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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    Titel :

    Simulated-altitude testing


    Weitere Titelangaben:

    Aircraft Production


    Erschienen in:

    Erscheinungsdatum :

    1947


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Simulated-altitude rocket testing

    Goethert, B.H. | Engineering Index Backfile | 1961


    Engine testing at simulated altitude conditions

    ROBERTS, J. / GUIDONE, J. / MANCUSO, B. et al. | AIAA | 1993




    Simulated altitude testing in USAF engine test facility

    Ferrell, J. / Harvey, R.W. | Engineering Index Backfile | 1956