WANG Jian1,WANG You-mei1,LIU Zhong-mao1. Study on Optimization of Magnetic Field in Magnetic Shielding of Hall Thruster[J]. Journal of Propulsion Technology, 2020, 41(3): 715-720.
[1] Levchenko I,Xu S,Teel G,et al.Recent Progress and Perspectives of Space Electric Propulsion Systems Based on Smart Nanomaterials[J].Nature Communications,2018,9(1).
[2] Mazouffre S.Electric Propulsion for Satellites and Spacecraft: Established Technologies and Novel Approaches[J].Plasma Sources Science and Technology,2016,25(3).
[3] Ahedo E.Plasmas for Space Propulsion[J].Plasma Physics and Controlled Fusion,2011,53(12).
[4] 毛根旺,韩先伟,杨 涓,等.电推进研究的技术状态和发展前景[J].推进技术,2000,21(5):1-5.
[5] Ding Y,Sun H,Wei L,et al.A 200W Hall Thruster with Hollow Indented Anode[J].Acta Astronautica,2017,139:521-527.
[6] Sydorenko D,Smolyakov A,Kaganovich I,et al.Modification of Electron Velocity Distribution in Bounded Plasmas by Secondary Electron Emission[J].IEEE Transactions on Plasma Science,2006,34(3):815-824.
[7] Sydorenko D,Smolyakov A,Kaganovich I,et al.Plasma-Sheath Instability in Hall Thrusters Due to Periodic Modulation of the Energy of Secondary Electrons in Cyclotron Motion[J].Physics of Plasmas,2008,15(5).
[8] 于达仁,张凤奎,李 鸿,等.霍尔推进器中振荡鞘层对电子与壁面碰撞频率的影响研究[J].物理学报,2009,58(3):1844-1848.
[9] 段 萍,覃海娟,周新维,等.霍尔推进器壁面材料二次电子发射及鞘层特性[J].物理学报,2014,63(8):288-294.
[10] 边兴宇.霍尔推力器放电通道壁面分割及磁屏蔽效应研究[D].大连:大连海事大学,2018.
[11] Kamhawi H,Haag T,Jacobson D,et al.Performance Evaluation of the NASA-300M 20kW Hall Thruster[R].AIAA2011-5521.
[12] Mikellides I G,Katz I,Hofer R R,et al.Magnetic Shielding of a Laboratory Hall Thruster. I. Theory and Validation[J].Journal of Applied Physics,2014,115(4).
[13] 张志远,严 立,王平阳,等.霍尔推力器放电室壁面溅射产额研究[J].推进技术,2015,36(3):476-480.
[14] Yu D R,Zhang F K,Liu H,et al.Effect of Electron Temperature on Dynamic Characteristics of Two-Dimensional Sheath in Hall Thrusters[J].Physics of Plasma,2008,15(10).
[15] 丁永杰,扈延林,颜世林,等.聚焦磁场及发散磁场对霍尔推力器壁面侵蚀的影响研究[J].推进技术,2015,36(5):795-800.
[16] Wang Y M,Xu S,Levchenko I,et al.Approach to Simplified Numerical Optimization of Low-Power Hall Thrusters[J].Vacuum,2018,152:173-183.
[17] Ahedo E,Martínez-Sánchez M,Martínez-Sánchez M.One-Dimensional Model of the Plasma Flow in a Hall Thruster[J].Physics of Plasmas,2001,8(6):3058-3068.
[18] Baltzis K B.The FEMM Package: A Simple, Fast, and Accurate Open Source Electromagnetic Tool in Science and Engineering[J].Journal of Engineering Science and Technology Review,2008,1:83-89.