Cathode studies of a radiation cooled MPD arc thruster

机译：辐射冷却MPD电弧推进器的阴极研究

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Cathode insulator modifications of radiation cooled MPD arc thrustor tested in power range of 9.8 to 46.4 kW using ammonia as principal propellant

机译：使用氨气作为主要推进剂的辐射冷却MPD弧形推进器的阴极绝缘体修改在9.8至46.4 kW的功率范围内进行了测试

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Esker D. W.; Kroutil J. C.; Sedrick A. V.;
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年度 1971
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1. Discharge characteristics of two-stage micro-cathode arc MPD thrusters with a permanent magnet and a pulsed magnetic field [J] . Zolotukhin D., Daniels K., Keidar M. Journal of Physics, D. Applied Physics: A Europhysics Journal . 2021,第1期

机译：具有永磁体和脉冲磁场的两级微阴极电弧MPD推进器的放电特性
2. Cathode Jet Structure in Quasi-Steady MPD thrusters [J] . Kazunori Mitsuo, Hirokazu Tahara, Naoya Yamasaki 日本航空宇宙学会論文集 . 2000,第555期

机译：准稳态MPD推进器的阴极射流结构
3. Cathode Jet Structure in Quasi-Steady MPD thrusters [J] . Kazunori Mitsuo, Hirokazu Tahara, Naoya Yamasaki 日本航空宇宙学会論文集 . 2000,第555期

机译：准稳态MPD推进器的阴极射流结构
4. Experimental study of a Multichannel Hollow Cathode for High Power MPD Thrusters [C] . R. Albertoni, M. De Tata, P. Rossetti, AIAA/ASME/SAE/ASEE joint propulsion conference exhibit . 2012

机译：大功率MPD推进器多通道空心阴极的实验研究
5. Enhancing Micro-Cathode Arc Thruster (muCAT) Plasma Generation to Analyze Magnetic Field Angle Effects on Sheath Formation in Hall Thrusters. [D] . Lukas, Joseph Nicholas. 2016

机译：增强微型阴极电弧推力器（muCAT）等离子体的产生，以分析磁场角度对霍尔推力器鞘层形成的影响。
6. Radiofrequency ablation using internally cooled wet electrodes in bipolar mode for the treatment of recurrent hepatocellular carcinoma after locoregional treatment: A randomized prospective comparative study [O] . Jae Won Choi, Jeong Min Lee, Dong Ho Lee, 2020

机译：射频消融在局部处理后双极模式中使用内部冷却的湿润电极进行治疗型肝细胞癌：随机性前瞻性比较研究
7. Initial performance data on a low-power MPD arc thruster with a downstream cathode [O] . Burkhart, J. A. 1970

机译：具有下游阴极的低功率MPD弧推进器的初始性能数据
8. Cathode studies of a radiation cooled MPD arc thruster [R] . Esker, D. W., Kroutil, J. C., Sedrick, A. V. 1971

机译：辐射冷却mpD电弧推进器的阴极研究

Cathode studies of a radiation cooled MPD arc thruster

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