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Aerodynamic characteristics of two blunt, half-cone wedge entry configurations at Mach numbers from 2.30 to 4.63Aerodynamic characteristics of two blunt half cone wedge entry configurations at supersonic speeds
Document ID
19680020558
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Foster, G. V. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1621
Report Number: NASA-TM-X-1621
Accession Number
68N30030
Funding Number(s)
CONTRACT_GRANT: 124-08-03-18-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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