Endurance test of a 35-cm xenon ion thruster
Author:
Affiliation:
1. National Aerospace Lab., Tokyo, Japan
2. Toshiba Corp., Kanagawa, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3530
Reference7 articles.
1. Validation of the NSTAR ion propulsion system on the Deep Space One mission - Overview and initial results
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1. Numerical Simulation of Characteristics of CEX Ions in Ion Thruster Optical System;Chinese Journal of Aeronautics;2010-02
2. Application of Ion Thrusters to High-Thrust, High-Specifi c-Impulse Nuclear Electric Missions;Nuclear Space Power and Propulsion Systems;2008-08-22
3. Life Test of a Graphite-Orificed Hollow Cathode;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21
4. Status of the 150-mN Ion Engine Research at JAXA;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-21
5. Performance improvement of 150-mN xenon ion thrusters;Acta Astronautica;2003-01
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