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Kinetic electron model for plasma thruster plumes
Open accessAbstract
A paraxial model of an unmagnetized, collisionless plasma plume expanding into vacuum is presented. Electrons are treated kinetically, relying on the adiabatic invariance of their radial action integral for the integration of Vlasov's equation, whereas ions are treated as a cold species. The quasi-2D plasma density, self-consistent electric potential, and electron pressure, temperature, and heat fluxes are analyzed. In particular, the model yields the collisionless cooling of electrons, which differs from the Boltzmann relation and the simple polytropic laws usually employed in fluid and hybrid PIC/fluid plume codes.
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At low electron temperatures, the contribution of metastable states to the total ionization rate can be relevant.
“Additionally, the ionization rates of the ground state and of these two metastable states are also reported, showing that, at low electron temperatures, the contribution of metastable states to the total ionization rate can be relevant.”
From Plasma propulsion modeling with particle-based algorithms (2023) · cites this paper as [283]
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Research works printed but not linked: 38
- Roy, 1996, Ion-thruster plume modeling for backflow contamination, J. Spacecr. Rockets, 33, 525, 10.2514/3.26795 · DOI
- Tverdokhlebova, 2000, Plasma plume/spacecraft interaction. State of the art in investigation methodology, Spacecr. Propul., 465, 675
- Tajmar, 2001, Modelling of spacecraft-environment interactions on SMART-1, J. Spacecr. Rockets, 38, 393, 10.2514/2.3697 · DOI
- Goebel, 2008, 10.1002/9780470436448 · DOI · Paper page
- Garrett, 2000, Spacecraft charging, an update, IEEE Trans. Plasma Sci., 28, 2017, 10.1109/27.902229 · DOI
- Garrett, 2012, 10.1002/9781118241400 · DOI
- Leboeuf, 1996, Modeling of plume dynamics in laser ablation processes for thin film deposition of materials, Phys. Plasmas, 3, 2203, 10.1063/1.871676 · DOI
- Lieberman, 2005, 10.1002/0471724254 · DOI · Paper page
- Lebedev, 2005, Production of radiatively cooled hypersonic plasma jets and links to astrophysical jets, Plasma Phys. Control. Fusion, 47, B465, 10.1088/0741-3335/47/12B/S33 · DOI
- Gallimore, 2001, Near- and far-field characterization of stationary plasma thruster plumes, J. Spacecr. Rockets, 38, 361, 10.2514/2.3703 · DOI
- Beal, 2005, Plasma properties downstream of a low-power Hall thruster, Phys. Plasmas, 12, 123503, 10.1063/1.2145097 · DOI
- Foster, 2006, Plasma characteristics measured in the plume of a next multi-thruster array, 10.2514/6.2006-5181 · DOI
- Ekholm, 2006, Plume characteristics of the Busek 600 W Hall thruster, 10.2514/6.2006-4659 · DOI
- Nakles, 2007, Experimental and numerical examination of the BHT-200 Hall thruster plume, 10.2514/6.2007-5305 · DOI
- Dannenmayer, 2012, Hall effect thruster plasma plume characterization with probe measurements and self-similar fluid models, 10.2514/6.2012-4117 · DOI
- Dannenmayer, 2013, Electron flow properties in the far-field plume of a Hall thruster, Plasma Sources Sci. Technol., 22, 10.1088/0963-0252/22/3/035004 · DOI
- Giono, 2018, Non-Maxwellian electron energy probability functions in the plume of a SPT-100 Hall thruster, Plasma Sources Sci.Technol., 27, 10.1088/1361-6595/aaa06b · DOI
- Hilgers, 2006, A simple model of the effect of solar array orientation on SMART-1 floating potential, IEEE Trans. Plasma Sci., 34, 2159, 10.1109/TPS.2006.883405 · DOI
- Gabdullin, 2008, The plasma plume emitted onboard the international space station under the effect of the geomagnetic field, IEEE Trans. Plasma Sci., 36, 2207, 10.1109/TPS.2008.2004236 · DOI
- Estublier, 2008, The SMART-1 spacecraft potential investigations, IEEE Trans. Plasma Sci., 36, 2262, 10.1109/TPS.2008.2002032 · DOI
- Aston, 1978, Ion beam divergence characteristics of two-grid accelerator systems, AIAA J., 16, 516, 10.2514/3.7538 · DOI
- Boyd, 2002, Far field modeling of the plasma plume of a Hall thruster, J. Appl. Phys., 92, 1764, 10.1063/1.1492014 · DOI
- Merino, 2015, Collisionless plasma thruster plume expansion model, Plasma Sources Sci. Technol., 24, 10.1088/0963-0252/24/3/035006 · DOI · Paper page
- Wang, 2001, Three-dimensional particle simulation modeling of ion propulsion plasma environment for Deep Space I, J. Spacecr. Rockets, 3, 433, 10.2514/2.3702 · DOI
- Hu, 2015, Electron properties in collisionless mesothermal plasma expansion: fully kinetic simulations, IEEE Trans. Plasma Sci., 43, 2832, 10.1109/TPS.2015.2433928 · DOI
- Korsun, 2004, Simulation of plasma plume-to-spacecraft interaction, Comput. Phys. Commun., 164, 353, 10.1016/j.cpc.2004.06.047 · DOI
- Ortega, 2015, Self-consistent model of a high-power Hall thruster plume, IEEE Trans. Plasma Sci., 43, 2875, 10.1109/TPS.2015.2446411 · DOI · Paper page
- VanGilder, 1999, Hybrid Monte Carlo-particle-in-cell simulation of an ion thruster plume, J. Propul. Power, 15, 530, 10.2514/2.5475 · DOI
- Brieda, 2004, Development of the DRACO code for modeling electric propulsion plume interactions, 10.2514/6.2004-3633 · DOI
- Taccogna, 2014, Three-dimensional plume simulation of multi-channel thruster configuration, Plasma Sources Sci.Technol., 23, 10.1088/0963-0252/23/6/065034 · DOI
- Araki, 2016, SM/MURF: current capabilities and verification as a replacement of AFRL plume simulation tool COLISEUM, 4939, 10.2514/6.2016-4939 · DOI
- Cichocki, 2017, Hybrid 3D model for the interaction of plasma thruster plumes with nearby objects, Plasma Sources Sci. Technol., 26, 10.1088/1361-6595/aa986e · DOI · Paper page
- Boyd, 2004, Modeling of the near field plume of a Hall thruster, J. Appl. Phys., 95, 4575, 10.1063/1.1688444 · DOI
- Passaro, 2004, 3D computation of plasma thruster plumes, 10.2514/6.2004-3632 · DOI
- Raadu, 1979, Expansion of a plasma injected from an electrodeless gun along a magnetic field, Plasma Phys., 21, 331, 10.1088/0032-1028/21/4/003 · DOI
- Martinez-Sanchez, 2015, Electron cooling and finite potential drop in a magnetized plasma expansion, Phys. Plasmas, 22, 10.1063/1.4919627 · DOI
- Plaza, 2016, Expansion of a collisionless magnetized plasma plume with bi-Maxwellian electrons, 10.2514/6.2016-5035 · DOI
- Martínez-Sánchez, 2011, Magnetic mirror effects on a collisionless plasma in a convergent geometry, Phys. Plasmas, 18, 033509, 10.1063/1.3554650 · DOI
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“370 Temperature anisotropy is a relevant feature in most cases and a real challenge for diagnostics too.”
Self-citationLatest 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
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
- Merino, M., Mauriño, J., & Ahedo, E.
- Affiliations
- Universidad Carlos III de Madrid (ES)
- Corresponding author
- Merino, Mario
- Venue
- Plasma Sources Science and Technology
- Publisher
- IOP Publishing
- Published
- 2018-03-01
- Volume
- 27
- Issue
- 3
- Pages
- 035013
- ISSN
- 0963-0252 (ISSN-L)
- 1361-6595
- OpenAlex
- W2791151390
- Cited by
- 30
- References
- 0
- Citations by year
- 2026: 2 · 2025: 2 · 2024: 3 · 2023: 5 · 2022: 4 · 2021: 3 · 2020: 5 · 2019: 4 · 2018: 2
- FWCI
- 1.34
- Type
- journal article
- Language
- en
- Open access
- bronze
- doi.org
- Licence
- Locations
- Plasma Sources Science and Technology (publishedVersion)
- LA Referencia (Red Federada de Repositorios Institucionales de Publicaciones Científicas) (acceptedVersion, other-oa)
- e-Archivo (Carlos III University of Madrid) (submittedVersion, other-oa)
- Funders
- European Space Agency (4000116180/15/NL/PS)
- 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 › Atomic and Molecular Physics, and Optics › Dust and Plasma Wave Phenomena
- Keywords
- collisionless plasma, Vlasov equation, adiabatic invariance, electron cooling, electron pressure, electron heat flux, unmagnetized plasma
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