Performance Evaluation of a Two-Kilowatt Magnetically Shielded Hall Thruster
Author:
Affiliation:
1. Tokyo Metropolitan University, Hino 191-0065, Japan
2. Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
3. Japan Aerospace Exploration Agency, Chofu 182-8522, Japan
Funder
Japan Society for the Promotion of Science
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Reference38 articles.
1. Electric propulsion for satellites and spacecraft: established technologies and novel approaches
2. Solar Electric Propulsion for Discovery-Class Missions
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5. Magnetic shielding of a laboratory Hall thruster. II. Experiments
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2. Electrical characteristics of a Hall effect thruster body in a vacuum facility testing environment;Journal of Electric Propulsion;2022-10-10
3. Method of Suppressing Ingestion Particles Flowing Back to a Hall Thruster using a Beam Target during Ground Testing;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2022
4. Design and demonstration of a micro air-fed magnetoplasmadynamic thruster for small satellites;Acta Astronautica;2021-04
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