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Orbit Transfer Vehicle (OTV) advanced expander cycle engine point design study, volume 2The engine requirements are emphasized and include: high specific impulse within a restricted installed length constraint, long life, multiple starts, different thrust levels, and man-rated reliability. The engine operating characteristics and the major component analytical design are summarized.
Document ID
19810021640
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
March 15, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-161832
FR-14615-VOL-2
Report Number: NASA-CR-161832
Report Number: FR-14615-VOL-2
Accession Number
81N30179
Funding Number(s)
CONTRACT_GRANT: NAS8-33567
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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