PIC/Fluid simulations of the plasma expansion in a planar magnetic arch

dc.bibliographicCitation.articleNumber015007
dc.bibliographicCitation.issue1
dc.bibliographicCitation.journalTitlePlasma Sources Science and Technology
dc.bibliographicCitation.volume34
dc.contributor.authorGuaita, M.
dc.contributor.authorAhedo, E.
dc.contributor.authorMerino, M.
dc.date.accessioned2026-03-06T14:31:30Z
dc.date.available2026-03-06T14:31:30Z
dc.date.issued2025
dc.description.abstractMagnetic arches (MA) (i.e. the magnetic topology that emerges when placing two magnetic nozzles with opposite polarities side by side) are an attractive option for the clustering of multiple electrodeless plasma thrusters, as they are characterized by a zero magnetic dipole moment and thus allow a reduction of perturbing magnetic forces on the spacecraft. This work employs the hybrid code EP2PLUS to simulate and study the plasma expansion for such a magnetic topology in the planar limit. First, a reference simulation is used to analyze the leading physical mechanisms that govern the plume properties. Ions are thus found to be characterized by a double peaked velocity distribution function close to the symmetry plane, where the plasma beams emitted by the two thrusters merge, while the magnetic force acting on electrons is shown to shape both the lateral confinement of the plume, and the thrust profile provided. Second, a parametric sweep on the strength of the magnetic field shows that its influence on the propulsive properties and on the characteristics of the plume saturates for values of the Hall parameter larger than around 10. Beyond this value of the Hall parameter, only the in-plane electron currents are found to be particularly sensitive both to the magnetization levels and the boundary conditions employed, although they are also largely decoupled from the rest of plasma properties. Finally, background pressure effects were considered by including collisions with neutral atoms in the simulations, highlighting the relevance of neutral entrainment in the modification of the plume properties and in the propulsive performance of the MA.eng
dc.description.versionpublishedVersioneng
dc.identifier.urihttps://oa.tib.eu/renate/handle/123456789/32182
dc.identifier.urihttps://doi.org/10.34657/31251
dc.language.isoeng
dc.publisherBristol : IOP Publ.
dc.relation.doihttps://doi.org/10.1088/1361-6595/adab8e
dc.relation.essn1361-6595
dc.relation.issn0963-0252
dc.rights.licenseCC BY 4.0 Unported
dc.rights.urihttps://creativecommons.org/licenses/by/4.0
dc.subject.ddc530
dc.subject.otherelectrodeless plasma thrustereng
dc.subject.otherfacility effectseng
dc.subject.othermagnetic nozzleeng
dc.subject.othermagnetized plasma expansionseng
dc.subject.otherparticle in celleng
dc.subject.otherplasma space propulsioneng
dc.subject.otherLTP researcheng
dc.titlePIC/Fluid simulations of the plasma expansion in a planar magnetic archeng
dc.typeArticle
tib.accessRightsopenAccess

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