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A comparison of experimental heat-transfer coefficients in a nozzle with analytical predictions from Bartz's methods for various combustion chamber pressures in a solid propellant rocket motorComparison of experimental heat transfer coefficients in a nozzle with analytical predictions for various combustion chamber pressures in solid rocket propellant engine
Document ID
19690030691
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Smith, D. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-61900
Report Number: NASA-TM-X-61900
Accession Number
69N40076
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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