Kinetic plasma dynamics in a radial model of a Hall thruster with a curved magnetic field

A 1D particle-in-cell model of a Hall thruster discharge is used to analyze the effect of a curved magnetic topology in the radial plasma response and the plasma fluxes to dielectric walls. The kinetic solution shows a significant replenishment of the velocity distribution function tail and temperature isotropization for both negative (i.e. anode pointing) and positive curvatures. The new radial magnetic force is electron confining or expanding for, respectively, negative and positive curvatures, and this modifies significantly the electric and pressure radial forces. As a consequence, the plasma density near the wall and the degree of radial ion defocusing are affected: they are highly reduced for negative curvatures, the case of higher interest. For positive curvatures, the kinetic solution shows that the radial ion flow becomes supersonic within the plasma bulk, away from the Debye sheaths. An ancillary quasineutral fluid model is presented to explain this feature and other aspects of the kinetic solution. Some kinetic studies on additional phenomena complete the work.

Automated summary

A one-dimensional particle-in-cell model was used to study the effect of a curved magnetic topology on the discharge plasma response and fluxes in a Hall thruster. The results showed that both positive and negative curvatures led to significant tail replenishment and isotropization of the temperature distribution. The radial magnetic force was found to either confine or expand electrons depending on the curvature, which greatly modified the radial electric and pressure forces. These changes in turn affected the plasma density near the wall and the degree of radial ion defocusing.