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Advanced oxygen-hydrocarbon rocket engine studyPreliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were used to produce a consistent and reliable data base for vehicle optimization and design studies. cycles G and C were chosen for design analysis. Preliminary design analysis of the heat transfer subsystem was performed to establish major technology requirements.
Document ID
19810020618
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Obrien, C. J. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Salkeid, R. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Mueggenburg, H. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Ewen, R. L. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 4, 2013
Publication Date
August 11, 1980
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
REPT-33452-M-5
NASA-CR-161758
Report Number: REPT-33452-M-5
Report Number: NASA-CR-161758
Accession Number
81N29156
Funding Number(s)
CONTRACT_GRANT: NAS8-33452
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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