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小型感性耦合射频等离子体中和器的实验研究 被引量:9

Experimental Study of a Mini Inductively Coupled Radio-Frequency Plasma Neutralizer
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摘要 为了研究适用于百瓦级电推力器的离子束流中和技术,基于电子鞘层模型、射频等离子体最优放电技术和通过插入探针实现快速点火的方法,设计了一套小型感性耦合射频等离子体中和器(RF plasma neutralizer,RPN)。实验研究了RPN中和器的稳定工作条件和电子引出特性,实现了RPN中和器稳定工作和电子有效引出。实验结果表明:电子引出特性主要取决于发射孔附近阳极斑的形成与否,而阳极斑的形成又主要受结构设计、工质流量和偏置电压等运行条件的影响;通过对RPN运行条件的优化试验,获得了55~150m A可调电子束流范围和较高的工质利用系数(3.9~10.5),满足离子束流中和需求;另外,实验中还观察到了电子束流随工质流量或偏置电压的迟滞现象。 In order to study the ion beam neutralization technology which is applicable to the electric thruster at the level of 100 W,the mini inductively coupled radio-frequency plasma neutralizer(RPN)was developed.Electron sheath model and the optimal discharge techniques of RF plasma are used to design the neutralizer's structures and stable operating parameters,and the fast ignition is achieved by inserting a floating probe. Then,the electron-extraction characteristics of RPN neutralizer were studied experimentally. Thus,the RPN neutralizer achieve a better working stability and electron-extraction performances. The experimental results show that the electron-extraction performances mainly depend on the formation of anode-spot near the emission hole. However,the formation of anode-spot is mainly affected by the structural design,mass flow rates and bias voltage and other operating conditions. Through the optimization experiments of RPN neutralizer,the electron-extraction range of 55-150 m A and working gas utilization factor of 3.9-10.5 are obtained. This satisfies the requirements of design. In addition,the hysteresis of electron-extraction current is observed with the regulation of mass flow rate or bias voltage.
作者 贺建武 马隆飞 薛森文 章楚 段俐 康琦 HE Jian-wu;MA Long-fei;XUE Sen-wen;ZHANG Chu;DUAN Li;KANG Qi(National Micro Gravity Laboratory,Institute of Mechanics,CAS,Beijing 100190,China;School ofEngineeringSciences,University of Chinese Academy of Sciences,Beijing 100049,China)
出处 《推进技术》 EI CAS CSCD 北大核心 2018年第7期1673-1680,共8页 Journal of Propulsion Technology
基金 中国科学院战略性先导科技专项B类(XDB23030300) 中国科学院空间科学战略性先导科技专项(XDA04078600)
关键词 感性耦合等离子体 中和器 离子推力器 空心阴极 电子源 Inductively coupled plasma Neutralizer RF ion thruster Hollow cathode Electron source
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  • 1郭宁,顾佐,邱家稳.空心阴极在空间技术中的应用[J].真空,2005,42(5):32-35. 被引量:12
  • 2郭宁,邱家稳,顾佐,江豪成.20cm氙离子发动机空心阴极3000h寿命试验[J].真空与低温,2006,12(4):204-206. 被引量:14
  • 3Ismat M, Ahmed Rudwan. Emitter Depletion Measurement and Modeling in the T5&T6 Kaufman-Type Ion Thrusters[ R]. IEPC 2007-256. 被引量:1
  • 4Grubisicl A N,Gabriel S B. Preliminary Thrust Characte ization of a T5 Hollow Cathode[ R]. AIAA 2007-5194. 被引量:1
  • 5Hani Kamhawi, Michael J Patterson. Update on the Operational Status of the International Space Station Plasma Contactor Hollow Cathode Assemblies [ R ]. AIAA 2007-5190. 被引量:1
  • 6Herman Daniel A, Soulas George C, Patterson Michael J. Next Long-Duration Test After 11,570 h and 237 kg of Xenon Processed [ R ]. IEPC 2007-033. 被引量:1
  • 7James E Polk, Goebely Dan M. XIPS 25-cm ThrusterCathode Life Qualification for Use on Deep Space Missions[ R]. IEPC 2007-193. 被引量:1
  • 8Alex Mathers. Development of a High Power Cathode Heater[ R]. AIAA 2008-4815. 被引量:1
  • 9Yasushi Ohkawa, Yukio Hayakawa, Hideki Yoshida. Hollow Cathode Life Test for the Next-Generation Ion Engine in JAXA[ R]. IEPC 2007-89. 被引量:1
  • 10Yasushi Ohkawal, Yukio Hayakawa. Life Test of a Graphite-Orificed Hollow Cathode[ R]. AIAA 2008-4817. 被引量:1

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