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Wind tunnelsSupersonic wind tunnel test data, angle of attack envelope computations, and accelerometer package for reconstructing density profile of unknown atmosphere
Document ID
19670006387
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jaffe, P. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Klose, C. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Walker, B. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Weaver, R. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
October 31, 1965
Subject Category
Facilities, Research, And Support
Accession Number
67N15716
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ACCELEROMETER
ANGLE OF ATTACK
SUPERSONIC WIND TUNNEL
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