Design study of feasibility of flying crane type helicopters for Army usage made to determine optimum helicopter configuration for carrying 8 to 16 tons of cargo for distance of 10 to 100 nautical miles and to estimate costs for operation of cranes; production of helicopters within next 5 to 7 yr considered feasible; tip jet driven machines indicated to be superior to shaft driven machines for flying crane mission.


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    Titel :

    Summary of parametric studies of flying crane helicopters


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Graham, R.R. (Autor:in)


    Erscheinungsdatum :

    1958


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Flying helicopters by instruments

    Fay, J.S. | Engineering Index Backfile | 1950


    On flying qualities of helicopters

    Reeder, J.P. / Gustafson, F.B. | Engineering Index Backfile | 1949



    Physiological Effects of Flying Helicopters

    Wagstaff, A. S. / Flight Safety Foundation | British Library Conference Proceedings | 1997