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Space shuttle RCS engineThe design of the space shuttle RCS engine has the primary objective of reusability with minimum servicing. Engine S/N FT-2A has successfully completed all ten environmental (salt water spray, sand and dust, vibration and humidity) and hot fire cycles with no change in engine performance (steady state or pulse mode).
Document ID
19740002607
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
August 22, 1973
Subject Category
Propulsion Systems
Report/Patent Number
REPT-8701-910013
NASA-CR-136021
Report Number: REPT-8701-910013
Report Number: NASA-CR-136021
Accession Number
74N10720
Funding Number(s)
CONTRACT_GRANT: NAS9-12996
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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