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STS spin-stabilized upper stage study (study 2.6). Volume 1: Executive summarySpinning solid propellant upper stage rocket engines designed for geosynchronous satellite payloads are investigated. Factors considered include: impact of the spinning stages on the payloads; applicability to 1981-1991 NASA mission model; and cost effectiveness.
Document ID
19760007073
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
September 30, 1975
Subject Category
Space Transportation
Report/Patent Number
ATR-75(7367)-1-VOL-1
NASA-CR-145907
Report Number: ATR-75(7367)-1-VOL-1
Report Number: NASA-CR-145907
Accession Number
76N14161
Funding Number(s)
CONTRACT_GRANT: NASW-2727
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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