Approach of DeHavilland Aircraft of Canada to STOL aircraft; advantages of civil and military applications; development and export figures of "Beaver" and "Otter"; project of larger unit DHC-4, Caribou, having aerodynamic and structural features tested in two earlier designs; expected payload of 2 1/2 tons and takeoff and landing run of about 500 ft; future trends.


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    Title :

    Slow take off and landing aeroplane


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:
    Bannack, R. (author)

    Conference:

    Society of Automotive Engineers -- Meeting (Canadian Section) ; 1957 Takeoff



    Publication date :

    1957


    Size :

    4 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    SLOW TAKE OFF AND LANDING AEROPLANE

    BANNACK, R. | SAE Technical Papers | 1957


    Aeroplane landing and take-off

    Engineering Index Backfile | 1936


    Aeroplane landing lights

    Calvert, E.S. | Engineering Index Backfile | 1938


    Aeroplane Landing Lights

    Calvert, E.S. | Emerald Group Publishing | 1938


    Aeroplane landing lights

    Calvert, E.S. | Engineering Index Backfile | 1938