Engineering flight tests of the UH-1B helicopter equipped with the XM-16 and XM-21 armament subsystems were conducted. The overall objective was to determine the effect of the installation of the subsystems on the UH-1B. Specific objectives were to determine the existence of any safety-of-flight conditions by evaluation of equantitative stability and control and vibration data and to determine any performance losses.


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    Titel :

    Engineering Flight Test of UH-1B Helicopter Equipped with XM-16 Armament Subsystem and Engineering Flight Test of UH-1B Helicopter Equipped with XM-21 Armament Subsystem


    Beteiligte:
    G. M. Yamakawa (Autor:in) / J. K. Foster (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    129 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch