Report of the fabrication and design verification testing of a Dual Mode Electro/Pneumatic Actuator. Pneumatic model open loop operation and control verified. Torque/Speed performance less than design goal due to excessive gear separation force. (Author)


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    Title :

    Advanced Flight Control Actuation System (AFCAS - E/P). Fabrication and Design Verification Testing of a Dual Mode Electro/Pneumatic Actuator for the T-2C Aircraft


    Contributors:
    W. Kineyko (author)

    Publication date :

    1982


    Size :

    55 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English