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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Modeling of an Arcjet Plume for Thin Film Synthesis


    Contributors:
    I. D. Boyd (author)

    Publication date :

    2000


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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


    Plume characteristics of an arcjet thruster

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


    Ceramic thin film synthesis via arcjet CVD

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