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Heat-Transfer and Pressure Measurements from a Flight Test of a 1/18-Scale Model of the Titan Intercontinental Ballistic Missile up to a Mach Number of 3.95 and Reynolds Number Per Foot of 23 by 10 to the 6Th Power
Document ID
19710075828
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Chauvin, L. T. (NASA Langley Research Center Hampton, VA, United States)
Graham, J. B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Speegle, K. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
December 19, 1957
Subject Category
Unknown
Report/Patent Number
NACA-RM-SL57L16A
AF-AM-70
Report Number: NACA-RM-SL57L16A
Report Number: AF-AM-70
Accession Number
71X74410
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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