Significance of Fairchild's XC-120 airplane with detachable fuselage; specifications presented; unique design problems posed by 4-wheel landing gear and fittings for locking pack of airplanes; numerous C-119 parts used in experimental plane; experiment considered to be first major step in separating cargo container from carrier in aircraft.


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    Titel :

    Concrete phase in development of load detachability principle in aircraft


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Lescher, G.W. (Autor:in) / Sterhardt, J.A. (Autor:in)


    Erscheinungsdatum :

    1951


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A CONCRETE PHASE IN THE DEVELOPMENT OF THE LOAD DETACHABILITY PRINCIPLE IN AIRCRAFT

    LESCHER, GEO. W. / STERHARDT, JAS. A. | SAE Technical Papers | 1950


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