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密度梯度薄板超高速撞击特性的实验研究
引用本文:侯明强,龚自正,徐坤博,郑建东,曹燕,牛锦超. 密度梯度薄板超高速撞击特性的实验研究[J]. 物理学报, 2014, 63(2): 24701-024701. DOI: 10.7498/aps.63.024701
作者姓名:侯明强  龚自正  徐坤博  郑建东  曹燕  牛锦超
作者单位:1. 中国空间技术研究院北京卫星环境工程研究所, 可靠性与环境工程技术重点实验室, 北京 100094;2. 中国空间技术研究院通信卫星事业部, 北京 100094
基金项目:国家重点基础研究发展计划(批准号:2010CB731600)和国家国防科工局空间碎片专项研究计划(批准号:KJSP06209,K0202210)资助的课题.
摘    要:以二级轻气炮作为加载手段,在撞击速度范围为4.0—7.0 km/s内获得了Ti6Al4V/Ly12 Al/聚酰胺纤维密度梯度薄板的穿孔特性、验证板损伤特性和弹道极限特性.与Ly12 Al薄板的相应实验结果的对比显示,在相同撞击速度下,该密度梯度薄板的穿孔直径更大,且随撞击速度的增大而增加;其验证板上的撞击坑尺寸小,且随撞击速度的增大而减小;其弹道极限比Ly12 Al薄板的弹道极限高50%以上.分析认为,超高速撞击下Ti6Al4V/Ly12 Al/聚酰胺纤维密度梯度薄板中高阻抗的Ti6Al4V产生的峰值冲击压力比Ly12 Al薄板的峰值冲击压力高,这增强了对弹丸的破碎能力;而其中的聚酰胺纤维层延长了冲击波在薄板中的传播时间,增大了冲击波的耗散,使撞击过程中转化的不可逆功增多,从而消耗了弹丸更多的动能.使用这种密度梯度材料作为防护屏具有很好的抗撞击能力,在航天器空间碎片防护工程应用中具有很大的潜力.

关 键 词:超高速撞击  密度梯度材料  弹道极限  空间碎片
收稿时间:2013-07-15

Experimental study on hypervelocity impact characteristics of density-grade thin-plate
Hou Ming-Qiang,Gong Zi-Zheng,Xu Kun-Bo,Zheng Jian-Dong,Cao Yan,Niu Jin-Chao. Experimental study on hypervelocity impact characteristics of density-grade thin-plate[J]. Acta Physica Sinica, 2014, 63(2): 24701-024701. DOI: 10.7498/aps.63.024701
Authors:Hou Ming-Qiang  Gong Zi-Zheng  Xu Kun-Bo  Zheng Jian-Dong  Cao Yan  Niu Jin-Chao
Affiliation:1. Science and Technology on Reliability and Environment Engineering Laboratory, Beijing Institute of Spacecraft Environment Engineering, China Academy of Space Technology, Beijing 100094, China;2. Institute of Telecommunication Satellite, China Academy of Space Technology, Beijing 100094, China
Abstract:Hypervelocity impact (HVI) characteristics of Ti6Al4V/Ly12 Al/polyamide fibre density-grade thin-plate are investigated experimentally in a velocity range of 4.0–6.5 km/s by using two-stage light gas gun. The perforation in target, damage to witness wall, and ballistic limit curve are obtained and compared with those in the case of aluminum thin-plate. The results show that the diameter of the perforation hole is larger than that of aluminum thin-plate, the crater size in witness plate is smaller, and the ballistic limit curve is 50% larger than the latter. The analysis of shock wave propagation and the calculation of energy dissipation property in the density-grade thin-plate show that higher peak shock pressure is produced in it, and it has longer pressure duration time. Thus, more dissipation energy is consumed than in the case of aluminum thin-plate. So the density-grade thin-plate has a very good performance in withstanding HVI, and is promising in engineering application, e.g. protecting spacecraft from HVI of micro-meteoroid and orbital debris.
Keywords:hypervelocity impact  density-grade material  ballistic limit  space debris
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