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A preliminary investigation of oxidizer-rich oxygen-hydrogen combustion characteristicsIgnition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen propellant mixture combustion
Document ID
19670002483
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Bailey, C. R. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-3729
Report Number: NASA-TN-D-3729
Accession Number
67N11812
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
IGNITION
HYDROGEN FUEL
PROPELLANT COMBUSTION
LIQUID OXYGEN /LOX/

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