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Thermodynamic property measurements in reflected shock air plasmas at 12,000 - 16,000 KReflected shock air plasma thermodynamic properties at 12,000 to 16,000 deg K
Document ID
19700023343
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wilson, K. H. (Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Wood, A. D. (Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
August 5, 2013
Publication Date
July 1, 1970
Publication Information
Publisher: NASA
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-1617
Report Number: NASA-CR-1617
Accession Number
70N32654
Funding Number(s)
CONTRACT_GRANT: NAS7-704
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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