A High-Speed Probe Positioning System for Interrogating the Discharge Plasma of a 30cm Ion Thruster.
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American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
テクニカルペーパー
Comparison of Discharge Plasma Parameters in a 30-m NSTAR Type Ion Engine with and Without Beam Extraction
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
テクニカルペーパー
Laser-induced Fluorescence Velocimetry of Xe II in the 30-cm NSTAR-type Ion Engine Plume
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
テクニカルペーパー
Discharge Cathode Electron Energy Distribution Functions in a 40-cm NEXT-Type Ion Engine
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |