The invention belongs to the technical field of cosmic sailing, and relates to a satellite with an electrostatic electric propulsion system, the satellite comprises a body and one or more propulsion systems, at least one propulsion system adopts an inertial electrostatic confinement ion thruster, and the inertial electrostatic confinement ion thruster comprises an air supply device; the magnetic conductive device comprises an electromagnetic coil and a magnetic conductive spray pipe; the anode is a spherical shell; the whole body of the cathode is in a cage shape, and the cathode is provided with a first connector connected with the air supply device and a second connector connected with the magnetic conductive spray pipe; the cathode is contained in the anode, and the gas supply device is used for guiding gas located outside the anode into the cathode; and one part of the magnetic conductive spray pipe is positioned outside the anode. According to the invention, a brand-new ionization mode of inertial electrostatic constraint is adopted, and the attitude and orbit of the satellite can be adjusted.
本发明属于宇宙航行技术领域,涉及一种具有静电式电推进系统的卫星,包括:本体,一个或多个推进系统,其中至少一个所述推进系统采用惯性静电约束离子推力器,所述惯性静电约束离子推力器包括:供气装置;导磁装置,所述导磁装置包括电磁线圈和导磁喷管;阳极,所述阳极为球状的壳体;阴极,所述阴极的本体整体上呈笼状,且所述阴极上设置有与所述供气装置连接的第一接口以及与所述导磁喷管连接的第二接口;所述阴极容纳于所述阳极的内部,且所述供气装置用于将位于所述阳极外部的气体导入到所述阴极内部;所述导磁喷管的一部分位于所述阳极的外部。本发明采用惯性静电约束这种全新的电离方式,能够对卫星的姿态和轨道进行调整。
Satellite with electrostatic electric propulsion system
一种具有静电式电推进系统的卫星
2023-05-12
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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