液体工质激光推进冲量耦合系数实验测试

推进技术 ›› 2007, Vol. 28 ›› Issue (5): 526-529.

液体工质激光推进冲量耦合系数实验测试

李修乾,洪延姬,崔村燕,文明,何国强

西北工业大学航天工程学院陕西西安710072;装备指挥技术学院北京101416;装备指挥技术学院北京101416;西北工业大学航天工程学院陕西西安710072;装备指挥技术学院北京101416;装备指挥技术学院北京101416;西北工业大学航天工程学院陕西西安710072

发布日期:2021-08-15
基金资助:
国家“九七三”项目(61328)

Measurements of impulse coupling coefficient for laser propulsion with liquid propellants

Coll.of Astronautics,Northwestern Polytechnical Univ.,Xi’an 710072,China;Inst.of Equipment Command and Technology,Beijing 101416,China;Inst.of Equipment Command and Technology,Beijing 101416,China;Coll.of Astronautics,Northwestern Polytechnical Univ.,Xi’an 710072,China;Inst.of Equipment Command and Technology,Beijing 101416,China;Inst.of Equipment Command and Technology,Beijing 101416,China;Coll.of Astronautics,Northwestern Polytechnical Univ.,Xi’an 710072,China

Published:2021-08-15

摘要/Abstract

摘要： 在成功研制液体工质注入系统的基础上,以脉冲式CO2激光器为光源,将雾化水滴用作工质,进行了激光推进性能实验测试研究。实验发现水工质激光推进冲量耦合系数较大气吸气模式获得了较为明显的提高,达到了50×10-5N.s.J-1左右。与国内外相关实验结果进行了对比分析,讨论了提高液体工质激光推进性能参数的方法。

关键词: 激光推进;工质注入系统+;雾化;耦合系数

Abstract: A CO2 laser was employed to ablate water droplets provided by a pulsed liquid propellant feeding system.Experimental results indicate that momentum coupling coefficient Cm is increased to 50×10-5N·s·J-1,which is higher than that of air-breathing mode laser propulsion.The measurement data were compared to the results of other authors.The way to improve the performance parameters of laser propulsion with liquid propellants was discussed.

Key words: Laser propulsion;Propellant feeding system+;Atomization;Coupling coefficient

李修乾,洪延姬,崔村燕,文明,何国强. 液体工质激光推进冲量耦合系数实验测试[J]. 推进技术, 2007, 28(5): 526-529.