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.
| Original language | English |
|---|---|
| Pages (from-to) | 603-611 |
| Number of pages | 9 |
| Journal | Contributions to Plasma Physics |
| Volume | 48 |
| Issue number | 9-10 |
| DOIs | |
| State | Published - Dec 2008 |
Keywords
- Hall thruster
- Ignition
- Particle-in-cell
- Simulation
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