用于空间站的螺旋波等离子体推进研究进展  

Research Progress of Helicon Plasma Thruster for Space Station

作　　者：夏广庆[1,2] 张军军 陈留伟 余水淋 刘佳 杭观荣 XIA Guangqing;ZHANG Junjun;CHEN Liuwei;YU Shuilin;LIU Jia;HANG Guanrong(State Key Laboratory of Structural Analysis for Industrial Equipment,Dalian University of Technology,Dalian 116024,China;Key Laboratory of Advanced Technology for Aerospace Vehicles of Liaoning Province,Dalian University of Technology,Dalian 116024,China;Shanghai Institute of Space Propulsion,Shanghai 201112,China)

机构地区：[1]大连理工大学工业装备结构分析国家重点实验室,大连116024 [2]大连理工大学辽宁省空天飞行器前沿技术重点实验室,大连116024 [3]上海空间推进研究所,上海201112

出　　处：《载人航天》2019年第2期265-270,共6页Manned Spaceflight

基　　金：国家自然科学基金(11675040);载人航天预先研究项目(050303);辽宁省自然科学基金(201602175)

摘　　要：针对如何利用空间站中气态物质作为电推力器的推进工质,产生空间站姿轨控所需动力,提高空间站物质利用率以及降低空间站长期运行成本,介绍了螺旋波等离子体推力器的工作原理及性能特点,结合气态物质的主要成分,综述了国内外对于复杂工质螺旋波等离子体推力器的最新研究进展,讨论了复杂工质螺旋波等离子体推力器的关键技术和研究方法,对复杂气体用于螺旋波等离子体推力器的应用进行了展望。To improve the space station material utilization rate and reduce the long-term operation cost of the space station,the working principle and the performance characteristics of helicon plasma thruster(HPT)were introduced aiming at the efficient use of the gaseous substances in the space station as the propellant of the electric thruster to generate the power required for the space station attitude control.The main components of gaseous materials were introduced and the latest research progress of complex propellant HPT was reviewed.Then the key technologies and research methods of complex propellant HPT were discussed.In the end,the application of complex propellant for helicon plasma thrusters was prospected.

关 键 词：空间站 电推进 螺旋波等离子体推力器 复杂工质 等离子体诊断 

分 类 号：V439.4[航空宇航科学与技术—航空宇航推进理论与工程]