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STATIC AERODYNAMIC CHARACTERISTICS OF A THREE-STAGE ROCKET VEHICLE HAVING VARIOUS FIN CONFIGURATIONS AT LOW SUBSONIC MACH NUMBERS AND ANGLES OF ATTACK UP TO 28 DEGStatic aerodynamic characteristics of three-stage trailblazer ii rocket vehicle determined in low turbulence pressure wind tunnel
Document ID
19630005431
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Brown, C. A., Jr. (NASA Langley Research Center Hampton, VA, United States)
Putnam, L. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1786
Accession Number
63N15307
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRAILBLAZER II REENTRY VEHICLE
TURBULENCE
STATIC AERODYNAMIC CHARACTERISTICS
WIND TUNNEL

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