感应式脉冲等离子体推力器技术综述  

Review of Technology and Research on Inductive Pulsed Plasma Thruster

作　　者：程谋森[1] 李小康[1] 车碧轩 郭大伟[1] CHENG Mousen LI Xiaokang CHE Bixuan GUO Dawei(National University of Defense Technology, Changsha 410073, China)

机构地区：[1]国防科技大学,长沙410073

出　　处：《空间控制技术与应用》2017年第5期1-6,21,共7页Aerospace Control and Application

基　　金：国家自然科学基金资助项目(51306203)

摘　　要：综合文献及作者研究实践,介绍了感应式脉冲等离子体推力器的原理和特点.从国外研究机构与项目、推力器组件和系统集成实验、工作机理数值仿真等方面,总结和评述了达到的技术状态与认识.最后梳理了面临的技术挑战,提出了可能的解决途径.The principle and virtues of the concept of inductive pulsed plasma thruster （IPPT） are intro- duced based on the interpretation of extensive literatures and expertise from experience. The state-of-the- art for IPPT attained by oversea and domestic researchers are concluded by reviewing the institutes and programs, components and system integration experiments, modeling and numerical simulation. The tech- nical challenges are identified and the approaches are proposed.

关 键 词：气体感应放电 电流片 脉冲等离子体推力器 磁推进 

分 类 号：V439[航空宇航科学与技术—航空宇航推进理论与工程]