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The Effects of Nude Faraday Probe Design and Vacuum Facility Backpressure on the Measured Ion Current Density Profile of Hall Thruster Plumes

机译：裸体法拉第探头设计和真空设施背压对霍尔推进器羽毛测量离子电流密度曲线的影响

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《American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/Society of Automotive Engineers/American Society for Engineering Education Joint Propulsion Conference Exhibit》|2002年||共15页
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中图分类航空发动机（推进系统）;
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1. Plume Profiles of a Planar Crossed-Field Thruster with Hall Current Injection [J] . Joshua L. Rovey, Matthew P. Giacomi, Robert A. Stubbers, Journal of propulsion and power . 2009,第3期

机译：带有霍尔电流注入的平面交叉场推进器的羽状轮廓
2. Plume Profiles of a Planar Crossed-Field Thruster with Hall Current Injection [J] . Joshua L. Rovey, Matthew Giacomi, Robert Stubbers, Journal of Propulsion and Power . 2009,第3期

机译：带有霍尔电流注入的平面交叉场推进器的羽状轮廓
3. Evaluation of Facility Effects on Ion Migration in a Hall Thruster Plume [J] . Daniel L. Brown, Alec D. Gallimore Journal of propulsion and power . 2011,第3期

机译：设施对霍尔推力器羽流中离子迁移的影响评估
4. The Effects of Nude Faraday Probe Design and Vacuum Facility Backpressure on the Measured Ion Current Density Profile of Hall Thruster Plumes [C] . M. Walker, R. Hofer, A. Gallimore AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2002

机译：法拉第裸探头设计和真空设施背压对霍尔推进器羽流离子电流密度分布的影响
5. Effects of facility backpressure on the performance and plume of a Hall thruster. [D] . Walker, Mitchell Louis Ronald. 2005

机译：设施背压对霍尔推进器性能和羽流的影响。
6. Conduction Band Edge Energy Profile Probed by Hall Offset Voltage in InGaZnO Thin Films [O] . Hyo-Jun Joo, Dae-Hwan Kim, Hyun-Seok Cha, 2020

机译：通过HALL偏移电压探测InGazno薄膜的传导带边的能量轮廓
7. Evaluation of a Magnetically Filtered Faraday Probe for Measuring the Ion Current Density Profile of a Hall Thruster [O] . Joshua Rovey, Mitchell Walker, Peter Peterson, 2004

机译：磁过滤法拉第探头测量霍尔推进器的离子电流密度剖面的评价
8. Evaluation of Plume Divergence and Facility Effects on Far-Field Faraday Probe Current Density Profiles [R] . Brown, D. L., Gallimore, A. D. 2009

机译：羽流发散和设施对远场法拉第探头电流密度分布的影响评估

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