首页 | 本学科首页   官方微博 | 高级检索  
     

纳秒激光烧蚀液态工质冲量耦合特性研究
引用本文:叶继飞,洪延姬,李南雷.纳秒激光烧蚀液态工质冲量耦合特性研究[J].红外与激光工程,2015,44(1):102-106.
作者姓名:叶继飞  洪延姬  李南雷
作者单位:1.装备学院激光推进及其应用国家重点实验室,北京101416
摘    要:激光微推进技术是利用激光与物质相互作用产生的力学效应实现推进的一种新的激光动力的电推进技术。液态工质是激光微推进工质选择的最新热点,其与激光相互作用所形成的冲量耦合特性决定了液态工质激光微推进性能的好坏。利用激光干涉差动测量微小冲量的扭摆装置,以聚叠氮缩水甘油醚(GAP)、单组元凝胶推进剂(单推-3)和甘油为工质,测量注入不同激光能量条件下,所形成的冲量和冲量耦合系数大小,进而针对冲量耦合性能较好的GAP 工质,测量了比冲和烧蚀效率。结果表明:液态GAP 冲量耦合特性较好,冲量耦合系数一般在500 uN/W 以上,最高可达1 493.0 uN/W,但是,比冲和烧蚀效率较低,比冲最高仅为140 s,烧蚀效率为37.6%。

关 键 词:激光微推进    比冲    冲量耦合系数    烧蚀效率
收稿时间:2014-05-11

Impulse coupling performance of liquid propellant with ns laser micro ablation
Ye Jifei,Hong Yanji,Li Nanlei.Impulse coupling performance of liquid propellant with ns laser micro ablation[J].Infrared and Laser Engineering,2015,44(1):102-106.
Authors:Ye Jifei  Hong Yanji  Li Nanlei
Affiliation:1.State Key Laboratory of Laser Propulsion & Application,Academy of Equipment,Beijing 101416,China
Abstract:Laser micro-propulsion is a new laser-powered electric propulsion technology, which uses the mechanical effect generated by laser-matter interaction. Liquid as propellant is the latest points of interest. Impulse coupling characteristics of interaction between liquid and laser decided the merits of propulsive performance. Torsion pendulum device was used to measure the micro-impulse. Monopropellant gel propellant, GAP and glycerol were used as propellant. Impulse and impulse coupling coefficient were measured under different laser energy. GAP obtained higher impulse coupling coefficient and was further studied. The results show that impulse coupling characteristics of GAP are better. Impulse coupling coefficient is generally greater than 500 uN/W, maximum is 1 493.0 uN/W. However, specific impulse and ablation efficiency are relatively low. Maximum specific impulse is 140 s; maximum ablation efficiency is 37.6%.
Keywords:laser micro propulsion  specific impulse  impulse coupling coefficient  ablation efficiency
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《红外与激光工程》浏览原始摘要信息
点击此处可从《红外与激光工程》下载全文
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