A micro-cathode arc propulsion system. By replacing an inductive circuit in a traditional micro-cathode arc propulsion system with a capacitor circuit, the stability of the operation of a micro-cathode arc thruster can be improved due to the stable discharging mode of the capacitor, and as the internal resistance of the capacitor is small during operation, the additional power consumption of the circuit is reduced, and the efficiency of the system is improved. In addition, as a pulse power supply is used to power in a pulse manner, the average power inputted into the micro-cathode arc thruster is greatly reduced.


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    Titel :

    MICRO-CATHODE ARC PROPULSION SYSTEM


    Beteiligte:
    WEI LIQIU (Autor:in) / DING YONGJIE (Autor:in) / LI HONG (Autor:in) / HAN LIANG (Autor:in) / YU DAREN (Autor:in)

    Erscheinungsdatum :

    2023-08-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H05H Plasmatechnik , PLASMA TECHNIQUE



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