Abstract The paper presents the research results of the effect of a capacitor energy storage device configuration on the specific characteristics of advanced modern propulsion systems based on the ablative pulsed plasma thrusters (APPT). These thrusters are designed to perform specific tasks within the small spacecrafts with the onboard power capacity up to 200 W.


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    Titel :

    Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems


    Beteiligte:
    Bogatyi, A. V. (Autor:in) / El’nikov, R. V. (Autor:in) / Nazarenko, I. P. (Autor:in) / Popov, G. A. (Autor:in) / Semenikhin, S. A. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 61 , 3 ; 445-451


    Erscheinungsdatum :

    2018-07-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems

    Bogatyi, A. V. / El’nikov, R. V. / Nazarenko, I. P. et al. | Online Contents | 2018



    Pulsed Plasma Thrusters for Small Spacecraft Attitude Control

    McGuire, M. / Myers, R. / Goddard Space Flight Center | British Library Conference Proceedings | 1996