An axisymmetric hybrid model of the plasma in a radio-frequency ion thruster chamber

Abstract An axisymmetric hybrid particle/fluid code has been applied to simulate the plasma behavior in the discharge chamber of a radio-frequency ion thruster (RIT). Suitable assumptions have been made to include the coupling with the three other elements of the thruster: the time-averaged deposited power from the radio-frequency (RF) source, the effective transparencies for ion and neutral extraction from the grid system, and the electrical connection with the external neutralizer. A detailed parametric analysis has been carried out in terms of deposited RF power and injected mass flow rate of xenon. As the RF power increases: high propellant utilization and ion beam current are obtained, the maximum plasma density moves away from the chamber center and close to the flow injector, and the beam-to-total energy efficiency decreases. As a result, for a given mass flow rate, there is an optimal RF power that maximizes the thrust efficiency. At these conditions, about 60% of the RF deposited power is lost into the walls due to the lack of magnetic confinement and multiple re-ionizations of wall-recombined neutrals penalize the inelastic losses too. Additional studies have analyzed the influence of: the electrical connections to the neutralizer, which just change the electron current paths; the effective transparency of the grids, where a large sensitivity is found to the ion transparency; the reduction of the energy accommodation of heavy species after wall impact, which penalizes much the maximum thrust efficiency; the presence of metastable atoms and stepwise ionization, which although present, have marginal effects on performances as a result of the multiple wall interactions. A global model, derived from the 2D model and constituted of algebraic expressions, can yield the main performance figures and averaged plasma magnitudes in the chamber with a relative error of up to ± 15%. Finally, 2D simulations are compared indirectly with existing data for a RIT-4.

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Publication Details

Journal
Plasma Sources Science and Technology
Published
2025-07-30
DOI
https://doi.org/10.1088/1361-6595/adf5e3
Citations
1
Primary Topic
Plasma Diagnostics and Applications
Type
article
Field-Weighted Citation Impact
0.73
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article

An axisymmetric hybrid model of the plasma in a radio-frequency ion thruster chamber

Jiewei Zhou, Simone Dalle Fabbriche, Eduardo Ahedo
1 citations
Plasma Sources Science and Technology
Plasma Diagnostics and Applications
0.73
article

An axisymmetric hybrid model of the plasma in a radio-frequency ion thruster chamber

Jiewei Zhou, Simone Dalle Fabbriche, Eduardo Ahedo
article en
1 citations

Abstract

Abstract An axisymmetric hybrid particle/fluid code has been applied to simulate the plasma behavior in the discharge chamber of a radio-frequency ion thruster (RIT). Suitable assumptions have been made to include the coupling with the three other elements of the thruster: the time-averaged deposited power from the radio-frequency (RF) source, the effective transparencies for ion and neutral extraction from the grid system, and the electrical connection with the external neutralizer. A detailed parametric analysis has been carried out in terms of deposited RF power and injected mass flow rate of xenon. As the RF power increases: high propellant utilization and ion beam current are obtained, the maximum plasma density moves away from the chamber center and close to the flow injector, and the beam-to-total energy efficiency decreases. As a result, for a given mass flow rate, there is an optimal RF power that maximizes the thrust efficiency. At these conditions, about 60% of the RF deposited power is lost into the walls due to the lack of magnetic confinement and multiple re-ionizations of wall-recombined neutrals penalize the inelastic losses too. Additional studies have analyzed the influence of: the electrical connections to the neutralizer, which just change the electron current paths; the effective transparency of the grids, where a large sensitivity is found to the ion transparency; the reduction of the energy accommodation of heavy species after wall impact, which penalizes much the maximum thrust efficiency; the presence of metastable atoms and stepwise ionization, which although present, have marginal effects on performances as a result of the multiple wall interactions. A global model, derived from the 2D model and constituted of algebraic expressions, can yield the main performance figures and averaged plasma magnitudes in the chamber with a relative error of up to ± 15%. Finally, 2D simulations are compared indirectly with existing data for a RIT-4.

Plasma Sources Science and TechnologyVol. 34(8)
Universidad Carlos III de Madrid (ES)
Openalex Percentile: Top 25%
Plasma Diagnostics and Applications
0.73
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