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PRESSURE DISTRIBUTIONS OVER THE FORWARD PORTION OF THE PROJECT FIRE SPACE-VEHICLE CONFIGURATION AT MACH NUMBERS FROM 0.25 TO 0.60Pressure distributions over forward portion of project fire space-vehicle configuration at subsonic speed
Document ID
19630003074
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Henderson, W. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1612
Report Number: NASA-TN-D-1612
Accession Number
63N12950
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION
REENTRY VEHICLE
FIRE PROJECT
SUBSONIC SPEED
SPACE PROBE

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