Effect of body bias on near-field electron behavior in a magnetically shielded Hall thruster

This work investigates the influence of thruster body bias on near-field electron behavior in a magnetically shielded Hall effect thruster (HET) through spatially resolved laser Thomson scattering diagnostics. Experiments were conducted on the 9 kW class H9 magnetically shielded HET operating at 40 A discharge current and 150 V discharge voltage on krypton propellant in the Georgia Tech Vacuum Test Facility 2. Three electrical configurations were examined: floating (body electrically isolated), cathode-tied (body at cathode potential, approximately −10.3 V relative to facility ground), and +2 V bias (body biased +2 V relative to ground). Spatially resolved measurements of electron density, electron temperature, and radial electron bulk velocity were obtained at up to 23 locations (a 15-point radial grid and up to eight axial stations along the cathode centerline) spanning the cathode near-field from the cathode centerline to the discharge channel centerline. A configuration-dependent spatial density inversion reveals distinct circuit topologies: at z/r0 = 0.029, cathode-tied elevates ne at the cathode centerline (4.4 × 1019 m−3) while exhibiting the lowest channel-centerline density (6.6 × 1017 m−3), whereas the +2 V configuration shows the opposite pattern (3.4 × 1019 and 9.0 × 1017 m−3, respectively). The +2 V configuration exhibits the lowest Te at the inner front pole cover, consistent with magnetization-limited, energy-selective electron collection. Electron pressure does not serve as a reliable proxy for electrostatic potential in this near-field region due to unmeasured anomalous transport terms.

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Publication Details

Journal
Journal of Applied Physics
Published
2026-08-24
DOI
https://doi.org/10.1063/5.0340395
Primary Topic
Plasma Diagnostics and Applications
Type
article
Field-Weighted Citation Impact
0.00

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article

Effect of body bias on near-field electron behavior in a magnetically shielded Hall thruster

Mitchell L. R. Walker, Julian Lopez-Uricoechea, Naia Butler-Craig, R. Dutta
Journal of Applied Physics
Plasma Diagnostics and Applications
article

Effect of body bias on near-field electron behavior in a magnetically shielded Hall thruster

Mitchell L. R. Walker, Julian Lopez-Uricoechea, Naia Butler-Craig, R. Dutta
article en

Abstract

This work investigates the influence of thruster body bias on near-field electron behavior in a magnetically shielded Hall effect thruster (HET) through spatially resolved laser Thomson scattering diagnostics. Experiments were conducted on the 9 kW class H9 magnetically shielded HET operating at 40 A discharge current and 150 V discharge voltage on krypton propellant in the Georgia Tech Vacuum Test Facility 2. Three electrical configurations were examined: floating (body electrically isolated), cathode-tied (body at cathode potential, approximately −10.3 V relative to facility ground), and +2 V bias (body biased +2 V relative to ground). Spatially resolved measurements of electron density, electron temperature, and radial electron bulk velocity were obtained at up to 23 locations (a 15-point radial grid and up to eight axial stations along the cathode centerline) spanning the cathode near-field from the cathode centerline to the discharge channel centerline. A configuration-dependent spatial density inversion reveals distinct circuit topologies: at z/r0 = 0.029, cathode-tied elevates ne at the cathode centerline (4.4 × 1019 m−3) while exhibiting the lowest channel-centerline density (6.6 × 1017 m−3), whereas the +2 V configuration shows the opposite pattern (3.4 × 1019 and 9.0 × 1017 m−3, respectively). The +2 V configuration exhibits the lowest Te at the inner front pole cover, consistent with magnetization-limited, energy-selective electron collection. Electron pressure does not serve as a reliable proxy for electrostatic potential in this near-field region due to unmeasured anomalous transport terms.

Journal of Applied PhysicsVol. 140(8)
Georgia Institute of Technology (US), Electric Propulsion Laboratory (United States) (US), Georgia Power (United States) (US)
Space Technology Mission Directorate
Openalex Percentile: Top 19%
Plasma Diagnostics and Applications
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