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Simulation of the effect of a magnetically insulated anode on a low-power cylindrical Hall thruster 被引量:1
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作者 Yongjie DING Hong LI +7 位作者 Boyang JIA peng LI Liqiu WEI Yu XU wuji peng Hezhi SUN Yong CAO Daren YU 《Plasma Science and Technology》 SCIE EI CAS CSCD 2018年第3期156-162,共7页
The intersection point of the characteristic magnetic field line(CMFL) crossing the anode boundary with the discharge channel wall, and its influence on thruster performance and the energy and flux of ions bombardin... The intersection point of the characteristic magnetic field line(CMFL) crossing the anode boundary with the discharge channel wall, and its influence on thruster performance and the energy and flux of ions bombarding the channel wall, have been studied numerically. The simulation results demonstrate that with the increase in distance from the crossover point of the CMFL with the channel wall to the bottom of the thruster channel, the ionization rate in the discharge channel gradually increases; meanwhile, the ion energy and ion current density bombarding the channel wall decreases. When the point of the CMFL with the channel wall is at the channel outlet, the thrust, specific impulse, and efficiency are at a maximum, while the ion energy and ion current density bombarding the channel wall are at a minimum. Therefore, to improve the performance and lifetime of the thruster, it is important to control the point of intersection of the CMFL with the channel wall. 展开更多
关键词 magnetically insulated anode cylindrical Hall thruster PERFORMANCE
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