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Heat-transfer Measurements on a Blunt Spherical-segment Nose to a Mach Number of 15.1 and Flight Performance of the Rocket-propelled Model to a Mach Number of 17.8Heat transfer measurements on blunt spherical segment nose and cylindrical body and flight test of rocket-propelled model
Document ID
19650018847
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lee, D. B. (NASA Langley Research Center Hampton, VA, United States)
Rumsey, C. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1959
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-77
Report Number: NASA-TM-X-77
Accession Number
65N28448
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLIGHT TEST
HEAT TRANSFER
ROCKET
NOSE

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