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A 2-kW class magnetically shielded Hall thruster was developed and its performance was experimentally evaluated. Additionally, the effects of the discharge channel length, thruster body potential, anode dielectric coating, and vacuum facility on its performance were investigated.
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This page is a summary of: Performance Evaluation of a Two-Kilowatt Magnetically Shielded Hall Thruster, Journal of Propulsion and Power, January 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37550.
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