PIC-DSMC Simulation of a Hall Thruster Plume with Charge Exchange Effects Using pdFOAM
To develop technologies for the stable operation of electric propulsion systems, the effects of charge exchange (CEX) on the exhaust plume of a Hall thruster were studied using the particle-in-cell direct simulation Monte Carlo (PIC-DSMC) method. For the numerical analysis, an OpenFOAM-based code, p...
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MDPI AG
2023-01-01
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Online Access: | https://www.mdpi.com/2226-4310/10/1/44 |
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author | Sang Hun Kang |
author_facet | Sang Hun Kang |
author_sort | Sang Hun Kang |
collection | DOAJ |
description | To develop technologies for the stable operation of electric propulsion systems, the effects of charge exchange (CEX) on the exhaust plume of a Hall thruster were studied using the particle-in-cell direct simulation Monte Carlo (PIC-DSMC) method. For the numerical analysis, an OpenFOAM-based code, pdFOAM, with a simple electron fluid model was employed. In an example problem using the D55 Hall thruster exhaust plume, the results showed good agreement with experimental measurements of the plasma potential. In the results, CEX effects enhanced Xe<sup>+</sup> particle scattering near the thruster exit. However, due to the increase in the plasma potential with CEX effects, fewer Xe<sup>2+</sup> particles were near the thruster exit with CEX effects than without CEX effects. |
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format | Article |
id | doaj.art-19625055d880487694787cde94f3646d |
institution | Directory Open Access Journal |
issn | 2226-4310 |
language | English |
last_indexed | 2024-03-09T11:48:10Z |
publishDate | 2023-01-01 |
publisher | MDPI AG |
record_format | Article |
series | Aerospace |
spelling | doaj.art-19625055d880487694787cde94f3646d2023-11-30T23:18:24ZengMDPI AGAerospace2226-43102023-01-011014410.3390/aerospace10010044PIC-DSMC Simulation of a Hall Thruster Plume with Charge Exchange Effects Using pdFOAMSang Hun Kang0Department of Mechanical and Aerospace Engineering, Konkuk University, Seoul 05029, Republic of KoreaTo develop technologies for the stable operation of electric propulsion systems, the effects of charge exchange (CEX) on the exhaust plume of a Hall thruster were studied using the particle-in-cell direct simulation Monte Carlo (PIC-DSMC) method. For the numerical analysis, an OpenFOAM-based code, pdFOAM, with a simple electron fluid model was employed. In an example problem using the D55 Hall thruster exhaust plume, the results showed good agreement with experimental measurements of the plasma potential. In the results, CEX effects enhanced Xe<sup>+</sup> particle scattering near the thruster exit. However, due to the increase in the plasma potential with CEX effects, fewer Xe<sup>2+</sup> particles were near the thruster exit with CEX effects than without CEX effects.https://www.mdpi.com/2226-4310/10/1/44Hall thrustersPIC-DSMCexhaust plumecharge exchange effects |
spellingShingle | Sang Hun Kang PIC-DSMC Simulation of a Hall Thruster Plume with Charge Exchange Effects Using pdFOAM Aerospace Hall thrusters PIC-DSMC exhaust plume charge exchange effects |
title | PIC-DSMC Simulation of a Hall Thruster Plume with Charge Exchange Effects Using pdFOAM |
title_full | PIC-DSMC Simulation of a Hall Thruster Plume with Charge Exchange Effects Using pdFOAM |
title_fullStr | PIC-DSMC Simulation of a Hall Thruster Plume with Charge Exchange Effects Using pdFOAM |
title_full_unstemmed | PIC-DSMC Simulation of a Hall Thruster Plume with Charge Exchange Effects Using pdFOAM |
title_short | PIC-DSMC Simulation of a Hall Thruster Plume with Charge Exchange Effects Using pdFOAM |
title_sort | pic dsmc simulation of a hall thruster plume with charge exchange effects using pdfoam |
topic | Hall thrusters PIC-DSMC exhaust plume charge exchange effects |
url | https://www.mdpi.com/2226-4310/10/1/44 |
work_keys_str_mv | AT sanghunkang picdsmcsimulationofahallthrusterplumewithchargeexchangeeffectsusingpdfoam |