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)。
Field coil for steady-state plasma thruster
用于稳态等离子体推进器的场线圈
2022-12-02
Patent
Electronic Resource
Chinese