A general methodology is presented which allows prediction of the overall characteristics of thrust systems employing electron-bombardment ion thrusters. Elements of the thrust system are defined and their characteristics presented in a parametric fashion. Two system approaches are evaluated where power management and control elements and thruster characteristics were substantially different. For an assumed system approach, the methodology presented predicts overall system properties, such as input power and mass, when major mission and thrust system parameters, such as trip time and specific impulse, are assumed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Primary electric propulsion for future space missions


    Contributors:
    Byers, D. C. (author) / Terdan, F. F. (author) / Myers, I. T. (author)

    Conference:

    Conf. on Adv. Technol. for Future Space Systems ; 1979 ; Langley, VA, United States


    Publication date :

    1979-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Primary electric propulsion for future space missions

    BYERS, D. / TERDAN, F. / MYERS, I. | AIAA | 1979



    Power supplies for primary electric propulsion missions

    Jones, R. M. / Scott-Monck, J. A. | NTRS | 1985


    Power supplies for primary electric propulsion missions

    JONES, R. M. / SCOTT-MONCK, J. A. | AIAA | 1985


    Solar Electric Propulsion for Future NASA Missions

    Landis, Geoffrey A. / Oleson, Steven R. / Mercer, Carolyn R. | NTRS | 2015