This final report summarizes the research carried out on the development of numerical approaches for simulating the plumes of electric propulsion devices. In Appendix I, we describe the development of a particle based Monte Carlo approach for simulating the plumes and impingement of chemical propulsion systems, in Appendix II, we describe a plume model for an electric propulsion device (a Hall thruster). The research performed in this grant has led to significant advances in the capabilities for modeling these plume flows.


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    Titel :

    Modeling of an Arcjet Plume for Thin Film Synthesis


    Beteiligte:
    I. D. Boyd (Autor:in)

    Erscheinungsdatum :

    2000


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Fluctuation of Arcjet Plume Properties

    Pobst, J.A. | Online Contents | 1996


    Fluctuation of arcjet plume properties

    Pobst, Jeffrey A. / Spores, Ronald A. / Schilling, John H. et al. | AIAA | 1996


    Plume characteristics of an arcjet thruster

    LIEBESKIND, JOHN / HANSON, RONALD / CAPPELLI, MARK | AIAA | 1993


    Plume characteristics of an arcjet thruster

    Liebeskind, John G. / Hanson, Ronald K. / Cappelli, Mark A. | NTRS | 1993


    Ceramic thin film synthesis via arcjet CVD

    Berns, D / Kull, A / Cappelli, M | AIAA | 1995