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
  • [41] Ion-neutral phasing in Hall thruster breathing mode oscillations
    Konopliv, Mary F.
    Johnson, Lee K.
    Wirz, Richard E.
    Journal of Applied Physics, 1600, 136 (22):
  • [42] Neutral density map of Hall thruster plume expansion in a vacuum chamber
    Walker, MLR
    Gallimore, AD
    REVIEW OF SCIENTIFIC INSTRUMENTS, 2005, 76 (05):
  • [43] Study of the effect of neutral flow distribution on the performance of Hall micro thruster
    Lu, Shixu
    Zhu, Chunyuan
    Guo, Ning
    Dong, Liexiao
    Cong, Linxiao
    Wang, Jian
    Xu, Luxiang
    Wu, Mingshan
    Long, Jianfei
    VACUUM, 2025, 233
  • [44] Ion-neutral phasing in Hall thruster breathing mode oscillations
    Konopliv, Mary F.
    Johnson, Lee K.
    Wirz, Richard E.
    JOURNAL OF APPLIED PHYSICS, 2024, 136 (22)
  • [45] Status and prospect of Hall thruster of different thrust stages
    Liu Y.
    Zhang X.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2022, 37 (12): : 2782 - 2796
  • [46] Comparative analysis of simulation and experiment for the Hall-type thruster BPT-4000
    Porto, Marconi C.
    Martins, Alexandre A.
    Ferreira, Jose Leonardo
    Llanos, Carlos Humberto
    RESULTS IN ENGINEERING, 2023, 17
  • [47] Particle simulation of ion thruster plume characteristics
    Sun A.
    Mao G.
    Chen M.
    Xia G.
    Huo C.
    Qiangjiguang Yu Lizishu/High Power Laser and Particle Beams, 2010, 22 (02): : 401 - 405
  • [48] Influence of channel length on discharge performance of anode layer Hall thruster studied by particle-in-cell simulation
    曹希峰
    刘辉
    蒋文嘉
    宁中喜
    黎润
    于达仁
    Chinese Physics B, 2018, (08) : 372 - 377
  • [49] Influence of channel length on discharge performance of anode layer Hall thruster studied by particle-in-cell simulation
    Cao, Xi-Feng
    Liu, Hui
    Jiang, Wen-Jia
    Ning, Zhong-Xi
    Li, Run
    Yu, Da-Ren
    CHINESE PHYSICS B, 2018, 27 (08)
  • [50] Numerical analysis of Hall thruster firing tests
    Bober, Alexander
    JOURNAL OF PROPULSION AND POWER, 2007, 23 (03) : 537 - 543