Numerical study on the electron-wall interaction in a Hall thruster with segmented electrodes placed at the channel exit  

作　　者：卿绍伟 鄂鹏 段萍 徐殿国 

机构地区：[1]Power Engineering Institute, Chongqing University [2]Department of Electrical Engineering, Harbin Institute of Technology [3]School of Physics, Dalian Maritime University

出　　处：《Chinese Physics B》2013年第8期523-528,共6页中国物理B（英文版）

基　　金：supported by the Fundamental Research Funds for the Central Universities,China(Grant No.0903005203189);the National Natural Science Foundation of China(Grant Nos.11005025,10975026,and 11275034);the Scientific Research Innovation Foundation of Harbin Institution of Technology,China(GrantNo.HITNSRIF2009044);the Key Project of the Scientific Technology Program of Liaoning Province,China(Grant No.2011224007)

摘　　要：Electron-wall interaction is always recognized as an important physical problem because of its remarkable influences on thruster discharge and performance. Based on existing theories, an electrode is predicted to weaken electron-wall interaction due to its low secondary electron emission characteristic. In this paper, the electron-wall interaction in an Aton-type Hall thruster with low-emissive electrodes placed near the exit of discharge channel is studied by a fully kinetic particle-in cell method. The results show that the electron-wall interaction in the region of segmented electrode is indeed weakened, but it is significantly enhanced in the remaining region of discharge channel. It is mainly caused by electrode conductive property which makes equipotential lines convex toward channel exit and even parallel to wall surface in near-wall re- gion; this convex equipotential configuration results in significant physical effects such as repelling electrons, which causes the electrons to move toward the channel center, and the electrons emitted from electrodes to be remarkably accelerated, thereby increasing electron temperature in the discharge channel, etc. Furthermore, the results also indicate that the discharge current in the segmented electrode case is larger than in the non-segmented electrode case, which is qualitatively in accordance with previous experimental results.Electron-wall interaction is always recognized as an important physical problem because of its remarkable influences on thruster discharge and performance. Based on existing theories, an electrode is predicted to weaken electron-wall interaction due to its low secondary electron emission characteristic. In this paper, the electron-wall interaction in an Aton-type Hall thruster with low-emissive electrodes placed near the exit of discharge channel is studied by a fully kinetic particle-in cell method. The results show that the electron-wall interaction in the region of segmented electrode is indeed weakened, but it is significantly enhanced in the remaining region of discharge channel. It is mainly caused by electrode conductive property which makes equipotential lines convex toward channel exit and even parallel to wall surface in near-wall re- gion; this convex equipotential configuration results in significant physical effects such as repelling electrons, which causes the electrons to move toward the channel center, and the electrons emitted from electrodes to be remarkably accelerated, thereby increasing electron temperature in the discharge channel, etc. Furthermore, the results also indicate that the discharge current in the segmented electrode case is larger than in the non-segmented electrode case, which is qualitatively in accordance with previous experimental results.

关 键 词：Hall thruster electron-wall interaction segmented electrodes particle simulation 

分 类 号：TM910.3[电气工程—电力电子与电力传动]