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作 者:潘越 曹金乐 郑永赞 杜宝盛 张景源 吴立志[1,2,3] 叶迎华 沈瑞琪[1,2,3] PAN Yue;CAO Jin-le;ZHENG Yong-zan;DU Bao-sheng;ZHANG Jing-yuan;WU Li-zhi;YE Ying-hua;SHEN Rui-qi(School of Chemistry and Chemical Engineering,Nanjing University of Science and Technology,Nanjing 210094,China;Micro-Nano Energetic Devices Key Laboratory of MIIT,Nanjing 210094,China;Institute of Space Propulsion,Nanjing University of Science and Technology,Nanjing 210094,China;State Key Laboratory of Laser Propulsion and Application,University of Space Engineering,Beijing 101416,China)
机构地区:[1]南京理工大学化学与化工学院,江苏南京210094 [2]微纳含能器件工业和信息化部重点实验室,江苏南京210094 [3]南京理工大学空间推进技术研究所,江苏南京210094 [4]航天工程大学激光推进及其应用国家重点实验室,北京101416
出 处:《推进技术》2023年第12期206-216,共11页Journal of Propulsion Technology
摘 要:为获得脉冲激光能量对含能液态工质推进性能的影响规律,通过基于激光器、高速相机、扭摆搭建的测试系统对二硝酰胺铵(ADN)基液体工质的吸收性能、烧蚀性能、推进性能进行了研究。结果表明:ADN基含能液体是一种理想的液体工质,吸收系数达354.05cm^(-1),吸收深度为28.24μm。在0~63.97mJ能量范围内,增大激光能量有利于提高ADN基液体工质的推进性能。在激光能量为63.97mJ时,ADN基液体工质的推进性能达到最优,对应的推进性能参数分别为:冲量53.31μN·s,冲量耦合系数0.8757mN·s·J^(-1),比冲281.59s,能量转化效率122.40%。In order to study the effects of the pulsed laser energy on the propulsion performance of liquid propellant,the absorption performance,ablation performance and propulsion performance of the ammonium dinit⁃ramide(ADN)-based propellant were tested by the systems based on laser,high-speed camera and torsion pen⁃dulum.The experimental results show that the ADN-based propellant is an ideal liquid working medium,with an absorption coefficient of 354.05cm^(-1) and an absorption depth of 28.24μm.In the energy range of 0~63.97mJ,la⁃ser energy is beneficial to improving the propulsion performance of ADN-based propellant.When the laser energy is 63.97mJ,the propulsion performance of ADN-based propellant reaches the best,with an impulse of 53.31μN·s,an impulse coupling coefficient of 0.8757mN·s·J^(-1),a specific impulse of 281.59s and an energy conversion efficiency of 122.40%.
关 键 词:激光烧蚀 微推进 含能液体 二硝酰胺铵(ADN) 能量转化效率
分 类 号:V439[航空宇航科学与技术—航空宇航推进理论与工程] TN249[电子电信—物理电子学]
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