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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Main Author: Sang Hun Kang
Format: Article
Language:English
Published: MDPI AG 2023-01-01
Series:Aerospace
Subjects:
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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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