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Experimental performance of a hydrogen- fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratiosExperimental performance of hydrogen-fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios
Document ID
19660024058
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Aukerman, C. A. (NASA Lewis Research Center Cleveland, OH, United States)
Gibb, J. W. (NASA Lewis Research Center Cleveland, OH, United States)
Jones, W. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1960
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-387
Report Number: NASA-TM-X-387
Accession Number
66N33348
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NOZZLE EXPANSION
HYDROGEN FUEL
FLUORINE
LIQUID PROPELLANT ROCKET ENGINE
CHAMBER PRESSURE

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