The successful development of multimegawatt MPD thrusters depends, to a great extent, on testing them under steady state high altitude space conditions. Steady state testing is required to provide thermal characteristics, life cycle, erosion, and other essential data. the major technical obstacle for ground testing of MPD thrusters in a space simulation facility is the inability of state-of-the-art vacuum systems to handle the tremendous pumping speeds required for multimegawatt MPD thrusters. This is true for other types of electric propulsion devices as well. This paper discusses the results of the first phase of an evaluation of steady state MPD thruster test facilities. The first phase addresses the conceptual design of vacuum systems required to support multimegawatt MPD thruster testing. Three advanced pumping system concepts were evaluated and are presented here. (ERA citation 11:020618)


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    Titel :

    Evaluation of a Steady State MPD Thruster Test Facility


    Beteiligte:
    C. B. Reed (Autor:in) / L. W. Carlson (Autor:in) / H. Herman (Autor:in) / E. D. Doss (Autor:in) / O. Kilgore (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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