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The effect of surface reactions on the solid propellant response function.Surface coupled heat release effect on oscillatory amplitude of pressure coupled response in solid propellant
Document ID
19670051254
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Marxman, G. A.
Wooldridge, C. E.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Propellants
Accession Number
67A29983
Funding Number(s)
CONTRACT_GRANT: AF 49/638/-1367
CONTRACT_GRANT: NAS7-389
Distribution Limits
Public
Copyright
Other
Keywords
SOLID PROPELLANT
SURFACE REACTION
GAS PHASE
COMBUSTION INSTABILITY
PRESSURE OSCILLATION
EXOTHERMIC REACTION

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