The United States Army Aviation Systems Test Activity conducted a limited performance and handling qualities evaluation of the AH-1G helicopter with a Bell Helicopter Company commercial Model 212 tail rotor installed. This installation included changes to the pitch links and pitch control tube to accommodate the Model 212 tail rotor; however, the remaining components of the tail rotor drive system were standard AH-1G items. The evaluation was performed during the period 29 May to 7 August 1973 at Edwards Air Force Base, Bakersfield, and Bishop, California. (Modified author abstract)


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    Titel :

    Engineering Flight Test - AH-1G Helicopter with Model 212 Tail Rotor. Part II. Performance and Handling Qualities


    Beteiligte:
    J. I. Nagata (Autor:in) / G. L. Skinner (Autor:in) / L. J. Hepler (Autor:in) / G. A. Smith (Autor:in) / P. R. Bonin (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    121 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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