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AERODYNAMIC CHARACTERISTICS AT A MACH NUMBER OF 6.77 OF A 9 DEG CONE CONFIGURATION, WITH AND WITHOUT SPHERICAL AFTERBODIES, AT ANGLES OF ATTACK UP TO 180 DEG WITH VARIOUS DEGREES OF NOSE BLUNTINGAerodynamic characteristics at mach 6.77 of 9-deg cone, with and without spherical afterbody and nose blunting at angles of attack to 180-deg
Document ID
19630003686
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Neal, L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1606
Report Number: NASA-TN-D-1606
Accession Number
63N13562
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AFTERBODY
AERODYNAMIC CHARACTERISTICS
REENTRY VEHICLE
CONE
NOSE
HYPERSONIC SPEED
BLUNT BODY

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