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Performance of a towed, 48-inch-diameter /121.92-cm/ ballute decelerator tested in free flight at Mach numbers from 4.2 to 0.4Inflation, drag, and stability characteristics of towed inflatable ballute decelerator at free flight
Document ID
19690008066
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Usry, J. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4943
Report Number: NASA-TN-D-4943
Accession Number
69N17398
Funding Number(s)
CONTRACT_GRANT: 124-07-03-05-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20070030990Supplement ToPerformance of a Towed, 48-Inch-Diameter (121.92) Ballute Decelerator Tested in Free-Flight Mach Numbers from 4.2 to 0.420070030990Supplemented ByPerformance of a Towed, 48-Inch-Diameter (121.92) Ballute Decelerator Tested in Free-Flight Mach Numbers from 4.2 to 0.4
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