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Orbit Transfer Vehicle (OTV) Engine: Phase A Study - Volume II: Study ReportsThe 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
Marshall Space Flight Center
Document Type
Contractor Report (CR)
Authors
J A Mellish (Aerojet Sacramento, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 29, 1979
Publication Information
Publisher: National Aeronautics and Space Administration
Volume: 2
Subject Category
Spacecraft Propulsion and Power
Report/Patent Number
NASA-CR-161298
REPT-32999-F-VOL-2
Accession Number
79N33236
Funding Number(s)
CONTRACT_GRANT: NAS8-32999
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management

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