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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    Title :

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


    Contributors:


    Publication date :

    2005-01-01


    Size :

    565082 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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