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System specification for the reusable reentry satelliteThe RRS design shall provide a relatively inexpensive method of access to micro and fractional gravity space environments for an extended period of time, with eventual intact recovery on the surface of the Earth. This specification establishes the performance, design, development, and test requirements for the Reusable Reentry Satellite (RRS) system.
Document ID
19930006443
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
February 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:187882
NASA-CR-187882
SAIC-RRS-038
RRS-SS-100
Report Number: NAS 1.26:187882
Report Number: NASA-CR-187882
Report Number: SAIC-RRS-038
Report Number: RRS-SS-100
Accession Number
93N15632
Funding Number(s)
CONTRACT_GRANT: NAS9-18202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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