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Using electron fluid models to analyze plasma thruster discharges
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Abstract Fluid models of the slow-dynamics of magnetized, weakly-collisional electrons lead to build computationally-affordable, long-time simulations of plasma discharges in Hall-effect and electrodeless plasma thrusters. This paper discusses the main assumptions and techniques used in 1D to 3D electron fluid models, and some examples illustrate their capabilities. Critical aspects of these fluid models are the expressions for the pressure tensor, the heat flux vector, the plasma-wall fluxes, and the high-frequency-averaged electron transport and heating caused by plasma waves, generated either by turbulence or external irradiation. The different orders of magnitude of the three scalar momentum equations characterize the electron anisotropic transport. Central points of the discussion are: the role of electron inertia, magnetically-aligned meshes versus Cartesian-type ones, the use of a thermalized potential and the infinite mobility limit, the existence of convective-type heat fluxes, and the modeling of the Debye sheath, and wall fluxes. Plasma plume models present their own peculiarities, related to anomalous parallel cooling and heat flux closures, the matching of finite plume domains with quiescent infinity, and solving fully collisionless expansions. Solutions of two 1D electron kinetic models are used to derive kinetically-consistent fluid models and compare them with more conventional ones.
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“For example, in EM codes, an explicit solver with integration time step ∆ t has to satisfy ω p , e ∆ t < 2, where ω p , e is the electron plasma frequency, or the Courant-Friedlich-Levy condition c ≤ ∆ r / ∆ t , where c is the phase wave velocity and ∆ r the mesh spacing.”
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“Among the different kinetic approaches 31 available, the particle representation allows a simple and intuitive implementation to account for a detailed description of plasma-gas and plasma-wall interactions, although it suffers from the inevitable but controllable limitation due to inherent discrete particle noise 32-35 and from its computationally intensive nature.”
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Wall material effects in stationary plasma thrusters. II. Near-wall and in-wall conductivity
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Latest progress in Hall thrusters plasma modelling
Taccogna, F., & Garrigues, L. (2019) · Reviews of Modern Plasma Physics · doi:10.1007/s41614-019-0033-1 · Cited by 103
Surface-driven asymmetry and instability in the acceleration region of Hall thruster
Taccogna, F., Longo, S., Capitelli, M., & Schneider, R. (2008) · Contributions to Plasma Physics · doi:10.1002/ctpp.200810061 · Cited by 28
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Plasma propulsion modeling with particle-based algorithms
Taccogna, F., Cichocki, F., Eremin, D., Fubiani, G., & Garrigues, L. (2023) · Journal of Applied Physics · doi:10.1063/5.0153862 · Cited by 29
Metadata
- Authors
- Ahedo, E.
- Affiliations
- Universidad Carlos III de Madrid (ES)
- Corresponding author
- Ahedo, Eduardo
- ORCID
- Ahedo, Eduardo
- Venue
- Journal of Electric Propulsion
- Published
- 2023-01-25
- Volume
- 2
- Issue
- 1
- ISSN
- 2731-4596 (ISSN-L)
- OpenAlex
- W4317937478
- Cited by
- 23
- References
- 3
- Citations by year
- 2026: 5 · 2025: 11 · 2024: 2 · 2023: 5
- FWCI
- 1.71
- Type
- journal article
- Language
- en
- Open access
- hybrid
- doi.org
- Locations
- Journal of Electric Propulsion (publishedVersion, cc-by)
- e-Archivo (Carlos III University of Madrid) (submittedVersion, cc-by)
- Funders
- Comunidad de Madrid (Y2018/NMT-4750 PROMETEO-CM)
- Topics
- Physical Sciences › Engineering › Electrical and Electronic Engineering › Low-Pressure Plasma Processing and Diagnostics
- Physical Sciences › Physics and Astronomy › Atomic and Molecular Physics, and Optics › Vacuum and Plasma Arcs
- Physical Sciences › Physics and Astronomy › Nuclear and High Energy Physics › Magnetic confinement fusion research
- Keywords
- electron fluid model, Hall thruster, electrodeless plasma thruster, pressure tensor, heat flux, electron inertia, convective heat flux, plasma sheath, magnetized plasma
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