In this article problem of low-power SPT development actualite is considered. The main requirements for this thruster class are represented. Some methods of low-power Hall thruster developing and their advantages and disadvantage. The test results and main parameters of new law-power thruster laboratory model SPT-20M are represented. Comparative characteristics of SPT model and law power hollow thrusters developed by leading world specialists is shown.


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    Titel :

    The low power hollow thruster for orbit correction system for small, mini and micro satellites


    Beteiligte:
    Maksymenko, T.A. (Autor:in) / Loyan, A.V. (Autor:in) / Koshelev, N.N. (Autor:in)


    Erscheinungsdatum :

    01.01.2005


    Format / Umfang :

    565082 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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