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Aerodynamic characteristics of three axisymmetric low fineness ratio reentry shapes at Mach 6.9Force, stability and control characteristics of three axisymmetric low fineness ratio reentry shapes at Mach 6.9
Document ID
19670024547
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Bernot, P. T. (NASA Langley Research Center Hampton, VA, United States)
Penland, J. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4122
Report Number: NASA-TN-D-4122
Accession Number
67N33876
Funding Number(s)
CONTRACT_GRANT: 124-07-02-57-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
LOW FINENESS RATIO
AXISYMMETRIC BODY
REENTRY BODY

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