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Pressure measurements on rigid model of ballute decelerator at Mach numbers from 0.56 to 1.96Pressure measurements on rigid model of ballute decelerator at mach 0.56 to 1.96
Document ID
19660022653
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Turk, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3545
Report Number: NASA-TN-D-3545
Accession Number
66N31943
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE MEASUREMENT
DECELERATOR
RIGID STRUCTURE
BALLUTE
TRANSONIC WIND TUNNEL

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