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Investigation of the Start Transient in a Hall Thruster

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Indexed by:期刊论文

Date of Publication:2008-01-01

Journal:CONTRIBUTIONS TO PLASMA PHYSICS

Included Journals:SCIE、Scopus

Volume:48

Issue:9-10

Page Number:603-611

ISSN No.:0863-1042

Key Words:Hall thruster; particle-in-cell; ignition; simulation

Abstract:A two dimensional axisymmetric fully kinetic Particle-in-Cell/Monte Carlo Collision (PIC-MCC) model is used to describe the ignition process in a Hall thruster. A current peak and latter the periodic oscillation of current and electric potential are found. The corresponding evolutions of plasma density, electric potential and atom density during the ignition process are introduced in the paper. In addition, influences of mass flow rate and discharge potential on current peak are modeled and analyzed. The simulated results are consistent with former experimental results. (C) 2008 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim

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