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Aerodynamic heating at Mach 8 of attached inflatable decelerator configurationsMach 8 variable-density tunnel used for determination of aerodynamic heating of attached inflatable decelerator configurations
Document ID
19710029282
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Creel, T. R., Jr. (NASA Langley Research Center Hampton, VA, United States)
Miserentino, R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-2355
L-7864
Report Number: NASA-TM-X-2355
Report Number: L-7864
Accession Number
71N38758
Funding Number(s)
PROJECT: RTOP 117-07-04-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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