A program was conducted to demonstrate and establish the applicability of using dual property steel armore (DPSA) integrally in complex Army aircraft critical components, thus eliminating or minimizing the requirement for adding armor plate (shielding) to protect these components from small-arms ballistic impacts. A CH-54B primary flight control hydraulic servo actuator was selected as the critical component and was redesigned using DPSA as the cylinder material. Three experimental units were fabricated and tested. (Author)


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    Title :

    Design, Fabrication, and Performance Testing of Integral Armored Servo Actuators


    Contributors:

    Publication date :

    1972


    Size :

    118 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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