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Orbit Transfer Vehicle (OTV) engine phase A study, extension 1. Volume 3: Study cost estimatesProgram cost and planning data based on 1980 technology and shown in 1979 dollars for a 20K lb Thrust Staged Combustion Cycle Engine are presented. These data were compared with those for the Advanced Expander Cycle Engine at 10K lb and 20K lb thrust levels.
Document ID
19810003651
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Christensen, K. L.
(Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 4, 2013
Publication Date
August 20, 1980
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
REPT-32999-F-E1-VOL-3
NASA-CR-161608
Report Number: REPT-32999-F-E1-VOL-3
Report Number: NASA-CR-161608
Accession Number
81N12161
Funding Number(s)
CONTRACT_GRANT: NAS8-32999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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