Future aerospace vehicles will require use of the Electrical Actuator systems for flight control elements. This report presents a proposed ELA Test Facility for dynamic evaluation of high power linear Electrical Actuators with primary emphasis on Thrust Vector Control actuators. Details of the mechanical design, power and control systems, and data acquisition capability of the test facility are presented. A test procedure for evaluating the performance of the ELA Test Facility is also included.


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    Title :

    Strategic Avionics Technology Definition Studies. Subtask 3-1A3: Electrical Actuation (ELA) Systems Test Facility


    Contributors:
    J. P. Rogers (author) / K. L. Cureton (author) / J. R. Olsen (author)

    Publication date :

    1994


    Size :

    53 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    Strategic avionics technology definition studies. Subtask 3-1A: Electrical Actuation (ELA) systems

    Pond, Charles L. / Mcdermott, William A. / Lum, Ben T. F. | NTRS | 1993


    Strategic avionics technology planning

    Cox, Kenneth J. / Brown, Don C. | NTRS | 1991