Facility at Palo Alto research laboratories of Lockheed Missile Systems Div, designed to investigate problems associated with heating and stability during re-entry from ICBM trajectory or satellite orbit; Hot Shot Facility supplies power to "low speed" blowdown tunnel with Mach number range from 10 to 24, and high speed shock tube facility for range above 100; advantages of arc heated and shock tube wind tunnels, compared.
Lockheed arc-heated hypersonic tunnel
Soc Automotive Engrs -- Paper
SAE Meeting ; 1958 Supersonic
1958
19 pages
Conference paper
English
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LOCKHEED ARC-HEATED HYPERSONIC TUNNEL
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