On a force balance and role of cathode plasma in Hall effect thrusters

Abstract

The cathode plasma is a specific transition region in the Hall Effect Thruster (HET) discharge that localizes between the strongly magnetized acceleration layer (magnetic layer or B-layer) and non-magnetized exhaust plume. Cathode plasma provides a flow of electron current that supplies losses in the magnetic layer (due to ionization, excitation, electron-wall interactions, etc.). The electrons' transport in this region occurs in collisionless mode through the excitation of plasma instabilities. This effect is also known as "anomalous transport/conductivity". In this work, we present the results of a 2d (drift-plane) kinetic simulation of the HET discharge, including the outside region that contains cathode plasma. We discuss the process of cathode plasma formation and the mechanisms of "anomalous transport" inside it. We also analyze how fluid force balance emerges from collisionless kinetic approach. The acceleration mechanism in Hall Effect Thrusters (HETs) is commonly described in terms of force balance. Namely, the reactive force produced by accelerated ions has the same value as Ampère's force acting on a drift current loop. This balance written in integral form provides the basis for quantitative estimations of HETs' parameters and scaling models.

The comparison of two-term Boltzmann approximation and Monte-Carlo solutions for e+Ar0 plasma

“…The TTB code described in the article is based on the idea of a weak anisotropy of the eEDF in the electric field, which makes it possible to take into account only the first two terms of the eEDF decomposition in the energy space, i.e., to perform linearization of eEDF, and implements the solution of the non-stationary BKE. The MCC code takes its origin from the ΘHall PiC+MCC code described before in [36,37]. The Monte-Carlo module was heavily modified and rewritten to support an arbitrary set of reactions and active/background components.…”