A Numerical Simulation of Electromagnetic Environment around Ion Thruster Plume

Masahiro Kajikawa; Mengu Cho

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A Numerical Simulation of Electromagnetic Environment around Ion Thruster Plume

机译：离子推进器羽流周围电磁环境的数值模拟

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An ion thruster emits a high density plasma plume and the electromagnetic noise radiated from the plasma current may affect the spacecraft instrument. An electromagnetic particle simulation code has been developed to investi- gate the effects of the electromagnetic interference induced from the ion thruster plume. The electromagnetc waves are excited due to plasma instability caused by strong polarization field inside imperfectly neutralized plume.

机译：离子推进器会发射出高密度的等离子体羽流，而等离子体电流辐射出的电磁噪声可能会影响航天器仪器。已经开发出一种电磁粒子模拟程序来研究离子推进器羽流引起的电磁干扰的影响。电磁波由于不完全中和的羽状物内部的强极化场引起的等离子体不稳定性而被激发。

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《日本航空宇宙学会論文集》 |2000年第561期|p.343-349|共7页
作者
Masahiro Kajikawa; Mengu Cho;
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原文格式 PDF
正文语种 jpn
中图分类航空;
关键词
simulation; propulsion; space engineering;

机译：模拟;推进力太空工程;

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专利

1. A Numerical Simulation of Electromagnetic Environment around Ion Thruster Plume [J] . Masahiro Kajikawa, Mengu Cho 日本航空宇宙学会論文集 . 2000,第561期

机译：离子推进器羽流周围电磁环境的数值模拟
2. The importance of the cathode plume and its interactions with the ion beam in numerical simulations of Hall thrusters [J] . Ortega Alejandro Lopez, Mikellides Ioannis G. Physics of plasmas . 2016,第4期

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3. A 2D3V Electromagnetic PIC/MCC Simulation of Plume Properties in Ion Thruster [J] . Xiaolin Jin, Tao Huang, MingJuan Yang, Plasma Science, IEEE Transactions on . 2018,第8期

机译：离子推进器羽流特性的2D3V电磁PIC / MCC模拟
4. Computer Simulation of Electromagnetic Environment around the Ion Thruster Plume [C] . Mengu Cho, Masahiro Kajikara The Twenty-Second International Symposium on Space Technology and Science , May 28 - Jun 4, 2000, Morioka . 2000

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A Numerical Simulation of Electromagnetic Environment around Ion Thruster Plume

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