Attachment A.2 Launch Requirements.pdf
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- Attached to
- 80KSC020R0003 - CAPSTONE - Cislunar Autonomous Positioning System Technology Operations and Navigation Experiment - Launch Service Federal contract opportunity
- Solicitation number
- 80KSC020R0003
About this file
This solicitation requests launch services for the CAPSTONE spacecraft. NASA's Kennedy Space Center is seeking proposals to deliver the CAPSTONE spacecraft to a cislunar orbit via launch vehicle. Offerors must provide a launch vehicle capable of meeting the spacecraft's envelope, mass properties, mechanical interface requirements, and electrical interface requirements as specified in Attachment A.2. Proposals are due no later than the date and time set for receipt. Questions regarding the solicitation must be received by the contracting officer by December 18, 2019 to allow for analysis and response prior to the proposal due date.
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Tyvak Proprietary Information CAPSTONE Attachment A.2 – Launch Requirements 80KSC020R0003
CAPSTONE Spacecraft Envelope/Mass Properties, Mechanical Interface Requirements, and Electrical Interface Requirements
Tyvak Proprietary Information CAPSTONE Attachment A.2 – Launch Requirements 80KSC020R0003
• The payload dispenser has thermostatically controlled four each 5W 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 Attachment A.3, Tyvak 12U dispenser Users Guide
Electrical Interface Requirements
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