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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Concrete phase in development of load detachability principle in aircraft


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:

    Published in:

    Publication date :

    1951


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





    Quick release system vest with improved detachability

    KIM HAN GON | European Patent Office | 2022

    Free access

    Quick release system vest with improved detachability

    European Patent Office | 2024

    Free access

    Aircraft combining windlass lever principle and air pressure power principle

    ZHOU WEIPING | European Patent Office | 2023

    Free access

    Aircraft load cabin and aircraft

    LIU QING / YONG SIWEN / ZHONG WEN et al. | European Patent Office | 2024

    Free access