Features of new de Havilland test chambers for airframe components and fuel systems; specification called for installation able to hold large section of transport aircraft fuselage or complete fighter fuselage, and capable of evacuation to pressure equivalent to altitude of 70,000 ft with internal temperature controllable between 40 and -- 70 C.
Simulated-altitude testing
Aircraft Production
Aircraft Production ; 9 , n 110
1947
3 pages
Article (Journal)
English
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