Optimization of a Long-Lifetime Hall Thruster with an Internally Mounted Cathode

被引:15
|
作者
Zeng, Demai [1 ,2 ]
Li, Hong [1 ,2 ]
Liu, Jinwen [4 ]
Hu, Yanlin [3 ]
Ding, Yongjie [1 ,2 ]
Wei, Liqiu [1 ,2 ]
Yu, Daren [1 ,2 ]
机构
[1] Harbin Inst Technol, Plasma Prop Lab, Harbin 150001, Peoples R China
[2] Harbin Inst Technol, Minist Ind & Informat Technol, Key Lab Aerosp Plasma Prop, Harbin 150001, Peoples R China
[3] Beijing Inst Control Engn, Beijing 100190, Peoples R China
[4] Qingdao Haier Smart Technol, Qingdao 266100, Peoples R China
基金
中国国家自然科学基金;
关键词
Space Propulsion; Electric Propulsion; Hall Thruster; Magnetic Field Configurations; Plasma Propulsion; Hollow Cathodes; Plasma Thrusters; ELECTRIC PROPULSION; POSITION;
D O I
10.2514/1.J062246
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Hall thrusters with an internal cathode are widely used due to their ability to enhance efficiency, minimize plume divergence, and eliminate plume asymmetry. In addition, the long-lifetime technology of Hall thrusters typically relocates the intense magnetic-field region outside the channel, known as an "aft-loaded magnetic field," to mitigate erosion of the discharge channel caused by high-energy ions. However, this exacerbates plume divergence and diminishes overall performance. Therefore, this research focuses on optimizing a Hall thruster with an aft-loaded magnetic field and internal cathode. Given that electrons emitted by the internal cathode initially diffuse onto the magnetic separatrix and subsequently couple with the ion beam in the plume, this study experimentally investigates the impact of the magnetic separatrix shape on the discharge characteristics and plume behavior of the Hall thruster. The experimental findings indicate that expanding the envelope of the magnetic separatrix contributes to improved plume focusing and enhanced performance. Thus, the results of this study highlight the significance of the magnetic field outside the channel as a crucial design factor for long-lifetime Hall thrusters.
引用
收藏
页码:4259 / 4266
页数:8
相关论文
共 50 条
  • [31] Long-lifetime coherence in a quantum emitter induced by a metasurface
    Lassalle, Emmanuel
    Lalanne, Philippe
    Aljunid, Syed
    Genevet, Patrice
    Stout, Brian
    Durt, Thomas
    Wilkowski, David
    PHYSICAL REVIEW A, 2020, 101 (01)
  • [32] Design of long-lifetime lunar orbits: A hybrid approach
    Lara, Martin
    ACTA ASTRONAUTICA, 2011, 69 (3-4) : 186 - 199
  • [33] Long-lifetime metal-ligand pH probe
    Murtaza, Z
    Chang, Q
    Rao, GV
    Lin, H
    Lakowicz, JR
    ANALYTICAL BIOCHEMISTRY, 1997, 247 (02) : 216 - 222
  • [34] Optimization of a wall-less Hall thruster
    Vaudolon, Julien
    Mazouffre, Stephane
    Henaux, Carole
    Harribey, Dominique
    Rossi, Alberto
    APPLIED PHYSICS LETTERS, 2015, 107 (17)
  • [35] Ion Optics Lifetime Optimization for Ion Thruster
    Zhang X.-E.
    Zhang T.-P.
    Li D.-T.
    Meng W.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (09):
  • [36] Long-lifetime lunar repeat ground track orbits
    Russell, Ryan P.
    Lara, Martin
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (04) : 982 - 993
  • [37] Effects of cathode configuration on Hall thruster cluster plume properties
    Beal, Brian E.
    Gallimore, Alec D.
    Hargus, William A., Jr.
    JOURNAL OF PROPULSION AND POWER, 2007, 23 (04) : 836 - 844
  • [38] LONG-LIFETIME HIGH-INTENSITY GAAS PHOTOSOURCE
    CALABRESE, R
    CIULLO, G
    GUIDI, V
    LAMANNA, G
    LENISA, P
    MACIGSI, B
    TECCHIO, L
    YANG, B
    REVIEW OF SCIENTIFIC INSTRUMENTS, 1994, 65 (02): : 343 - 348
  • [39] A Long-Lifetime Sensor Platform for a Reliable Internet of Things
    Jackson, Neal
    Adkins, Joshua
    Dutta, Prabal
    IPSN '19: PROCEEDINGS OF THE 2019 INTERNATIONAL CONFERENCE ON INFORMATION PROCESSING IN SENSOR NETWORKS, 2019, : 331 - 332
  • [40] Comparison of Discharge Characteristics of a Hall Thruster with Different Cathode Arrangements
    Zeng, Demai
    Li, Hong
    Liu, Jinwen
    Ding, Yongjie
    Wei, Liqiu
    Yu, Daren
    Hu, Yanlin
    JOURNAL OF PROPULSION AND POWER, 2022, 38 (04) : 686 - 689