The flight characteristics and boundary conditions which affect a steep approach are described for rotary wing aircraft. The limits for steep instrument approach are presented, and experiences in flight operation are depicted. Essential advantages are shown for a flight path angle of 15 deg over the ILS approach. Some necessary prerequisites for a steep landing approach by instruments are briefly considered.


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    Title :

    Steep Approach Limits for Rotary Wing Aircraft ueber die Grenzen von Steilanfluegen MIT Drehflueglern


    Contributors:
    M. Rade (author)

    Publication date :

    1973


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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