中国空间科学技术

• • 上一篇    下一篇

15厘米射频离子推力器—“RIT-15”的实验研究

酆惠芬   

  1. 中国科学院空间科学技术中心
  • 发布日期:1986-06-25

AN EXPERIMENT INVESTIGATION OF “RIT15-” 15cm RF-THRUSTER

Feng Huifen   

  • Online:1986-06-25

摘要: 本文简单介绍了“RIT—15”的工作原理,性能参数计算及实验结果。推力器是用惰性气体氙(Xe)和氩(Ar)作工质,以代替水银。结果表明:推力器可以正常运行,可拔出离子电流为150—220mA,相应的推力达7—14mN。由于用惰性气体运行方便、无毒,所以这是一种有希望的工质,但随之而来的是推力水平和质量效率的下降。这必须通过推力器结构的改进及进一步提高高频发生器的耦合性能来解决。

Abstract: Working principle of RIT-15, its performance, parameter calculation and its experiments are presented briefly in the article. The inert gases Xenon(Xe) and Argon(Ar)have been used instead of Mercury(Hg)as the thruster propellant. Experiment results show the thruster has normal operation. Beam current of 150~220mA can be extracted from the source and the correspondent thrust is 7~14mN. Inert gas is a kind of hopeful propellant for ion propulsion because it is convenient in operation and nonpoisonous. But inert gas thruster has lower thrust level and lower mass utilization, these disadvantages could be eliminated with improving the thruster structure and increasing the coupling ability of RF generator.