Abstract
Hall thruster plasma dynamics is studied in the framework of multi-fluid model with ionization and recombination. Electrons are modeled as magnetized and hot, whereas ions are assumed unmagnetized and cold. The neutral dynamics is included through the neutral continuity equation with uniform neutral flow. The computed plasma density profile shows that the maximum density is located slightly inward from the channel exit suggesting maximum ionization inside the channel. The electron temperature peaks just near the exit closer to the inner wall. The plasma potential is fairly flat in most part of the channel before falling at the exit. Simulation results are interpreted in the light of published experimental data and numerical results.
| Original language | English |
|---|---|
| Title of host publication | 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit |
| Place of Publication | Reston, VA |
| Publisher | American Institute of Aeronautics and Astronautics |
| Pages | 1-1 |
| Number of pages | 1 |
| ISBN (Print) | 9781624100987 |
| Publication status | Published - Jul 2003 |
| Externally published | Yes |
| Event | 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit - 2003 - Huntsville, United States Duration: 20 Jul 2003 → 23 Jul 2003 |
Other
| Other | 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit - 2003 |
|---|---|
| Country/Territory | United States |
| City | Huntsville |
| Period | 20/07/03 → 23/07/03 |
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