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Heat-Transfer and Pressure Measurements from a Flight Test of the Second 1/18-Scale Model of the Titan Intercontinental Ballistic Missile up to a Mach Number of 3.91 and Reynolds Number Per Foot of 23.4 by 10 to the 6th Power
Document ID
19710075833
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Graham, J. B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
January 29, 1958
Subject Category
Unknown
Report/Patent Number
AF-AM-70
NACA-RM-SL58B10
Report Number: AF-AM-70
Report Number: NACA-RM-SL58B10
Accession Number
71X74415
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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