Cited by 27Low-Pressure Plasma Processing and DiagnosticsVacuum and Plasma ArcsIonosphere and magnetosphere dynamics

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On the limitations of hybrid particle-in-cell for ion thruster plume simulations

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Wang, Joseph, Hu, Yuan·2019·Physics of Plasmas

Abstract

A commonly used approach to simulate ion thruster plumes is a hybrid particle-in-cell (PIC) with the Boltzmann relation to model electrons. The limitations of such an approach are investigated by benchmarking hybrid PIC against fully kinetic PIC simulations using the real Xe+ to electron mass ratio (mi/me = 241073). The results show that both full PIC and hybrid PIC lead to similar plume density structures but very different plume potentials. If one could ignore the ion beam neutralization region near the thruster exit, the main physics missing from a hybrid PIC plume model is that from the anisotropic electron characteristics. Including the beam neutralization region leads to further changes in electron temperature and plume potential. Compared to full PIC simulations, the hybrid PIC model results in an overestimation of the plume potential by about 30%–40% in the transverse direction for the simulations considered. Since the electrons in the plume are nonequilibrium and anisotropic, simply replacing the Boltzmann relation with the more general polytropic thermodynamic relation for electrons in a hybrid PIC plume model will not lead to a significant improvement in accuracy.

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Research works printed but not linked: 26

  1. 1996, Three-dimensional modeling of dual ion-thruster plumes for spacecraft contamination, J. Spacecr. Rockets, 33, 519, 10.2514/3.26794 · DOI
  2. 2000, Deep space one investigations of ion propulsion plasma environment, J. Spacecr. Rockets, 37, 545, 10.2514/2.3608 · DOI
  3. 2001, Three-dimensional particle simulations of ion propulsion plasma environment for Deep Space 1, J. Spacecr. Rockets, 38, 433, 10.2514/2.3702 · DOI
  4. 2001, Review of Hall thruster plume modeling, J. Spacecr. Rockets, 38, 381, 10.2514/2.3695 · DOI
  5. 2006, Simulations of ion thruster plume–spacecraft interactions on parallel supercomputer, IEEE Trans. Plasma Sci., 34, 2148, 10.1109/TPS.2006.883406 · DOI
  6. 1996, Ion-thruster plume modeling for backflow contamination, J. Spacecr. Rockets, 33, 525, 10.2514/3.26795 · DOI
  7. 2001, Hybrid (particle/fluid) modeling of pulsed plasma thruster plumes, J. Propul. Power, 17, 945, 10.2514/2.5838 · DOI
  8. 2000, Particle simulations of a Hall thruster plume, J. Spacecr. Rockets, 37, 129, 10.2514/2.3536 · DOI
  9. 2014, Three-dimensional plume simulation of multi-channel thruster configuration, Plasma Sources Sci. Technol., 23, 065034, 10.1088/0963-0252/23/6/065034 · DOI
  10. 2004, Modeling of the near field plume of a Hall thruster, J. Appl. Phys., 95, 4575, 10.1063/1.1688444 · DOI
  11. 2015, Numerical studies on plasma plume flows from a cluster of electric propulsion devices, Aerosp. Sci. Technol., 41, 134, 10.1016/j.ast.2014.12.018 · DOI
  12. 2015, Influence of electron and ion thermodynamics on the magnetic nozzle plasma expansion, IEEE Trans. Plasma Sci., 43, 244, 10.1109/TPS.2014.2316020 · DOI
  13. 2015, Electron cooling and finite potential drop in a magnetized plasma expansion, Phys. Plasmas, 22, 053501, 10.1063/1.4919627 · DOI
  14. 2017, Hybrid 3d model for the interaction of plasma thruster plumes with nearby objects, Plasma Sources Sci. Technol., 26, 125008, 10.1088/1361-6595/aa986e · DOI · Paper page
  15. 2000, Three-dimensional simulations of ion thruster beam neutralization, Phys. Plasmas, 7, 5242, 10.1063/1.1322060 · DOI
  16. 2004, Investigation of ion beam neutralization processes with 2D and 3D PIC simulations, Comput. Phys. Commun., 164, 336, 10.1016/j.cpc.2004.06.045 · DOI
  17. 2012, Electron-ion coupling in mesothermal plasma beam emission: Full particle PIC simulations, IEEE Trans. Plasma Sci., 40, 230, 10.1109/TPS.2011.2179066 · DOI
  18. 2013, Electron behavior in ion beam neutralization in electric propulsion: Full particle-in-cell simulation, J. Phys.: Conf. Ser., 454, 012017, 10.1088/1742-6596/454/1/012017 · DOI
  19. 2015, Electron properties in collisionless mesothermal plasma expansion: Fully kinetic simulations, IEEE Trans. Plasma Sci., 43, 2832, 10.1109/TPS.2015.2433928 · DOI
  20. 2017, Fully kinetic simulations of collisionless, mesothermal plasma emission: Macroscopic plume structure and microscopic electron characteristics, Phys. Plasmas, 24, 033510, 10.1063/1.4978484 · DOI
  21. 2018, Expansion of a collisionless hypersonic plasma plume into a vacuum, Phys. Rev. E, 98, 023204, 10.1103/PhysRevE.98.023204 · DOI
  22. 2013, Experimental investigation on plasma plume potential, IEEE Trans. Plasma Sci., 41, 3438, 10.1109/TPS.2013.2277724 · DOI
  23. 1992, Ionospheric plasma flow over large high-voltage space platforms. I: Ion-plasma-time scale interactions of a plate at a zero-angle of attack, Phys. Fluids B, 4, 1597, 10.1063/1.860069 · DOI
  24. 1992, Ionospheric plasma flow over large high-voltage space platforms. II: The formation and structure of plasma wake, Phys. Fluids B, 4, 1615, 10.1063/1.860070 · DOI
  25. 2011, Ambipolar ion acceleration in an expanding magnetic nozzle, Plasma Sources Sci. Technol., 20, 015007, 10.1088/0963-0252/20/1/015007 · DOI
  26. 2018, In-plume acceleration of leading-edge ions from a pulsed plasma thruster, Plasma Sources Sci. Technol., 27, 104002, 10.1088/1361-6595/aae19d · DOI

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Metadata

Authors
Wang, J., & Hu, Y.
Affiliations
University of Southern California (US)
Corresponding author
Wang, Joseph
Venue
Physics of Plasmas
Published
2019-10-01
Volume
26
Issue
10
ISSN
  • 1070-664X (ISSN-L)
  • 1089-7674
OpenAlex
W2977320826
Cited by
27
References
0
Citations by year
2026: 1 · 2025: 3 · 2024: 3 · 2023: 6 · 2022: 3 · 2021: 8 · 2020: 3
FWCI
1.26
Type
journal article
Language
en
Open access
Locations
  • Physics of Plasmas (publishedVersion)
  • 中国科学院力学研究所 (submittedVersion)
Funders
University of Southern California
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 › Earth and Planetary Sciences › Space and Planetary Science › Ionosphere and magnetosphere dynamics
Keywords
ion thruster plume, Boltzmann relation, electron temperature, beam neutralization, nonequilibrium electrons, xenon ion beam

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