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The interior ballistics of the fluid controlled solid rocket motorFluid controlled solid rocket motor using fully oxidized solid propellant grain configured with oversized nozzle throat area
Document ID
19670002791
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Heiney, O. K. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
August 31, 1966
Subject Category
Propulsion Systems
Accession Number
67N12120
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SOLID PROPELLANT ROCKET ENGINE
NOZZLE GEOMETRY
FLUID POWER
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