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激光-电磁复合推力器研究现状与展望
吴建军,欧阳,张宇,赵元政,李宇奇
国防科技大学 空天科学学院,湖南 长沙 410073
摘要:
激光-电磁复合推力器不仅具有比冲高和体积小的特点,还具有推力精准可控、工作稳定、抗干扰强以及效率高的优势,可为微纳卫星提供可靠的动力来源。本文对激光-电磁复合推力器的相关研究进行了较为全面的介绍,概述了此类推力器的基本原理与优势特征,重点总结了样机设计、数值模型与推进剂研制三部分内容的研究进展,归纳了现有研究内容的关键问题。在此基础上,对激光-电磁复合推力器的进一步发展方向进行了展望。
关键词:  激光-电磁复合推力器  空间微推进技术  微纳卫星  数值模型  推进剂  综述
DOI:10.13675/j.cnki.tjjs.2208069
分类号:V439
基金项目:国家自然科学基金面上项目(11772354)。
Review and Prospect of Laser-Electric Hybrid Thruster
WU Jian-jun, OU Yang, ZHANG Yu, ZHAO Yuan-zheng, LI Yu-qi
College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China
Abstract:
Laser-electric hybrid thrusters are expected to achieve the higher specific impulse and the smaller volume, and they also have the advantages of accurate and controllable thrust, stable operation, strong anti-interference and high efficiency, which is now perceived as an advanced propulsion system to support the precise maneuvering of microsatellites. This paper presented a comprehensive review to the related research of laser-electric hybrid thrusters, summarized the basic principle and advantages of this kind of thruster, focused on the research progress of prototype design, numerical model and propellant development, and included the key problems of the existing researches. On the basis, the further key directions of laser-electric hybrid thrusters are prospected to provide reference for the research and application of space propulsion technology, and promote the further development of Chinese electric propulsion industry.
Key words:  Laser-electric hybrid thruster  Space micro-propulsion technology  Microsatellites  Numerical model  Propellant  Review