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Evaluation of Injector Principles in a 2400-pound-thrust Rocket Engine Using Liquid Oxygen and Liquid AmmoniaInjector evaluation in 2400-pound-thrust rocket engine using liquid oxygen and liquid ammonia
Document ID
19630004011
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Ehlers, R. C. (NASA Lewis Research Center Cleveland, OH, United States)
Graham, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Hendricks, R. C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1959
Subject Category
Propellants
Report/Patent Number
NASA-MEMO-12-11-58E
Report Number: NASA-MEMO-12-11-58E
Accession Number
63N13887
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
LIQUID OXYGEN /LOX/
LIQUID AMMONIA
INJECTOR

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