Wind Tunnel Tests Of Space Shuttle External Tank Insulation Material In The Aerothermal Tunnel At Elevated 1440 F Total Temperatures Addendum
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Wind Tunnel Tests of Space Shuttle External Tank Insulation Material in the Aerothermal Tunnel at Elevated (1440 F) Total Temperatures. Addendum
Wind tunnel tests of the Space Shuttle External Tank Foam Insulation were conducted in the von Karman Gas Dynamics Facility Tunnel C. For these tests, Tunnel C was run at Mach 4 with a total temperature of 1440 F and a total pressure which varied from 30-100 psia. Cold wall heating rates were changed by varying the test article support wedge angle and by adding or removing a shock generator or cylindrical protuberance. (Author).
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