Prototype CL-84 V/STOL aircraft which is in advanced stage of construction at Canadair Ltd, Montreal, is designed for Army support roles, in particular combat support and utility transport; V/STOL program, jointly funded by Canadian Dept of Defence Production and Canadair, is intended to develop CL-84 to point where military demonstrations can be made; structural features; lift-propulsion system includes, in each of 2 nacelles, engine and propeller/gearbox unit; engine is Lycoming T-53-LTCIK-4A; performance estimates; technical problems; comparison with other V/STOL aircraft.


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    Titel :

    Canadair tilt-wing/deflected slipstream V/STOL prototype program


    Weitere Titelangaben:

    Can Aeronautics Space J


    Beteiligte:
    Phillips, F.C. (Autor:in)


    Erscheinungsdatum :

    1964


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :