The patent application provides a circuit for driving a servo-amplifier which in turn drives a mechanical linkage mechanism attached to an aircraft member. The circuit electronically simulates a controlled load vs. time history for an aircraft holdback fitting fracture when the required catapult load is reached.


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    Title :

    Catapult Breakaway Load Simulator Circuit


    Contributors:
    R. D. Mood (author) / J. P. Hunter (author) / R. D. Burgen (author)

    Publication date :

    1975


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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