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An experimental investigation of gas evolution from a solid rocket propellant during pressure transients.Mass flow rate of gas evolution from burning solid rocket propellant during transient depressurization of combustion chamber
Document ID
19650031864
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bunde, G. W.
Fletcher, E. A.
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 65-104
Report Number: AIAA PAPER 65-104
Accession Number
65A14568
Funding Number(s)
CONTRACT_GRANT: NAS3-2554
Distribution Limits
Public
Copyright
Other
Keywords
TRANSIENT PRESSURE
MASS FLOW RATE
GAS EVOLUTION
ROCKET CHAMBER
PROPELLANT COMBUSTION
SOLID PROPELLANT IGNITION

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