The invention relates to a field coil (18, 20), in particular for a satellite Hall effect plasma thruster, said field coil (18, 20) comprising a core (22) on which a conductor (24) is wound, characterized in that the conductor comprises an inorganic insulated cable (26) impregnated with a high temperature resistant silicone coating (32).

    本发明涉及一种场线圈(18,20),特别是用于卫星霍尔效应等离子体推进器的场线圈,所述场线圈(18,20)包括核(22),导体(24)卷绕在核上,其特征在于,导体包括浸渍有耐高温硅酮涂层(32)的无机绝缘电缆(26)。


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    Title :

    Field coil for steady-state plasma thruster


    Additional title:

    用于稳态等离子体推进器的场线圈



    Publication date :

    2022-12-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen / B64G Raumfahrt , COSMONAUTICS / H01B CABLES , Kabel / H01F MAGNETS , Magnete





    Optimal Quasi-Steady Plasma Thruster System Characteristics

    DENNIS E. LUDWIG AND ARNOLD J. KELLY | AIAA | 1973



    Optimal Quasi-steady Plasma Thruster system characteristics.

    Ludwig, D. E. / Kelly, A. J. | NTRS | 1972