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Superalloy material test in a plasma arc tunnelSeven superalloy models were tested in a plasma arc tunnel at the peak heating condition existing on the space shuttle orbiter's lower surface during a low cross-range entry. The models were 3 x 3 in. flat surfaces, nominally 0.01 to 0.02 in. thick, and were held in a water-cooled wedge holder at a 60 deg angle of attack. Five test models were recycled 25 times for 10 min periods (two were recycled 50 times) in a Mach 4.6 test stream, with the model's leading edge temperature maintained at 2200 F (2000 F in one case).
Document ID
19720014644
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Land, D. W.
(McDonnell-Douglas Corp. Saint Louis, MO, 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
72N22294
Funding Number(s)
CONTRACT_GRANT: NAS3-14666-H
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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