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.


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    Title :

    Simulated-altitude testing


    Additional title:

    Aircraft Production


    Published in:

    Publication date :

    1947


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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