›› 2014, Vol. 23 ›› Issue (10): 105202-105202.doi: 10.1088/1674-1056/23/10/105202

• PHYSICS OF GASES, PLASMAS, AND ELECTRIC DISCHARGES • 上一篇    下一篇

A radial non-uniform helicon equilibrium discharge model

成玉国, 程谋森, 王墨戈, 李小康   

  1. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
  • 收稿日期:2014-01-30 修回日期:2014-03-28 出版日期:2014-10-15 发布日期:2014-10-15
  • 基金资助:
    Project supported by the National Natural Science Foundation of China (Grant No. 11305265).

A radial non-uniform helicon equilibrium discharge model

Cheng Yu-Guo (成玉国), Cheng Mou-Sen (程谋森), Wang Mo-Ge (王墨戈), Li Xiao-Kang (李小康)   

  1. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
  • Received:2014-01-30 Revised:2014-03-28 Online:2014-10-15 Published:2014-10-15
  • Contact: Wang Mo-Ge E-mail:tlothf@126.com
  • About author:52.75.Di; 52.50.Qt; 02.60.Cb; 88.85.J-
  • Supported by:
    Project supported by the National Natural Science Foundation of China (Grant No. 11305265).

摘要: Helicon discharges have attracted great attention in the electric propulsion community in recent years. To acquire the equilibrium properties, a self-consistent model is developed, which combines the helicon/Trivelpiece-Gould (TG) waves-plasma interaction mechanism and the plasma flow theory under the confinement of the magnetic field. The calculations reproduce the central peak density phenomenon observed in the experiments. The results show that when operating in the wave coupling mode, high magnetic field strength B0 results in the deviation of the central density versus B0 from the linear relationship, while the density rise becomes flatter as the radiofrequency (rf) input power Prf grows, and the electron temperature Te radial profile is mainly determined by the characteristic of the rf energy deposition. The model could provide suggestions in choosing the B0 and Prf for medium power helicon thrusters.

关键词: helicon discharges, magnetic field, radial properties, thruster

Abstract: Helicon discharges have attracted great attention in the electric propulsion community in recent years. To acquire the equilibrium properties, a self-consistent model is developed, which combines the helicon/Trivelpiece-Gould (TG) waves-plasma interaction mechanism and the plasma flow theory under the confinement of the magnetic field. The calculations reproduce the central peak density phenomenon observed in the experiments. The results show that when operating in the wave coupling mode, high magnetic field strength B0 results in the deviation of the central density versus B0 from the linear relationship, while the density rise becomes flatter as the radiofrequency (rf) input power Prf grows, and the electron temperature Te radial profile is mainly determined by the characteristic of the rf energy deposition. The model could provide suggestions in choosing the B0 and Prf for medium power helicon thrusters.

Key words: helicon discharges, magnetic field, radial properties, thruster

中图分类号:  (Ion and plasma propulsion)

  • 52.75.Di
52.50.Qt (Plasma heating by radio-frequency fields; ICR, ICP, helicons) 02.60.Cb (Numerical simulation; solution of equations) 88.85.J- (Vehicle energy storage)