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Orbit Transfer Vehicle (OTV) advanced expander cycle engine point design study. Volume 3: Engine data summaryThe engine operating characteristics were examined. Inlet pressure effects, tank pressurization effects, steady-state specific impulse, and the steady-state cycle were studied. The propellant flow schematic and operating sequence are presented. Engine hardware drawings are included.
Document ID
19810021641
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-161833
FR-14615-VOL-3
Report Number: NASA-CR-161833
Report Number: FR-14615-VOL-3
Accession Number
81N30180
Funding Number(s)
CONTRACT_GRANT: NAS8-33567
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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