激光-电场混合推进技术发展现状  

Review of laser-electric hybrid propulsion technology

作　　者：段卜仁 马腾飞 王科伟 李彤 黄金红 徐宁 代俊 Duan Buren;Ma Tengfei;Wang Kewei;Li Tong;Huang Jinhong;Xu Ning;Dai Jun(Liaoning North Huafeng Special Chemical Limited Company,Fushun 113003,China;Key Laboratory of Aerospace-grade Initiating Explosive Devices,Liaoning Province,Fushun 113003,China;School of Mechatronical Engineering,Beijing Institute of Technology,Beijing 100081,China;The Fourth Military Representative Office of the Air Force Equipment Department in Shenyang,Shenyang 110034,China;Military Representative Office of the Army Equipment Department in Fushun,Fushun 113122,China)

机构地区：[1]辽宁北方华丰特种化工有限公司,抚顺113003 [2]辽宁省宇航级火工品重点实验室,抚顺113003 [3]北京理工大学机电学院,北京100081 [4]空军装备部驻沈阳地区第四军事代表室,沈阳110034 [5]陆军装备部驻抚顺地区军事代表室,抚顺113122

出　　处：《战术导弹技术》2024年第4期103-114,共12页Tactical Missile Technology

基　　金：国家自然科学基金(52275084)。

摘　　要：激光推进和电推进都具备各自独特的优势,将激光推进和电推进结合,能够实现两种推进技术优势互补、缺点共同消除的目的。针对激光-电场混合推进技术进行了系统介绍,总结了推力器的结构设计、推进剂研制、测试方法等内容。结合综述内容,得到如下结论:激光-电场混合推进技术具有比冲大、体积小等特点,能够为微纳卫星姿态调整提供动力支持;其中,静电场耦合方案的结构简单,但是推力较小,目前仅停留在理论研究阶段,未形成原理样机,工程应用前景有限;电磁场耦合方案的推力性能更为优越,系统集成难度低,未来应致力于减小系统质量和体积,集成激光器、推力器、控制系统等模块,以实现星载推力器的应用。Both laser propulsion and electric propulsion have unique advantages.Combining laser propulsion and electric propulsion can realize the purpose of complementary advantages and eliminating disadvantages.The laser-electric hybrid propulsion technology is systematically reviewed and the structural design,propellant development and testing methods of thruster are summarized.Based on the review,the following conclusions are drawn.Laser-electric hybrid propulsion technology is characterized by high specific impulse and small volume,which is perceived as the power support for nanosat attitude control.Wherein the electrostatic coupling scheme has a simple structure but the thrust is relatively small.At present,it remains in the theoretical stage and the prototype has not be formed,which limits its engineering prospect.The electromagnetic coupling scheme has superior thrust performance and low integration difficulty.In the future,the system mass and volume should be reduced and the modules such as laser,thruster and control system should be integrated to realize the application of space-borne thrusters.

关 键 词：激光-电场混合推进技术 静电式耦合 电磁式耦合 推进剂 

分 类 号：V43[航空宇航科学与技术—航空宇航推进理论与工程]