The results of a flight test program utilizing a flexible wing air cargo delivery vehicle are presented. The objective of the program was to prove the feasibility of this vehicle for the delivery of cargo in a logistic system. Discussed are performance characteristics and handling qualities of both the towed flexible wing and the tow helicopter.


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    Titel :

    Flexible Wing Air Cargo Glider Delivery System


    Beteiligte:
    N. Sakamoto (Autor:in) / G. Cota (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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