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HEAT-TRANSFER AND PRESSURE DISTRIBUTIONS AT MACH NUMBERS OF 6.0 AND 9.6 OVER TWO REENTRY CONFIGURATIONS FOR THE FIVE-STAGE SCOUT VEHICLEHeat transfer and pressure distribution over reentry configuration for five-stage scout vehicle
Document ID
19630006418
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dunavant, J. C. (NASA Langley Research Center Hampton, VA, United States)
Holloway, P. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1963
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-1790
Report Number: NASA-TN-D-1790
Accession Number
63N16294
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SCOUT LAUNCH VEHICLE
PRESSURE DISTRIBUTION
REENTRY EFFECT

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