Attachment 05 Launch Service Capabilities Specs and Envs.pdf

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Venture-Class Acquisition of Dedicated and Rideshare (VADR) Launch Services
Solicitation number
80KSC021R0034
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This solicitation is for Venture-Class Acquisition of Dedicated and Rideshare Launch Services. The National Aeronautics and Space Administration John F. Kennedy Space Center is seeking proposals for indefinite-delivery/indefinite-quantity firm-fixed-price launch services contracts with a potential period of performance from October 2021 through 2026. Offerors must submit proposals by June 28, 2021. The North American Industry Classification System code for this acquisition is 481212 and the small business size standard is 1,500 employees. The solicitation includes requirements for launch vehicle capabilities and specifications, payload processing facilities, launch site integration services, and additional unique launch service capabilities. Award is anticipated in October 2021.

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Attachment 01 SOW.pdf PDF
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Amendment 1.pdf PDF
VADR RFP.docx DOCX document
Appendix A Past Performance Questionnaire.docx DOCX document
Attachment 05 Launch Service Capabilities Specs and Envs.docx DOCX document
Attachment 01 SOW.pdf PDF
VADR Change Log.pdf PDF
LAUNCH VEHICLE CERTIFICATION LSP PLN 324.01 Rev C.pdf PDF
VADR RFP.pdf PDF
VADR Questions and Responses.pdf PDF
Attachment 04 Definitions.pdf PDF
Attachment 02 Meetings and Formal Reviews.pdf PDF
Attachment 03 CDRLS.pdf PDF
Appendix A Past Performance Questionnaire.pdf PDF
VADR RFP Cover Letter.pdf PDF
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VADR RFP ATTACHMENT 05 80KSC021R0034

LAUNCH SERVICES CAPABILITIES, SPECIFICATIONS AND ENVIRONMENTS

ATTACHMENT 05

FOR

Venture-Class Acquisition of Dedicated and Rideshare (VADR) Launch Services

VADR RFP ATTACHMENT 05 80KSC021R0034

Requirements for Launch, Upper-Stage and Space Vehicles (SMC-S-016), the Contractor shall identify mitigation options. Some missions may require specific limits to launch environments.

Figure TBP

Figure A5-1: Maximum Electromagnetic Radiated Emissions Levels Encountered by the Payload

Figure A5-2: Maximum Electromagnetic Radiated Susceptibility Levels of the Launch System

Figure A5-3: PLF Pressure Profiles and Depressurization Rates

Table A5-8: Maximum Flight-Level Payload Acoustic Environment

Table TBP

VADR RFP ATTACHMENT 05 80KSC021R0034

Figure A5-4: Maximum Quasi-Steady Acceleration as a Function of Payload Separated Mass

Figure A5-5: Maximum Thermal Environment During Ascent

Rideshare Payload Adapter System(s)

Describe the commercial rideshare payload adapter and separation system(s), including physical and electrical characteristics provided by the Offeror for each proposed vehicle configuration.

Include a graphical description for separating and non-separating payloads and state associated ground rules that apply to the rideshare payload accommodations, including any CubeSat dispenser offerings.

Launch Site Integration

a. Describe the physical attributes, the capabilities, and the limitations (e.g. fueling, transportation, airlock, lifting, office space, GSE accommodation) of any payload processing facilities (PPF) to be available for any launch service being proposed including PPF occupancy duration(s). Specify the contamination environments achievable in the PPF and within the payload fairing. In addition, specify the temperature and humidity environments to which the PPF and PLF can be controlled (TBP to TBP°C (TBP to TBP°F) and TBP% to TBP%, respectively).

b. Describe the services, equipment, support, and limitations provided at the launch site(s) for the integration and launch of each payload.

Additional Information

Describe any unique capabilities of the proposed launch service. This should include anything that the Contractor wishes to emphasize as unique to their launch service.

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