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Effects of several ramp-fairing, umbilical, and pad configurations on aerodynamic heating to Apollo command module at Mach 8Variable density hypervelocity wind tunnel tests on effects of several ramp-fairing, umbilical, and pad configurations on aerodynamic heating to Apollo command module
Document ID
19680025669
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hunt, J. L. (NASA Langley Research Center Hampton, VA, United States)
Jones, R. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1640
Report Number: NASA-TM-X-1640
Accession Number
68N35141
Funding Number(s)
CONTRACT_GRANT: 129-01-03-07-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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