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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    Title :

    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


    Contributors:

    Publication date :

    1966


    Size :

    129 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English