Life Evaluation of a Lanthanum Hexaboride Hollow Cathode for High-Power Hall Thruster
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B36659
Reference22 articles.
1. 300-kW Solar Electric Propulsion System Configuration for Human Exploration of Near-Earth Asteroids
2. LaB6 Hollow Cathodes for Ion and Hall Thrusters
3. Compact lanthanum hexaboride hollow cathode
4. High-Current Lanthanum Hexaboride Hollow Cathode for High-Power Hall Thrusters
5. High-Current Lanthanum Hexaboride Hollow Cathode for 10-to-50-kW Hall Thrusters
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