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The ignition transient in solid propellant rocket motors.Ignition pressure transient of rocket motor, discussing initial ignition event, flame spreading and final chamber filling, convective heating effect on burning rate, etc
Document ID
19660055159
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Most, W. J.
Parker, K. H.
Summerfield, M.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 66-666
Report Number: AIAA PAPER 66-666
Accession Number
66A34449
Distribution Limits
Public
Copyright
Other
Keywords
CONVECTIVE HEAT TRANSFER
SOLID PROPELLANT ROCKET ENGINE
TRANSIENT PRESSURE
BURNING RATE
FLAME PROPAGATION
IGNITION SYSTEM

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