HEAT FLUX MEASUREMENT OF APOLLO CAPSULE MODEL AT HIGH STAGNATION PRESSURE IN SHOCK TUNNEL HIEST (AIAA 2018-5264)
AIAA International Space Planes and Hypersonic Systems and Technolgies (Conference)
2018-01-01
7 pages
Aufsatz (Konferenz)
Englisch
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Heat Flux Measurement of Apollo Capsule Model in the Free-Piston Shock Tunnel HIEST
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