Study investigates whether military and commercial transport capabilities of helicopter are likely to be surpassed in future by different VTOL designs and is confined to performance capabilities and cost of medium size, unpressurized, low subsonic speed, cargo, or passenger carrying vehicles; propulsion systems; VTOL, STOL and ejector configurations tabulated; method of analysis and ground rules; military and commercial direct operating costs, military and commercial capability.


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    Title :

    V/STOL cargo airplane characteristics


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    STOL demonstrated feasible for large cargo BLC airplane

    Dickerman, F.N. / Branson, C.F. | Engineering Index Backfile | 1961


    Development of STOL airplane

    MacDonald, A.F. | Engineering Index Backfile | 1960


    Preliminary design of "ARAVA" STOL airplane

    Mankuta, H. / Sa'Ar, D. | Engineering Index Backfile | 1967


    Commercial STOL - The Airplane, the Airport

    Davy, M. C. W. | SAE Technical Papers | 1978


    Fan inlet for a V/STOL airplane

    KONCSEK, J. / SYBERG, J. | AIAA | 1977