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Stability and drag characteristics at Mach numbers of 10 and 26 of a proposed slender atmospheric probeStability and drag characteristics of slender, flare-stabilized cone cylinder for Mars atmospheric probe at Mach numbers 10 and 26
Document ID
19670013967
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Malcolm, G. N.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3917
Report Number: NASA-TN-D-3917
Accession Number
67N23296
Funding Number(s)
CONTRACT_GRANT: 124-07-02-13-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SLENDER BODY
DRAG
AERODYNAMIC STABILITY
MARS PROBE
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