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ROCKET ENGINE STARTING WITH MIXED OXIDES OF NITROGEN AND LIQUID AMMONIA BY FLOW-LINE ADDITIVESRocket engine starting with mixed oxides of nitrogen and liquid ammonia by flow-line additives
Document ID
19630002660
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Hennings, G. (NASA Lewis Research Center Cleveland, OH, United States)
Humphrey, J. C. (NASA Lewis Research Center Cleveland, OH, United States)
Kinney, G. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
August 19, 1953
Subject Category
Propellants
Report/Patent Number
NACA-RM-E53F05
Report Number: NACA-RM-E53F05
Accession Number
63N12536
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
IGNITION SYSTEM
LIQUID PROPELLANT
LIQUID AMMONIA
ADDITIVE
NITROGEN OXIDE

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