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首页> 外文期刊>日本航空宇宙学会論文集 >Deformation and Fracture of CFRP under Hyper-Velocity Impact Test Using Laser-Accelerated Flyer
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Deformation and Fracture of CFRP under Hyper-Velocity Impact Test Using Laser-Accelerated Flyer

机译:激光加速飞行器超高速冲击试验下CFRP的变形和断裂

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摘要

Using laser-accelerated Al flyers, we examined hyper-velocity impact tests of CFRP (carbon fiber reinforced plastics) laminates as a simulation of orbital debris impact. A short-pulsed intense laser beam can accelerate a small flyer as fast as LEO (low earth orbit) satellite velocity. We succeeded in observing the deformation and fracture processes of the CFRP targets with a high-speed framing camera. When the pulsed laser was set the single shot energy of 26.4 J. corresponding to Al flyer velocity 8.3 km/s, we observed that the fiber breakage at the back surface of the CFRP target occurred at about 500ns after the impact.
机译:使用激光加速的Al传单,我们检查了CFRP(碳纤维增强塑料)层压板的超高速冲击试验,以模拟轨道碎片撞击。短脉冲强激光束可以像LEO(低地球轨道)卫星速度一样快地加速小飞行器。我们使用高速取景相机成功观察了CFRP靶材的变形和断裂过程。当将脉冲激光设置为26.4 J.的单发能量(对应于Al飞行器速度8.3 km / s)时,我们观察到CFRP靶背面的纤维断裂发生在撞击后约500ns。

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