The paper demonstrates the advisability of studying characteristics of transient processes in every component of a new high-pulse dual-mode correction unit based on the stationary plasma thruster during its firing, steady-state operation in all main modes, and cutoff for the purpose of considering the influence of gas-discharge processes on performance of the high-pulse dual-mode correction unit components.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Specific Features of Transient Processes in Stationary Plasma Thrusters and a Device for Their Simulation


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:
    Akhmetzhanov, R. V. (Autor:in) / Bogatyi, A. V. (Autor:in) / Kim, V. (Autor:in) / Rudenko, E. V. (Autor:in) / Shilov, E. A. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 66 , 2 ; 293-307


    Erscheinungsdatum :

    01.04.2023


    Format / Umfang :

    15 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Computational Modeling of Stationary Plasma Thrusters

    Koo, Justin / Boyd, Iain | AIAA | 2003


    Computational Modeling of Stationary Plasma Thrusters

    Koo, J. W. / Boyd, I. D. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2003


    Electric propulsion system with stationary plasma thrusters

    LORAND ANTHONY CLAUDE BERNARD | Europäisches Patentamt | 2016

    Freier Zugriff