The design, fabrication, and testing of thrust vectorable ion optical systems capable of controlling the thrust direction from both 5- and 30-cm diameter ion thrusters is described. Both systems are capable of greater than 10 deg thrust deflection in any azimuthal direction. The 5-cm system is electrostatic and hence has a short response time and minimal power consumption. It has recently been tested for more than 7500 hours on an operational thruster. The 30-cm system is mechanical, has a response time of the order of 1 min, and consumes less than 0.3% of the total system input power at full deflection angle.


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    Titel :

    Thrust vectoring systems


    Beteiligte:
    King, H. J. (Autor:in) / Schnelker, D. (Autor:in) / Ward, J. W. (Autor:in) / Dulgeroff, C. (Autor:in) / Vahrenkamp, R. (Autor:in)

    Erscheinungsdatum :

    1972-12-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Thrust vectoring systems

    KING, H. / SCHNELKER, D. | AIAA | 1970


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