It is shown that takeoff weight of helicopter can be considerably increased in operations which are based at airfield, provided helicopter is of suitable configuration to permit running takeoff; piloting technique for running takeoff and increase in payload range capability is shown for particular helicopter; suitable helicopters are Bell HSL, Bristol 192 and possibly 173, Vertol HUP and Yak-24.


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    Titel :

    Increase in helicopter payload through running takeoff


    Weitere Titelangaben:

    Can Aeronautical J


    Beteiligte:
    Adams, G.N. (Autor:in) / Sevier, H.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1958


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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