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Aerodynamic characteristics from mach 0.22 to 4.65 of a two-stage rocket vehicle having an unusual nose shape high power, high voltage, audio frequency transformer design manual final report, 1 jul. 1962 - 31 aug. 1964Transonic and supersonic aerodynamic characteristics for two-stage rocket vehicle with blunted nose cone on square body with conical flare termination
Document ID
19650000798
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Suttles, J. T. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1964
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2163
Accession Number
65N10399
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET VEHICLE
SUPERSONIC WIND TUNNEL
TRANSONIC WIND TUNNEL
TWO-STAGE ROCKET
AERODYNAMIC CHARACTERISTICS
NOSE CONE

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