The invention discloses a long-service-life microwave cusped field plasma thruster applying a magnetic shielding technology, relates to a thruster, and provides a design scheme of the long-service-life microwave cusped field plasma thruster aiming at the service life requirement of tens of thousands of hours generally required by current spacecrafts on micro propelling devices. The device comprises a plurality of permanent magnets, an aluminum oxide ceramic channel, a microwave coaxial resonator and a shell, the aluminum oxide ceramic channel is located at the left end in the shell, the microwave coaxial resonator is installed in the shell and located on the right side of the aluminum oxide ceramic channel, and the aluminum oxide ceramic channel is sleeved with the permanent magnets. On the basis of keeping the high performance of the design scheme of the thruster, by introducing the magnetic shielding technology, the degradation process of the thruster is effectively delayed, the service life of the microwave cusped field plasma thruster is greatly prolonged, and the applicability of the microwave cusped field plasma thruster to a space gravitational wave detection task scene is remarkably improved. The invention belongs to the technical field of spaceflight.

    一种应用磁屏蔽技术的长寿命微波会切场等离子体推力器,涉及一种推力器,本发明为了针对目前航天器对微型推进装置普遍要求的上万小时的寿命需要,提出一种长寿命微波会切场等离子体推力器的设计方案,本发明包括多个永磁铁、氧化铝陶瓷通道、微波同轴谐振器、外壳,所述氧化铝陶瓷通道位于外壳内的左端,微波同轴谐振器安装在外壳内并位于氧化铝陶瓷通道的右侧,多个永磁铁套装在氧化铝陶瓷通道的外则。本发明在保持了此前推力器设计方案具备的高性能的基础上,通过引入磁屏蔽技术,有效延缓了推力器的退化进程,极大的延长了微波会切场等离子体推力器的运行寿命,显著提高了其对“空间引力波探测”任务场景的适用性。本发明属于航天技术领域。


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    Title :

    Long-life microwave cusped field plasma thruster applying magnetic shielding technology


    Additional title:

    一种应用磁屏蔽技术的长寿命微波会切场等离子体推力器


    Contributors:
    LIU HUI (author) / WANG SHANGSHENG (author) / ZENG MING (author) / YU DAREN (author)

    Publication date :

    2024-08-09


    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



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