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Interrelations between combustion phenomena and mechanical properties in solid propellant rocket motors.Static and dynamic combustion phenomena effects on grain structural design for solid propellant rocket engine
Document ID
19670042147
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Parker, K. H.
Summerfield, M.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Propellants
Accession Number
67A20876
Distribution Limits
Public
Copyright
Other
Keywords
PROPELLANT GRAIN
STRUCTURAL DESIGN
COMBUSTION STABILITY
SOLID PROPELLANT ROCKET ENGINE

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