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Operating characteristics of the Air Force Flight Dynamics Laboratory 50 megawatt hypersonic tests legA 50 megawatt hypersonic arc wind tunnel was developed, with up to 5.0-feet-diameter test sections, for thermostructural tests of lifting entry vehicles.
Document ID
19720014642
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Beachler, J. C.
(Air Force Flight Dynamics Lab. Wright-Patterson AFB, OH, United States)
Kachel, W. A.
(Air Force Flight Dynamics Lab. Wright-Patterson AFB, OH, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Publication Information
Publication: NASA. Goddard Space Flight Center Space Simulation
Subject Category
Facilities, Research, And Support
Accession Number
72N22292
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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