2D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge Regions

Many hybrid simulations of Hall thrusters, where electrons and ions are solved using hydrodynamics and particle-in-cell methods, respectively, assume that the ionized gas is quasi-neutral everywhere in the computational domain and apply so-called thin-sheath approximations to account for space-charg...

Full description

Bibliographic Details
Main Authors: Alejandro Lopez Ortega, Ioannis G. Mikellides
Format: Article
Language:English
Published: MDPI AG 2023-09-01
Series:Plasma
Subjects:
Online Access:https://www.mdpi.com/2571-6182/6/3/38
_version_ 1797577778262966272
author Alejandro Lopez Ortega
Ioannis G. Mikellides
author_facet Alejandro Lopez Ortega
Ioannis G. Mikellides
author_sort Alejandro Lopez Ortega
collection DOAJ
description Many hybrid simulations of Hall thrusters, where electrons and ions are solved using hydrodynamics and particle-in-cell methods, respectively, assume that the ionized gas is quasi-neutral everywhere in the computational domain and apply so-called thin-sheath approximations to account for space-charge effects near solid boundaries. These approximations do not hold along boundaries near the exit of the thruster or in the near plume regions, where the plasma conditions can lead to Debye lengths on the order of or higher than the local grid resolution. We present a numerical scheme that fully resolves the conditions of the ionized gas in space-charge regions of any thickness and that is coupled consistently to a global hybrid simulation of Hall thrusters. We verify the numerical results with the closed-form solution for a Langmuir sheath in a simplified one-dimensional example, and then again in simulations where the model is integrated in a 2D multifluid/PIC axial–radial code called Hall2De. The new capability to resolve numerically large sheaths around solid boundaries in Hall thrusters allows for significantly more accurate assessments of ion sputtering, thus improving thruster lifetime predictions.
first_indexed 2024-03-10T22:12:49Z
format Article
id doaj.art-deb306ae1e78431b87361c9d6e0a97a7
institution Directory Open Access Journal
issn 2571-6182
language English
last_indexed 2024-03-10T22:12:49Z
publishDate 2023-09-01
publisher MDPI AG
record_format Article
series Plasma
spelling doaj.art-deb306ae1e78431b87361c9d6e0a97a72023-11-19T12:33:44ZengMDPI AGPlasma2571-61822023-09-016355056210.3390/plasma60300382D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge RegionsAlejandro Lopez Ortega0Ioannis G. Mikellides1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USAJet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USAMany hybrid simulations of Hall thrusters, where electrons and ions are solved using hydrodynamics and particle-in-cell methods, respectively, assume that the ionized gas is quasi-neutral everywhere in the computational domain and apply so-called thin-sheath approximations to account for space-charge effects near solid boundaries. These approximations do not hold along boundaries near the exit of the thruster or in the near plume regions, where the plasma conditions can lead to Debye lengths on the order of or higher than the local grid resolution. We present a numerical scheme that fully resolves the conditions of the ionized gas in space-charge regions of any thickness and that is coupled consistently to a global hybrid simulation of Hall thrusters. We verify the numerical results with the closed-form solution for a Langmuir sheath in a simplified one-dimensional example, and then again in simulations where the model is integrated in a 2D multifluid/PIC axial–radial code called Hall2De. The new capability to resolve numerically large sheaths around solid boundaries in Hall thrusters allows for significantly more accurate assessments of ion sputtering, thus improving thruster lifetime predictions.https://www.mdpi.com/2571-6182/6/3/38Hall thrusterssheathnumerical methods
spellingShingle Alejandro Lopez Ortega
Ioannis G. Mikellides
2D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge Regions
Plasma
Hall thrusters
sheath
numerical methods
title 2D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge Regions
title_full 2D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge Regions
title_fullStr 2D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge Regions
title_full_unstemmed 2D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge Regions
title_short 2D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge Regions
title_sort 2d fluid pic simulations of hall thrusters with self consistent resolution of the space charge regions
topic Hall thrusters
sheath
numerical methods
url https://www.mdpi.com/2571-6182/6/3/38
work_keys_str_mv AT alejandrolopezortega 2dfluidpicsimulationsofhallthrusterswithselfconsistentresolutionofthespacechargeregions
AT ioannisgmikellides 2dfluidpicsimulationsofhallthrusterswithselfconsistentresolutionofthespacechargeregions