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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    Titel :

    Aerospatiale's Experience on Helicopter Flight in Icing Conditions


    Beteiligte:
    D. Trivier (Autor:in) / G. Avedissian (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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