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Advanced oxygen-hydrocarbon rocket engine studyA consistent engine system data base was generated for defining advantages and disadvantages, system performance and operating limits, engine parametric data, and technology requirements for candidate high pressure LO2/HC engine systems. Optimum LO2/HC engine power cycles were synthetized and representative conceptual engine design generated for a specified advanced surface to orbit transportation system.
Document ID
19800006944
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
December 10, 1979
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
MPR-33452M-1
NASA-CR-161350
Report Number: MPR-33452M-1
Report Number: NASA-CR-161350
Accession Number
80N15203
Funding Number(s)
CONTRACT_GRANT: NAS8-33452
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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