Analysis of plume mode transition in a low-power iodine-fed hall thruster

Two distinct operating modes have been observed during development and testing of a low-power iodine-fed Hall thruster. These modes, named “jet” and “bell”, are visually identified by the plasma plume appearance and are associated with different performance figures. Thruster integral metrics and plasma properties are inferred and discussed to identify the parameters triggering the mode transition. It is found that a relevant fraction of slow ions appears when the thruster operates in bell mode and that the extracted ion flux spatially features a more diffused structure. Analysis of discharge current temporal dynamics supports the hypothesis that broadening of the discharge ionization length is responsible for the plume mode transition.

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Publication Details

Journal
Journal of Electric Propulsion
Published
2026-03-04
DOI
https://doi.org/10.1007/s44205-026-00183-z
Primary Topic
Plasma Diagnostics and Applications
Type
article
Field-Weighted Citation Impact
0.00

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article

Analysis of plume mode transition in a low-power iodine-fed hall thruster

F. Bianchi, Alfio E. Vinci
Journal of Electric Propulsion
Plasma Diagnostics and Applications
article

Analysis of plume mode transition in a low-power iodine-fed hall thruster

F. Bianchi, Alfio E. Vinci
article en

Abstract

Two distinct operating modes have been observed during development and testing of a low-power iodine-fed Hall thruster. These modes, named “jet” and “bell”, are visually identified by the plasma plume appearance and are associated with different performance figures. Thruster integral metrics and plasma properties are inferred and discussed to identify the parameters triggering the mode transition. It is found that a relevant fraction of slow ions appears when the thruster operates in bell mode and that the extracted ion flux spatially features a more diffused structure. Analysis of discharge current temporal dynamics supports the hypothesis that broadening of the discharge ionization length is responsible for the plume mode transition.

Journal of Electric PropulsionVol. 5(1)
Centre National de la Recherche Scientifique (FR), Université Toulouse III - Paul Sabatier (FR), Université Fédérale de Toulouse Midi-Pyrénées (FR), Institut National Polytechnique de Toulouse (FR), ThrustMe (France) (FR), Laboratoire Plasma et Conversion d'Energie (FR)
Association Nationale de la Recherche et de la Technologie
Openalex Percentile: Top 36%
Plasma Diagnostics and Applications
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Analysis of plume mode transition in a low-power iodine-fed hall thruster — F. Bianchi, Alfio E. Vinci · Journal of Electric Propulsion (2026) | TGRS Research Map | TGRS