journal article·2021-12-01Open access

Gas inlet impact on neutral density and recycle pattern with a disk shaped antenna in a miniature ion thruster through particle simulation

Ali Yousefian

AIP Advances· Volume 11· Issue 12

Abstract

The gas inlet configuration has a direct impact on the neutral density pattern within a miniature ion thruster. We aimed to investigate the impact the gas inlet configuration and neutral density pattern will have on the neutral recycle rate within a miniature ion thruster utilizing a disk shaped antenna. Four inlet configurations were considered for this study, and 3D electromagnetic particle-in-cell simulation was utilized to simulate the plasma inside the discharge chamber. The simulation results indicate a clear shift in neutral density toward the inlet, with the single horizontal inlet configuration having a 45% increase in neutral density in the vicinity of the inlet walls. The neutral recycle rate also experienced a clear shift toward the inlet walls, with the single bottom inlet configuration experiencing a 23% increase in the rate of ion loss near the inlet wall and a similar 22% increase for the single horizontal inlet while the four smaller inlets had a similar rate of neutral recycling throughout. These results are a novelty in this field as they clearly indicate the impact gas inlet and neutral density have on the miniature ion thruster’s performance and open a new area of research to further optimize the gas inlet configuration for miniature ion thrusters.
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Research context

OpenAlex topics: Plasma Diagnostics and Applications · Particle accelerators and beam dynamics · Electrostatic Discharge in Electronics

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Department of Advanced Energy Engineering Sciences, Kyushu University , Fukuoka, Japan

References (30)

Show source-provided references
1. 1968 · 2
2. Development of small microwave discharge ion thruster10.1016/j.tsf.2005.08.045 ↗
3. J. Propul. Power · 1998 · 14 · 70810.2514/2.5333 ↗
4. Antenna configuration effects on thrust performance of miniature microwave discharge ion engine
5. Vacuum · 2004 · 73 · 44910.1016/j.vacuum.2003.12.066 ↗
6. Trans. Jpn. Soc. Aeronaut. Space Sci. · 2010 · 8 · 5510.2322/tastj.8.pb_55 ↗
7. Three-dimensional particle in cell simulation of miniature plasma source for a microwave discharge ion thruster10.1088/0963-0252/23/6/064004 ↗
8. Two-dimensional numerical model of plasma flow in a Hall thruster10.2514/3.23974 ↗
9. A numerical study of low-frequency oscillations in simulation of electric propulsion thrusters Hall thrusters
10. Two-dimensional model of a stationary plasma thruster10.1063/1.1465125 ↗
11. Model study of the influence of the magnetic field configuration on the performance and lifetime of a Hall thruster10.1063/1.1622670 ↗
12. Critical assessment of a two-dimensional hybrid Hall thruster model: Comparisons with experiments10.1063/1.1719022 ↗
13. Modeling of double stage Hall effect thruster10.1109/tps.2005.845117 ↗
14. Computational model tracking primary electrons, secondary electrons and ions in the discharge chamber of an ion engine
15. Computational study of primary electron confinement by magnetic fields in the discharge chamber of an ion engine10.2514/1.18366 ↗
16. Dynamic electric field calculations using a fully kinetic ion thruster discharge chamber model
17. Ion thruster discharge chamber simulation in three dimensions
18. Discharge chamber primary electron modeling activities in 3-dimensions
19. Low frequency oscillations in a stationary plasma thruster10.1063/1.368529 ↗
20. Neutral density and recycle analysis in a miniature neutralizer utilizing particle in cell simulation with respect to inlet configuration
21. A Monte Carlo collision model for the particle-in-cell method: Applications to argon and oxygen discharges10.1016/0010-4655(94)00171-w ↗
22. 1996
23. M. Tsuru, “Performance optimization of miniature microwave discharge neutralizer,” M.S. thesis, Kyushu University, Fukuoka, Japan, 2008 (in Japanese).
24. K. Sugita, “Microwave frequency dependence of small microwave discharge type ion thruster,” M.S. thesis, Kyushu University, Fukuoka, Japan, 2011 (in Japanese).
25. Measurements of electron density and temperature in a miniature microwave discharge ion thruster using laser Thomson scattering technique10.1088/0963-0252/19/4/045009 ↗
26. Neutral density measurement of ion thruster with differential pressure gauge10.2322/tastj.12.pb_73 ↗
27. 2002 · 40
28. Numerical analysis of the electromagnetic fields in a microwave plasma source excited by azimuthally surface waves10.1143/jjap.41.2199 ↗
29. H. Masui, “Numerical analysis of microwave discharge type plasma propulsion plasma source,” Ph.D. thesis, Kyushu University, Fukuoka, Japan, 2005 (in Japanese).
30. K. Ushio, “Study on microwave discharge type small plasma thruster,” Ph.D. thesis, Kyushu University, Fukuoka, Japan, 2018 (in Japanese).