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Simulation of a helicon plasma source in a magnetoplasma rocket engine
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作者 杨振宇 范威 +1 位作者 魏建国 韩先伟 《Plasma Science and Technology》 SCIE EI CAS CSCD 2022年第7期53-62,共10页
The helicon plasma source,which generates high thrust and high impulse,is of vital importance for magnetoplasma rocket engines.In this work,a multi-component,two-dimensional,axisymmetric fluid model coupled with an el... The helicon plasma source,which generates high thrust and high impulse,is of vital importance for magnetoplasma rocket engines.In this work,a multi-component,two-dimensional,axisymmetric fluid model coupled with an electromagnetic field was developed to model the helicon discharge.The simulation results demonstrate that:(i)the discharge mode changes twice—each conversion is accompanied by a plasma density jump and an electron temperature peak in the discharge;(ii)when the input current increases,the plasma density increases,and ionization occurs faster;(iii)the background magnetic field clearly enhances the discharge;(iv)the plasma density may be smaller if the discharge has not entered the wave mode. 展开更多
关键词 space propulsion mpre helicon plasma source discharge mode conversion
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