首页 | 本学科首页   官方微博 | 高级检索  
     检索      

激光烧蚀微推进技术研究现状及展望
引用本文:叶继飞,洪延姬,李南雷,周伟静,常浩,邢宝玉.激光烧蚀微推进技术研究现状及展望[J].空间控制技术与应用,2021,47(4):1-9.
作者姓名:叶继飞  洪延姬  李南雷  周伟静  常浩  邢宝玉
作者单位:航天工程大学宇航科学与技术系激光推进及其应用国家重点实验室
摘    要:激光烧蚀微推进技术是空间微推进技术中的一种,是基于激光推进原理的电推进技术,可用于微纳卫星姿态与轨道控制.回顾激光烧蚀微推进技术发展的历程,简述其推进原理涉及的基本理论,对激光烧蚀微推进领域涉及的技术方向研究现状进行探讨,对相关各种类型微推力器进行对比分析,结合激光烧蚀微推进技术的特点,分析激光烧蚀微推进技术发展趋势,并给出了发展建议.

关 键 词:激光烧蚀  微推进  微纳卫星  推进性能  

Status and Prospect of Laser Ablation Micro Propulsion Technology
YE Jifei,HONG Yanji,LI Nanlei,ZHOU Weijing,CHANG Hao,XING Baoyu.Status and Prospect of Laser Ablation Micro Propulsion Technology[J].Aerospace Contrd and Application,2021,47(4):1-9.
Authors:YE Jifei  HONG Yanji  LI Nanlei  ZHOU Weijing  CHANG Hao  XING Baoyu
Abstract:Laser ablation micro propulsion technology is one of the space micro propulsion technologies. It is a kind of electric propulsion technology based on the principle of laser propulsion. It can be used for micro nanosatellite attitude and orbit control. In this paper, the development of laser ablation micro propulsion technology is reviewed. The basic theory is briefly described. The research status is discussed. Various types of micro thrusters are compared and analyzed. Combined with the characteristics of laser ablation micro propulsion technology, the development trend is analyzed, and suggestions are given for reference.
Keywords:laser ablation  micro propulsion  micro nanosatellite  propulsion performance  
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《空间控制技术与应用》浏览原始摘要信息
点击此处可从《空间控制技术与应用》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号