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Advanced oxygen-hydrocarbon rocket engine studyThe advantages and disadvantages, system performance and operating limits, engine parametric data, and technology requirements for candidate high pressure LO2/Hydrocarbon engine systems are summarized. These summaries of parametric analysis and design provide a consistent engine system data base. Power balance data were generated for the eleven engine cycles. Engine cycle rating parameters were established and the desired condition and the effect of the parameter on the engine and/or vehicle are described.
Document ID
19810014652
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Obrien, C. J. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Salkeld, R. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 4, 2013
Publication Date
June 10, 1980
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-161759
REPT-33452-M-4
BMPR-4
Report Number: NASA-CR-161759
Report Number: REPT-33452-M-4
Report Number: BMPR-4
Accession Number
81N23185
Funding Number(s)
CONTRACT_GRANT: NAS8-33452
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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