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Compressed-air model investigation of solid rocket overpressures due to interference from aft-end ignition rocketSolid rocket combustion chamber overpressures due to interference from aft-end ignition rocket
Document ID
19660022899
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Salmi, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3537
Report Number: NASA-TN-D-3537
Accession Number
66N32189
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET BOOSTER
CHAMBER PRESSURE
SOLID PROPELLANT IGNITION
COMBUSTION CHAMBER

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