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Static longitudinal aerodynamic characteristics of some supersonic decelerator models at Mach numbers of 2.30 and 4.63Aerodynamic characteristics of blunted cones, tension shell, and attached inflatable decelerator models
Document ID
19690017192
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Davenport, E. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1969
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-5219
Report Number: NASA-TN-D-5219
Accession Number
69N26570
Funding Number(s)
CONTRACT_GRANT: 124-07-02-67-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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