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Investigation of injectors for a low-chamber- pressure hydrogen-fluorine rocket enginePerformance tests of low pressure drop coaxial and shower-head injectors for gaseous hydrogen- liquid fluorine rocket chamber
Document ID
19660024043
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lubick, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Price, H. G., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Shinn, A. M., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1962
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-485
Report Number: NASA-TM-X-485
Accession Number
66N33333
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYDROGEN FUEL
ROCKET CHAMBER
FUEL INJECTION
FLUORINE
HIGH ENERGY PROPELLANT
PRESSURE DROP

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