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Orbit Transfer Vehicle (OTV) engine, phase A study. Volume 2: StudyThe hydrogen oxygen engine used in the orbiter transfer vehicle is described. The engine design is analyzed and minimum engine performance and man rating requirements are discussed. Reliability and safety analysis test results are presented and payload, risk and cost, and engine installation parameters are defined. Engine tests were performed including performance analysis, structural analysis, thermal analysis, turbomachinery analysis, controls analysis, and cycle analysis.
Document ID
19790025065
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mellish, J. A. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 29, 1979
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-161298
REPT-32999-F-VOL-2
Report Number: NASA-CR-161298
Report Number: REPT-32999-F-VOL-2
Accession Number
79N33236
Funding Number(s)
CONTRACT_GRANT: NAS8-32999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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