Practical analysis of different neutral algorithms for particle simulation of Hall thruster

被引:8
|
作者
Pan, Ruojian [1 ]
Ren, Junxue [2 ]
Mao, Renfan [1 ]
Tang, Haibin [2 ,3 ,4 ]
机构
[1] Beihang Univ, Sch Space & Environm, Beijing 100083, Peoples R China
[2] Beihang Univ, Sch Astronaut, Beijing 100083, Peoples R China
[3] Minist Educ, Key Lab Spacecraft Design Optimizat & Dynam Simula, Beijing 100083, Peoples R China
[4] Minist Ind & Informat Technol, Lab Space Environm Monitoring & Informat Proc, Beijing 100083, Peoples R China
来源
PLASMA SOURCES SCIENCE & TECHNOLOGY | 2023年 / 32卷 / 03期
关键词
Hall thruster; full-particle simulation; neutral iterations; low-frequency oscillation; quasi-steady-state algorithm; MODEL; OSCILLATIONS;
D O I
10.1088/1361-6595/acc134
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
The modeling of neutral atoms is important for the full-particle simulations of Hall thrusters. In previous studies, researchers have developed various algorithms to model the neutral kinetics. The choice of those algorithms can influence significantly the computational speed, simulation convergence, and physical results. In this work, we perform a full-particle simulation of a typical 1 kW-class SPT-100 Hall thruster using four neutral algorithms, including the fixed-neutral algorithm (FNA), the algorithm of direct simulation of Monte Carlo (DSMC), the collisionless-neutral algorithm (CLNA), and the fluid algorithm (FA), to analyze the effects of different neutral iteration approaches on the simulation results. We found that FNA is sensitive to the initial number density of neutrals, and is difficult to converge properly, while the other algorithms not neglecting the atomic dynamics can get stable results. We count the parameters of the thruster, that is, thrust, specific impulse, and plasma density using different neutral algorithms. The time-averaged results match well with those of the experiment. However, the results differ in the time scale due to the low-frequency oscillations in Hall thrusters. We verify that the oscillations are due to the periodic change of neutrals and establish a zero-dimensional model to analyze the properties of the oscillations in the time scale. It indicates that the ratio of ion migration to neutral migration is the essential factor that significantly affects the calculation results. The model reveals that the direct neutral iteration methods, like DSMC and CLNA, can better simulate the characteristics of discharge fluctuations in Hall thrusters than the quasi-steady-state method, like FA. Finally, we proposed practical suggestions for the selection of the neutral algorithms for the SPT-100 thruster, which can also be generalized to other low- and medium-power Hall thrusters.
引用
收藏
页数:14
相关论文
共 50 条
  • [21] Geometrical scaling of Hall thruster particle model
    Taccogna, F
    Longo, S
    Capitelli, M
    Schneider, R
    Rarefied Gas Dynamics, 2005, 762 : 1119 - 1124
  • [22] Research of influence of the additional electrode on Hall thruster plume by particle-in-cell simulation*
    Cao, Xi-Feng
    Liu, Hui
    Yu, Da-Ren
    CHINESE PHYSICS B, 2020, 29 (09)
  • [23] Performance Simulation of a 5 kW hall Thruster
    Yang, L.
    Wang, P. Y.
    Wang, T.
    FRONTIERS IN MATERIALS, 2021, 8
  • [24] Particle-in-cell simulation for effect of anode temperature on discharge characteristics of a Hall effect thruster
    Li, Hong
    Liu, Xingyu
    Gao, Zhiyong
    Ding, Yongjie
    Wei, Liqiu
    Yu, Daren
    Wang, Xiaogang
    PLASMA SCIENCE & TECHNOLOGY, 2018, 20 (12)
  • [25] Particle-in-cell simulation for effect of anode temperature on discharge characteristics of a Hall effect thruster
    李鸿
    刘星宇
    高志勇
    丁永杰
    魏立秋
    于达仁
    王晓钢
    Plasma Science and Technology, 2018, (12) : 100 - 110
  • [26] Particle-in-cell simulation for the effect of magnetic cusp on discharge characteristics in a cylindrical Hall thruster
    Liang, Sheng-Tao
    Liu, Hui
    Yu, Da-Ren
    CHINESE PHYSICS B, 2018, 27 (04)
  • [27] Particle simulation of an anode-layer Hall thruster plume using an anisotropic scattering model
    Wang, Jiahong
    Chen, Laiwen
    Jiang, Yazhong
    Lee, Chun-Hian
    ACTA ASTRONAUTICA, 2020, 175 : 19 - 31
  • [28] Particle-in-cell simulation for effect of anode temperature on discharge characteristics of a Hall effect thruster
    李鸿
    刘星宇
    高志勇
    丁永杰
    魏立秋
    于达仁
    王晓钢
    Plasma Science and Technology, 2018, 20 (12) : 100 - 110
  • [29] Particle-in-Cell Simulation on Effects of Magnetic Field on Discharge Characteristics and Performance of Hall Thruster
    Duan, Ping
    Song, Ji-Lei
    Jiang, Bo-Rui
    Chen, Long
    Li, Wen-Qing
    Hu, Xiang
    Liu, Guang-Rui
    Tuijin Jishu/Journal of Propulsion Technology, 2020, 41 (01): : 194 - 204
  • [30] Study of electron transport in a Hall thruster by axial-radial fully kinetic particle simulation
    Cho, Shinatora
    Watanabe, Hiroki
    Kubota, Kenichi
    Iihara, Shigeyasu
    Fuchigami, Kenji
    Uematsu, Kazuo
    Funaki, Ikkoh
    PHYSICS OF PLASMAS, 2015, 22 (10)