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Apollo afterbody heat transfer and pressure with and without ablation at M infinity of 5.8 to 8.3Apollo afterbody heat transfer and pressure with and without ablation at Mach numbers 5.8 - 8.3
Document ID
19660027030
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Lee, G. (NASA Ames Research Center Moffett Field, CA, United States)
Sundell, R. E. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-3620
Report Number: NASA-TN-D-3620
Accession Number
66N36320
Funding Number(s)
CONTRACT_GRANT: 129-03-12-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AFTERBODY
HEAT TRANSFER
APOLLO SPACECRAFT
ABLATION

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