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Gas evolution from a solid rocket propellant during depressurization to produce a quench.Mass flow rate of gas evolution from burning solid rocket propellant during transient depressurization of combustion chamber
Document ID
19660039873
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bunde, G. W.
Fletcher, E. A.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 65-104
Report Number: AIAA PAPER 65-104
Accession Number
66A19163
Funding Number(s)
CONTRACT_GRANT: NAS3-2554
Distribution Limits
Public
Copyright
Other
Keywords
GAS EVOLUTION
TRANSIENT PRESSURE
SOLID PROPELLANT IGNITION
ROCKET CHAMBER
PROPELLANT COMBUSTION
MASS FLOW RATE

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