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设计参数对脉冲等离子体推力器性能的影响
引用本文:侯大立,赵万生,康小明.设计参数对脉冲等离子体推力器性能的影响[J].上海交通大学学报,2007,41(7):1209-1212.
作者姓名:侯大立  赵万生  康小明
作者单位:上海交通大学,机械与动力工程学院,上海,200240
基金项目:致谢感谢航天科技集团801所康小录、余水林和乔彩霞在实验中给予的帮助.
摘    要:脉冲等离子体推力器的性能受电气参数、结构设计参数等方面的影响.针对脉冲等离子体推力器效率低的问题进行了理论分析并设计实验进行了验证,研究了设计参数与推力器性能之间的关系.结果表明,推力与放电电流有密切的关系,而脉冲等离子体推力器的电极间距、放电能量等设计参数对推力、放电电流等又有较大的影响.实验结果对设计高性能的推力器有参考价值.

关 键 词:脉冲等离子体推力器  比冲  推力  元冲量
文章编号:1006-2467(2007)07-1209-04
修稿时间:2006-11-15

The Effect of Designing Parameters on Performance of Pulsed Plasma Thruster
HOU Da-li,ZHAO Wan-sheng,KANG Xiao-ming.The Effect of Designing Parameters on Performance of Pulsed Plasma Thruster[J].Journal of Shanghai Jiaotong University,2007,41(7):1209-1212.
Authors:HOU Da-li  ZHAO Wan-sheng  KANG Xiao-ming
Institution:School of Mechanical Eng. , Shanghai Jiaotong Univ. , Shanghai 200240, China
Abstract:The performance of pulsed plasma thruster(PPT) is influenced by electric and structural parameters.For the low thrust efficiency of pulsed plasma thruster,the correlation between the designing(parameters) and performance was studied through theoretical analysis and experimental investigation.The(result) shows that the thrust and discharge current are closely related.The change of the electrode gap and discharge energy in pulsed plasma thruster will influence the thrust and discharge current significantly.The experimental result implies considerable information to the design of an optimized thruster.
Keywords:pulsed plasma thruster  specific impulse  thrust  impulse bit
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