Active Stabilization of a Magnesium Hall Thruster in Constant Voltage Mode
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Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. Massey, D.,A.Kieckhafer,J.Sommervilleand L.B. King,"Development ofa VaporizingLiquid Bismuth Anode for Hall Thrusters", 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA-2004-3768, Fort Lauderdale,Florida,2004.
2. Development of a Direct Evaporation Bismuth Hall Thruster
3. Makela, J. M., L. B. King, D. R. Massey and E. C. Fossum, "Development and Testing of a Prototype Bismuth Cathode for Hall Thrusters", 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA-2005-4236,Tucson,Arizona,2005.
4. Announcements and Acknowledgments
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Performance Comparison Between a Magnesium- and Xenon-Fueled 2 Kilowatt Hall Thruster;Journal of Propulsion and Power;2016-07
2. Demonstration of an Automated Mass Flow Control System for Condensable Propellant Hall-effect Thrusters;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30
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