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Wind-tunnel investigation of thermal and pressure environments in the base of the Saturn S-IC booster from Mach 0.1 to 3.5Wind tunnel testing of thermal and pressure in base of Saturn S-IC booster
Document ID
19660026835
Document Type
Other - NASA Technical Note (TN)
Authors
Wasko, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-3612
Accession Number
66N36125
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL
SATURN S-IC STAGE
BASE PRESSURE

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