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用于微小卫星推进装置的脉冲等离子体推力器

The Pulsed Plasma Thruster for Propeller in Small and Micro Satellite

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【作者】 牛禄王宏伟杨威

【Author】 NIU Lu, WANG Hong-wei, YANG Wei (Shanghai Xin Li Institute of Propulsion, Shanghai 200125, China)

【机构】 上海新力动力机械研究所上海新力动力机械研究所 上海200125上海200125上海200125

【摘要】 论述了脉冲等离子体推力器(PPT)的工作原理和研究状况。在分析其主要优缺点的基础上,讨论了PPT技术的发展方向,并就PPT的应用前景作了展望。分析认为PPT是一种先进的小推力动力装置,特别适合于微小卫星的轨道转移、姿态控制、位置保持以及星座编队飞行。

【Abstract】 The principle and research status of pulsed plasma thruster (PPT) were put forward in this paper. The technology development trend of PPT was disscused on the basis of the analysis of advantages and disadvantages. The expectation for the technology in future was also presented. It was showed that PPT was a kind of advanced propeller with small thrust, which was suitable to orbit transfer, attitude control, station keeping and formation flying for small and micro satellite.

  • 【文献出处】 上海航天 ,Aerospace Shanghai , 编辑部邮箱 ,2004年05期
  • 【分类号】V439.2
  • 【被引频次】40
  • 【下载频次】715
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