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Effect of oxidizer particle size on solid- propellant combustion stabilityOxidizer particle size effect on solid propellant combustion stability
Document ID
19650011392
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Morrell, G. (NASA Lewis Research Center Cleveland, OH, United States)
Pinns, M. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1965
Subject Category
Propellants
Report/Patent Number
NASA-TN-D-2736
Report Number: NASA-TN-D-2736
Accession Number
65N20993
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
OXIDIZER
SOLID PROPELLANT
PARTICLE SIZE
COMBUSTION STABILITY

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