This report discusses the design, analysis, and performance evaluation of a helium driven closed center servo actuator system. The actuator was sized to operate a trapped ball type of movable nozzle thrust vector control system for tactical missiles. Predicted and actual performance are compared and typical test data are presented. (Author)


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    Title :

    Low Cost Servo Actuator for Tactical Missile Thrust Vector Control (TVC)


    Contributors:
    R. Levi (author) / P. H. Stahlhuth (author)

    Publication date :

    1977


    Size :

    118 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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