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Orbit Transfer Vehicle (OTV) Engine: Phase A Study - Volume I: Executive SummaryDesign and parametric data for the hydrogen oxygen engine used in the orbiter transfer vehicle are presented. The engine design is analyzed and minimum engine performance and man rating requirements are discussed. Candidate cycle performance, weight and tradeoff analysis, and cost estimates are reported.
Document ID
19790025064
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: 1
Subject Category
Spacecraft Propulsion and Power
Report/Patent Number
NASA-CR-161297
REPT-32999-F-VOL-1
Accession Number
79N33235
Funding Number(s)
CONTRACT_GRANT: NAS8-32999
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management

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