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Advanced oxygen-hydrocarbon rocket engine studyPreliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket engine cycles is reported. A consistent and reliable data base for vehicle optimization and design studies, to demonstrate the significance of propulsion system improvements, and to select the critical technology areas necessary to realize such advances is presented.
Document ID
19800010909
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Obrien, C. J. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 11, 1980
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-161390
REPT-33452-M2
Report Number: NASA-CR-161390
Report Number: REPT-33452-M2
Accession Number
80N19186
Funding Number(s)
CONTRACT_GRANT: NAS8-33452
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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