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Aerodynamic characteristics of two trailblazer ii blunted 9 deg cone reentry bodies at mach 6.8 in air and 21.2 in heliumEffect of aerodynamic characteristics of nose bluntness on electromagnetic and luminous efficiency by comparing radar and optical data of two reentry bodies at escape velocities
Document ID
19650014772
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Marcum, D. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Neal, L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Schippell, H. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2786
Report Number: NASA-TN-D-2786
Accession Number
65N24373
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REENTRY BODY
LUMINOUS INTENSITY
NOSE CONE
ELECTROMAGNETIC PROPAGATION
RADAR DATA
AERODYNAMIC CHARACTERISTICS

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