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Experimental hydrogen-fluorine rocket performance at low pressures and high ratiosHydrogen-fluorine performance at low combustion chamber pressures in rockets with high area ratio exhaust nozzles
Document ID
19660024035
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Aukerman, C. (NASA Lewis Research Center Cleveland, OH, United States)
Church, B. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1963
Subject Category
Propellants
Report/Patent Number
NASA-TM-X-724
Report Number: NASA-TM-X-724
Accession Number
66N33325
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
CHAMBER PRESSURE
HYDROGEN
EXHAUST NOZZLE
FLUORINE
COMBUSTION CHAMBER

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