performance reserve is calculated.

D. Sequence of events and tracking coverage.

E. Time history of trajectory from launch to targeted condition and end of mission maneuvers.

F. Launch vehicle summary weight statement.

G. Sources and magnitude for all dispersions used. If statistical dispersions are used, then the distribution method (e.g., normal, gaussian) shall be specified for each parameter.

H. Definition of all coordinate systems used.

I. Reference to the source(s) for all payload and launch vehicle inputs to this analysis (e.g., requirements, mass properties).

J. Evaluation of compliance with applicable ICD requirements and constraints.

K. Launch windows determined by analysis.

L. Input file.

M. An itemized list of all modeling changes made since the previous CDRL C4-1 release

(including launch vehicle propulsion, mass properties, aerodynamics, and mission design ground rules), along with an assessment of the performance effect of each change.

CDRL DESCRIPTION Number: CAPSTONE-5

COUPLED DYNAMIC LOADS ANALYSIS

DESCRIPTION/PURPOSE:

This analysis defines flight loads to 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 shall be identified and included in the analysis.

C. Output from each flight event shall include maximum/minimum tables of interface accelerations and interface loads as well as interface shock response spectra.

D. One load cycle will be required per mission.

CDRL DESCRIPTION Number: CAPSTONE-6

FINAL FLIGHT REPORT

DESCRIPTION/PURPOSE:

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

DATA REQUIREMENTS:

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

This report shall also include:

i. Orbit elements determined from vehicle guidance data.

ii. Vehicle data indicating payload separation.

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

iv. Post flight determination of actual flight environments.

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

vi. Vehicle sequence and attitudes data.

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 CAPSTONE-3.

CDRL DESCRIPTION Number: CAPSTONE-7

SPACECRAFT 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:

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. Fairing installation.

ATTACHMENT C

MILESTONE DELIVERABLE DESCRIPTIONS AND REQUIREMENTS

CAPSTONE ATTACHMENT C – Milestone Deliverable Descriptions And Requirements 80KSC020R0003

Milestone /Payment

Payment Name

Typical Payment Months

Before/After Milestone*

Invoice

Submission Dates

Amount (% of Launch

Service CLIN Price)

1 Kick-off No Earlier Than Award TBP 5%

Preliminary ICD submittal *L-8 months TBP 10%

Mission Critical Design Review

Core Stage Engine(s) Qualification Testing

Complete*

Contractor Signed Baseline ICD and

Verification Matrix

*L-6 months TBP 20%

Core Stage(s) Propulsion

*L- 4 months

TBP 20%

Qualification Data or

Post Flight Data

L-2 months

TBP 20%

TLI stage Propulsion

LVRR

FRR

Launch

L - 0 TBP 15%

7 Post-Launch L + 1 months TBP 10%

*This represents a generic scenario with 10 months from ATP to the CAPSTONE launch, and a launch vehicle that requires a Contractor proposed engine and a stage qualification being completed after award. Longer periods of performance should consider the earliest dates possible for the ICD and CDR. Offeror's should propose an update, including earlier L minus dates for the ICD and CDR dates, if the period of performance is greater than 10 months. The Offeror should propose a launch vehicle manufacturing (i.e. engines, stages, and avionics) or flight propulsion acceptance test milestone if any of the listed propulsion milestones have been completed.

NOTE: Alternate payment schedules may be proposed.

Milestone Deliverable Descriptions and Requirements

Kick-Off Meeting

A. Vehicle Overview B. Proposed Schedule C. Risks to implementation of SOW (Cost, Schedule, Technical)

Interface Control Drawing (ICD)

Delivery of an ICD per CDRL CAPSTONE-2

ICD Verification Matrix

Delivery of an ICD Verification Matrix per CDRL CAPSTONE-3

Engine and Stage Propulsion Testing

Core stage engines are defined as propulsive engines on stages required for the launch vehicle to achieve low earth orbit. Engines needed for an added Trans Lunar Injection (TLI) stage are not considered core stage engines. Qualification Tests are not required to be on the actual engines or stages to be used on the CAPSTONE launch vehicle.

Core Stage Engine(s) Qualification Testing Completed

The Contractor shall have completed all core stage engine qualification tests consistent with the planned qualification tests specifically identified as proposed by the offeror in Section L.12, Volume I, Technical/Management Capability, [L.12.(x).d)]. The test shall demonstrate that the Contractor has high confidence in the ability to successfully deliver the launch service on schedule. Deviations, anomalies during qualification testing and a list describing all configuration changes under consideration prior to the CAPSTONE mission shall be documented in the Contractor's risk system and/or technical decision-making system with only a summary provided to the Government. NASA reserves the right to withhold approval based on the Contractor not having a credible plan to resolve risks and/or implement planned changes in time for the CAPSTONE mission.

The mission profile demonstrated in this test shall become an input for the Performance and Guidance Accuracy Analysis (PGAA) CDRL CAPSTONE-4.

Core Stages Propulsion Qualification Testing Complete

The Contractor shall have completed propulsion testing of all core stages in a flight like configuration demonstrating the stage(s) successfully achieved Contractor proposed propulsion test objectives. The tests will demonstrate high confidence in the ability to successfully deliver the launch service on schedule. Deviations, anomalies during qualification testing, and a list describing all configuration changes under consideration prior to the CAPSTONE mission shall be documented in the Contractor's risk system and/or technical decision-making system with only a summary provided to the Government. NASA reserves the right to withhold approval based on the Contractor not having a credible plan to resolve risks and/or implement planned changes in time for the CAPSTONE mission.

TLI stage Propulsion Qualification Testing Complete

The Contractor shall have completed propulsion testing of the TLI stage (if applicable) in a flight like configuration demonstrating the stage successfully achieved Contractor proposed propulsion test objectives. The tests will demonstrate high confidence in the ability to successfully deliver the launch service on schedule. Deviations, anomalies during qualification testing, and a list describing all configuration changes under consideration prior to the CAPSTONE mission shall be documented in the Contractor's risk system and/or technical decision-making system with only a summary provided to the Government. NASA reserves the right to withhold approval based on the Contractor not having a credible plan to resolve risks and/or implement planned changes in time for the CAPSTONE mission.

Reviews

The Contractor shall conduct and chair reviews, as described below, that apply to the system, subsystem, component, and software level items of the launch service (payload interface, and any supporting equipment). Where there is not a direct match between a SOW specified 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.

Mission Critical Design Review (CDR)

The Contractor shall conduct a Mission CDR before significant fabrication of mission interface hardware begins. The Contractor shall present a final detailed design based on drawings, analyses, and evaluation testing that shows the mission design meets final performance and interface specifications, safety requirements, and mission objectives. The Contractor shall identify and describe all planned mission qualification and acceptance tests to be performed to prove validity. NASA reserves the right to withhold approval of this milestone if the design does not meet performance or schedule requirements and until all action items have been closed. As a minimum, the Contractor shall provide verification of the following items at the CDR:

i. All known technical design problems and development anomalies associated with meeting the ICD requirements have been resolved without compromising required system function, performance and safety. If not resolved a credible and detailed resolution plan exists to resolve them prior to qualification testing or final analysis cycle as appropriate.

ii. The detailed mission hardware and analytical design will meet performance, functional requirements, and schedule.

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

iv. All key engineering analyses have been performed to support the detailed design.

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

vi. Launch vehicle/payload compatibility test plans, if any, have been defined.

vii. The baseline ICD and Verification Matrix has been signed by the Contractor and submitted to the Government (CDRLs CAPSTONE-2 and CAPSTONE-3).

Qualification Data Review (QDR)

The Contractor shall present rational to Launch Service Program (LSP) showing that the below listed vehicle components and subsystems are “qualified” to the Contractor’s satisfaction (i.e.

meets internal standards, documented deviation/waiver processes, and risk management practices). The QDR will include a high-level description of the as-built and qualified implementation/fabrication, the component or assembly part number, and details on any differences in between the qualification and flight configurations. Sufficient information shall be presented for LSP to understand what component acceptance, component qualification, and system level qualification/compatibility testing has been performed and if or how all elements of the hardware’s entire life cycle have been accounted for in the qualification determination.

Qualification rationale shall include the qualification and acceptance test and/or analysis levels, the environments derivation methodology and examples. The rationale will be clear on the use of analysis, test and/or similarity. All anomalies and deviations from the qualification test plans/procedures, with associated resolutions and rationale will be identified.

The QDR presentation shall address the core stage engines and tanks, flight computer, Inertia Navigation Unit (INU), engine actuators, main batteries, separation systems, and flight software processes/test status. It shall also address analysis methods, assumptions, results and margins for launch vehicle loads, trajectory, controls and thermal.

It is recognized and accepted by NASA that the contractor chooses or maintains their own technical standards for design and test and NASA will not approve them. The Contractor’s technical standards for design and test of the vehicle shall be included in the final presentation package. The final presentation package shall be provided 1 week prior to the QDR or the QDR will be rescheduled.

NASA reserves the right to withhold approval of this milestone if the design of the listed items is not qualified to the Contractor’s standard(s) and until all action items related to the payload interface have been closed.

Post Flight Data Review (PFDR)

The Contractor may choose to provide a PFDR in lieu of a QDR if there has been a successful flight of the launch vehicle using core engines and core stages identified in milestones 3 (Core Stage Engines Qualification Testing Complete) and 4 (Core Stages Propulsion Qualification Testing Complete)

The Contractor shall present the PFDR with a technical team to a Launch Services Program small, multifunctional technical team that includes a safety and mission assurance representative.

The Contractor’s post fight data report, in their own format, shall be provided 1 month prior to the PFDR. Regardless of what is in the post-fight data report, the PFDR shall include identification of actual vehicle and performance parameters in the flight telemetry which exceed three sigma predictions, regardless of Contractor’s mission success determination. The Contractor’s resolution or plans for resolution of the anomalies shall also be presented to NASA.

NASA reserves the right to withhold approval of this milestone if the anomaly resolution plans do not support the CAPSTONE contract launch date.

Launch Vehicle Readiness Review

The Contractor shall conduct a Launch Vehicle 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 payload and launch vehicle configuration; integration status; summary of mission specific waivers; mission specific analyses results; status including updates, if any, from the QDR; flight launch vehicle and launch site hardware/software production and testing status, and Contractor’s assessments of any significant manufacturing and test anomalies.

ii. A detailed schedule showing all activities (ground and flight with relationship to any other manifested missions) remaining to achieve a successful, on-time CAPSTONE launch.

Launch

Flight Readiness Review (FRR)

The Contractor shall conduct an FRR for the mission to ensure the launch vehicle is acceptable for flight to their satisfaction and all Range and other mission requirements have been met or will be satisfied prior to launch. The FRR shall include participation from any appropriate Range approving officials.