Investigation of aluminium Whipple Shield response to hypervelocity impacts close to ballistic limit between 2.5 and 5 km/s

射弹 超高速 弹道极限 护盾 背景(考古学) 光滑粒子流体力学 护盾 航程(航空) 机械 碎片 材料科学 航空航天工程 地质学 物理 工程类 气象学 复合材料 冶金 古生物学 热力学 岩石学
作者
Lorenzo Olivieri,Rannveig Marie Færgestad,Cinzia Giacomuzzo,Stefano Lopresti,G. Pitacco,Alessandro Francesconi,Tiziana Cardone,Jens Kristian Holmen,Tore Børvik
出处
期刊:Acta Astronautica [Elsevier BV]
卷期号:219: 41-47 被引量:2
标识
DOI:10.1016/j.actaastro.2024.03.009
摘要

For impact velocities larger than a threshold velocity of 3 km/s, aluminium Whipple Shields present an enhanced protection capability with respect to monolithic protections with the same areal density. In particular, in the range between 3 and 7 km/s the projectile partially fragments and melts after impacting the bumper; modelling this transition might be complex due to the high number of parameters affecting the collision. In particular, limited data is available in literature with a systematic evaluation of such parameters. In this context, a campaign of 22 experiments was performed to assess the response of aluminium Whipple Shields to normal impacts of aluminium projectiles in the transition range up to 5 km/s. In the tests, the projectile diameter was fixed at 2.9 mm and the bumper thickness and impact velocity were systematically varied respectively at 1, 1.5, and 2 mm and between 2.6 and 5 km/s. Collected data included high-velocity videos of the debris cloud generated by the impacts at both low resolution (for all shots) and high resolution (for 19 out of 22 tests); in addition, for 10 experiments high-resolution images of both the bumper and the wall were acquired after the tests. In this paper, the experimental campaign is described and the main collected results are presented; in particular, the influence of the different impact parameters is discussed. Experimental results are finally compared with numerical simulations conducted with a smoothed particle hydrodynamics method available in IMPETUS Solver.
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