Performance Degradation of a Spacecraft Electron Cyclotron Resonance Neutralizer and Its Mitigation
Author:
Affiliation:
1. Dept. of Aeronautics and Astronautics, University of Tokyo, Bunkyo, Tokyo 113-8656, Japan
2. Dept. of Space Flight Systems, Institute of Space and Astronautical Science, Sagamihara, Kanagawa 252-5210, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35062
Reference9 articles.
1. Development of microwave discharge ion thruster for asteroid sample return mission
2. Development and Demonstration of a Cathodeless Electron Cyclotron Resonance Ion Thruster
3. Verification Tests of Carbon-Carbon Composite Grids for Microwave Discharge Ion Thruster
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