20cm氙离子推力器性能扩展研究  

Research of Improvement Performance for 20cm Xenon Ion Thruster

作　　者：郑茂繁[1] 张天平[1] 孟伟[1] 李兴坤[1] 梁凯[1] 

机构地区：[1]兰州空间技术物理研究所真空技术与物理国家级重点实验室,甘肃兰州730000

出　　处：《推进技术》2015年第7期1116-1120,共5页Journal of Propulsion Technology

基　　金：真空低温技术与物理国家级重点实验室基金项目(9140C550206130C55003)

摘　　要：为了满足未来深空探测任务的需求,在20cm氙离子推力器的技术基础上,对其性能进行扩展提升研究,将推力提高50%,使推力由原来的40m N提高到60m N。通过对离子推力器工作参数的分析与研究,确定了离子推力器60m N推力模式的工作参数,并进行了优化实验。结果表明:性能扩展的20cm氙离子推力器推力提高到60m N,比冲提高到3500s,效率也提高到65%,并能够在40m N和60m N二种推力模式下工作。通过对2台推力器的组合,能够实现40,60,80,100,120m N五种推力工作模式。In order to meet the demand of deep space exploration,study was carried out based on the heritage of 20 cm Xenon Ion Thruster to enhance its performance. Thrust increased from 40 m N to 60 m N,which is improved by 50%. The operating parameters at 60 m N were finalized by the study and analysis and optimization with experiments. The results show that the thrust is extended to 60 m N,and specific impulse increases to 3500 s. Meanwhile efficiency is improved to 65%. After performance improvement,the thruster can be operated in 2 operating modes which are 40 m N and 60 m N,respectively. In addition,it is achievable for 40 m N,60 m N,80 m N,100 m N and120 m N 5 operating modes by combination of two thrusters,which can be adopted for deep space exploration.

关 键 词：电推进 离子推力器 性能扩展 研究 

分 类 号：V439.1[航空宇航科学与技术—航空宇航推进理论与工程]