This paper describes the results of a feasibility study for an Electric Propulsion Orbital Platform (EPOP), whose primary objective is to provide an instrumented platform for testing electric propulsion devices in space. It is anticipated that the first flight, EPO-1, will take place on the Shuttle-deployed Wake Shield Facility in 1996, and will be designed around a modified version of a commercial 1.8 kW hydrazine arcjet system, to be operated on gaseous hydrogen propellant. Specific subsystems are described, including the arcjet system, the propellant and power systems, and the diagnostics systems. Also, system engineering and integration issues are discussed.


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    Titel :

    EPOP - Toward the realization of an Electric Propulsion Orbital Platform


    Beteiligte:
    Friedly, V. J. (Autor:in) / Garrison, G. W. (Autor:in) / Ruyten, W. M. (Autor:in)

    Erscheinungsdatum :

    01.07.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    FRIEDLY, V. / GARRISON, G. / RUYTEN, W. | AIAA | 1992


    EPOP: The Electric Propulsion Orbital Platform

    Friedly, V. J. / Ruyten, W. M. | NTRS | 1995


    Electric Propulsion Orbital Platform

    Friedly, V. J. / Ruyten, Wilhelmus M. / Litchford, R. J. et al. | NTRS | 1993



    Diagnostics development for the Electric Propulsion Orbital Platform

    Ruyten, Wilhelmus M. / Friedly, V. J. / Litchford, R. J. | NTRS | 1993