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A 3-inch combustion drive shock tube for studying chemical kineticsStructural analysis and operating ranges of 3-inch combustion drive shock tube for studying chemical kinetics
Document ID
19660020074
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Polentz, P. P. (NASA Ames Research Center Moffett Field, CA, United States)
Presley, L. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1965
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TM-X-56497
Report Number: NASA-TM-X-56497
Accession Number
66N29364
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK TUNNEL
CHEMISTRY
COMBUSTION
CHEMICAL KINETICS

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