磁路对30cm离子推力器性能影响研究  

Study on Effects of Magnetic Circuit on Performance of 30cm Diameter Ion Thruster

作　　者：吴先明[1] 张天平[1] 陈娟娟[1] 龙建飞[1] 孙明明[1] 

机构地区：[1]兰州空间技术物理研究所真空技术与物理重点实验室,甘肃兰州730000

出　　处：《推进技术》2016年第1期193-200,共8页Journal of Propulsion Technology

基　　金：真空低温技术与物理重点实验室基金(9140c550206130c5503)

摘　　要：为了研究磁路结构对与新型GEO平台配套的30cm离子推力器(LIPS-300)性能的影响,采用PIC-MCC数值模拟方法对LIPS-300在其典型工作点下的放电损耗和束流平直度进行了研究,其中输入磁场采用有限元软件Maxwell计算得到,另外还利用Maxwell研究了磁体尺寸对侧壁磁环对产生的磁场等值线的影响。结果表明在LIPS-300的典型工作点下,4极场推力器比3极场推力器放电损耗高3%,分别是164W/A和160W/A,束流平直度高30%,分别为0.65和0.50。利用较厚较窄的磁环能够获得更大的无场区体积。因此,采用4极场将获得更好的推力器性能,采用较大厚度/宽度比的磁体有利于推力器束流平直度的改进。In order to study the effects of magnetic circuit on the performance of 30 cm diameter ion thruster（LIPS-300） which matches the new type of GEO satellite platform,PIC-MCC numerical simulation method was used to study LIPS-300＇s discharge loss and beam flatness under its typical operating point. The magnetic field input of PIC-MCC simulation was calculated using infinite element software Maxwell. It was also used to study the effects of different magnet sizes on the magnetic contour produced by side-wall magnet pair. The obtained results indicate that under LIPS-300＇s typical operating point,4 pole field thruster＇s discharge loss is higher than that of 3 pole field by 3%. They are 164W/A and 160W/A,respectively. The 4 pole field thruster＇s beam flatness is larger than that of 3 pole field thruster by 30%. They are 0.65 and 0.50,respectively. More field free volume can be obtained by utilization of thicker and narrower magnet. So,the thruster can achieve better performance by applying 4 pole magnetic field and moderately large thickness/width ratio of the magnet is beneficial to the improvement of the beam flatness.

关 键 词：离子推力器 磁路 PIC-MCC 放电损耗 束流平直度 

分 类 号：V439.4[航空宇航科学与技术—航空宇航推进理论与工程]