Rotating spoke instabilities in a wall-less Hall thruster: Simulations

Abstract

The low-frequency rotating plasma instability (spoke) in the ISCT200 thruster operating in the wall-less configuration was simulated with a 3 dimensional PIC MCC code. In the simulations an m = 1 spoke rotating with a velocity of 6.5 km/s in the ExB direction was observed. The rotating electron density structure in the spoke is accompanied by a strongly depleted region of the neutral gas, which clearly shows that the spoke instability is of an ionization nature, similar to the axial breathing mode oscillations. In the simulation the electron cross-field transport through the spoke core was caused by diffusion in the high-frequency (4-10 MHz), short-scale (3 mm) electric field oscillations. These short-scale oscillations play a crucial role in the thruster discharge as over 70% of the electron current to the anode originates from the spoke core. The rest of the current originates from the spoke front where the electron cross-field transport toward the anode is due to the ExB drift in the spoke macroscopic azimuthal electric field.

arXiv commentSubmitted to Plasma Sources Sci. Technol., 2019

Cited by in corpus (4)

• Perspectives on Physics of ExB Discharges Relevant to Plasma Propulsion and Similar Technologies
• Direct evidence of the gradient drift instability being the origin of a rotating spoke in a crossed field plasma
• Mode transitions and spoke structures in ExB Penning discharge
• The nonmodal kinetic theory for the electrostatic instabilities of a plasma with a sheared Hall current