Electron transport in a Hall thruster from an axial-azimuthal PIC code including interaction with radial walls.
ORAL
Abstract
Addressing the development and nonlinear saturation of the involved plasma instabilities requires a self-consistent formulation of the weakly-collisional magnetized discharge. Unfortunately, 3D kinetic models have an extremely high computational cost due to the disparate dynamics of plasma species and the small Debye length. Thus a common approach is using axial-azimuthal (2D) simulations, but these often neglect or oversimplify the strong plasma interaction with radial walls. The present work incorporates semi-consistently this radial interaction in an axial-azimuthal PIC code and analyzes parametrically how it affects the kinetic instabilities and the resulting cross-field electron transport.
–
Publication: Previous related work
- G. Cuerva-Lazaro, E. Bello-Benıtez,A. Marin-Cebrian, E. Ahedo,`Towards self-consistent simulation of radial effects on an axial PIC model of the Hall discharge`, IEPC-2024-699, Presented at the 38th International Electric Propulsion Conference, Toulouse, France, June 23-28, 2024
- E. Bello-Benítez, A. Marín-Cebrián, E. Ahedo, 'Effect of injection conditions on the non-linear behavior of the ECDI and related
turbulent transport', arXiv preprint 2405.08761, 2024, arxiv.org
Presenters
-
EDUARDO ( AHEDO
UNIVERSIDAD CARLOS III DE MADRID, Universidad Carlos III de Madrid
Authors
-
EDUARDO ( AHEDO
UNIVERSIDAD CARLOS III DE MADRID, Universidad Carlos III de Madrid
-
Guillermo Cuerva Lazaro
UC3M
-
Alberto Marin-Cebrian
UC3M
-
Enrique Bello-Benítez
UC3M