Helicopter rotor icing protection systems are evaluated through flight tests under actual icing conditions. The development of a practical flight envelope which considers altitude, temperature, and icing severity is discussed. Flights without deicing protection are conducted to determine flight characteristics under total system failure.


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    Title :

    Aerospatiale's Experience on Helicopter Flight in Icing Conditions


    Contributors:
    D. Trivier (author) / G. Avedissian (author)

    Publication date :

    1983


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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