Experimental Characterization of the Near-Wall Plasma in a 6-kW Hall Thruster and Comparison to Simulation

Author:

Shastry Rohit,Gallimore Alec,Hofer Richard

Publisher

American Institute of Aeronautics and Astronautics

Reference39 articles.

1. Hofer, R. R., Katz, I., Mikellides, I. G., Goebel, D. M., Jameson, K. K. et al. "Efficacy of Electron MobilityModels in Hybrid-PIC Hall Thruster Simulations," Presented at the44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,AIAA-2008-4924,Hartford, CT, July20-23, 2008.

2. Hofer, R. R., Mikellides, I. G., Katz, I., and Goebel, D. M. "BPT-4000 Hall Thruster Discharge Chamber Erosion Model Comparison with Qualification Life Test Data," Presented at the30th International Electric Propulsion Conference, IEPC-2007-267,Florence, Italy, September 17-20,2007.

3. Mikellides, I. G., Katz, I., Hofer, R. R., and Goebel, D. M. "Hall-effect Thruster Simulations with 2-D Electron Transport and Hydrodynamic Ions," Presented at the31st International Electric Propulsion Conference, IEPC-2009-114, Ann Arbor,MI,September 20 -24,2009.

4. Magnetic shielding of the channel walls in a Hall plasma accelerator

5. Yim, J. T., Keidar, M., and Boyd, I. D. "A Hydrodynamic-Based Erosion Model for Hall Thrusters," Presented at the29th International ElectricPropulsion Conference, IEPC-2005-013,Princeton, NJ, October31 -November4,2005.

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