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Title: Geometrical Scaling of Hall Thruster Particle Model

Journal Article · · AIP Conference Proceedings
DOI:https://doi.org/10.1063/1.1941684· OSTI ID:20722255
 [1]; ;  [1];  [2]
  1. Dipartimento di Chimica, Universita degli Studi di Bari, via Orabona 4, 70126 Bari (Italy)
  2. Max Planck Institute fur Plasmaphysik, Wendelsteinstr. 1, D-17491 Greifswald (Germany)

Non-Maxwellian behaviour and plasma-wall interaction are key processes in the physics of Hall thrusters. For this purpose, a 2D{l_brace}r,z{r_brace}-3V axisymmetric fully kinetic Particle-in-Cell/Monte Carlo Collision (PIC-MCC) model of the acceleration channel including the process of secondary electron emission (SEE) from the dielectric walls has been developed. In order to make the simulation possible with regard to the computational time, a reduction of the thruster dimension was done. This was derived from a new physics-based scaling law. This model has demonstrated its outstanding capability in improving the physics insight into the processes in Stationary Plasma Thruster (SPT) and in reproducing accurately well experimental data.

OSTI ID:
20722255
Journal Information:
AIP Conference Proceedings, Vol. 762, Issue 1; Conference: 24. international symposium on rarefied gas dynamics, Bari (Italy), 10-16 Jul 2004; Other Information: DOI: 10.1063/1.1941684; (c) 2005 American Institute of Physics; Country of input: International Atomic Energy Agency (IAEA); ISSN 0094-243X
Country of Publication:
United States
Language:
English