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Wind tunnelsHypersonic wind tunnel stagnation conditions, wedge flow measurements, transonic entry capsule configuration, and internal pressure in conical pintle nozzle
Document ID
19670002786
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bate, E. R., Jr. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kerr, W. R. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Marko, W. J. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Walker, B. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Welton, J. T. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
August 31, 1966
Subject Category
Facilities, Research, And Support
Accession Number
67N12115
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WEDGE FLOW
SPACE CAPSULE
CONICAL NOZZLE
HYPERSONIC WIND TUNNEL
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