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Performance and stability of rocket engine injectors using lox/rp-1 propellantsPerformance and stability characteristics of rocket engine injectors using liquid oxygen propellant
Document ID
19640023956
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bailey, C. R. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
September 4, 1964
Subject Category
Propellants
Report/Patent Number
NASA-TM-X-53126
Report Number: NASA-TM-X-53126
Accession Number
64N33870
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
INJECTOR

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