An Experimental Study of High-Velocity Impact on Aluminum Foam Composite Shield Structure

2013 ◽  
Vol 690-693 ◽  
pp. 20-24
Author(s):  
Qing Zhen Li ◽  
Zhong Hua Du ◽  
Kang Kang Wang

To study spacecraft shield structure against hypervelocity impact of space debris and its protective performances, 25mm ballistic gun launching 12.7mm cylindrical debris is selected against Aluminum foam composite structure at high speed. Based on the experimental results and analyze the effects of Aluminum foam protective structure with different combinations, the result is that protective effects with Aluminum foam in front of glass fiber is better.

2017 ◽  
Vol 203 ◽  
pp. 100-102 ◽  
Author(s):  
Xiaolong Liang ◽  
Hongjie Luo ◽  
Yongliang Mu ◽  
Linli Wu ◽  
Hao Lin

2007 ◽  
Vol 63 (1) ◽  
pp. 178-191 ◽  
Author(s):  
Masuhiro BEPPU ◽  
Koji MIWA ◽  
Tomonori OHNO ◽  
Masanori SHIOMI

2016 ◽  
Vol 50 ◽  
pp. 245-255 ◽  
Author(s):  
Ali Taherkhani ◽  
Mojtaba Sadighi ◽  
Ali Sadough Vanini ◽  
Mohsen Zarei Mahmoudabadi

2006 ◽  
Vol 321-323 ◽  
pp. 654-657 ◽  
Author(s):  
Do Yeon Hwang ◽  
Akira Shimamoto ◽  
Daiju Numata ◽  
Takamase Kikuchi ◽  
Kazuyoshi Takayama

In this study, dynamic penetration phenomena of high-velocity impact of magnesium alloy were investigated. The surface hardness of magnesium alloy (AZ31B-O) and the heat-treated magnesium alloy (AZ31B-200°C, AZ31B-300°C, and AZ31B-430°C) were examined using Micro Vickers, and the influence of the heat treatment temperature was observed. We analyzed the metal organization using a microscope. We also used a ballistic range (two-stage light gas gun), and the test specimens were set at 0°obliquity at room temperature. A high-speed camera allowed us to capture and analyzed the dynamic penetration phenomena of the test specimen.


Author(s):  
Erkai Watson ◽  
Nico Kunert ◽  
Robin Putzar ◽  
Hans-Gerd Maas ◽  
Stefan Hiermaier

Abstract Hypervelocity impacts (HVI) often cause significant fragmentation to occur in both target and projectile materials, and is often encountered in space debris and planetary impact applications [1]–[5]. In this paper, we focus on determining the individual velocities and sizes of fragments tracked in high-speed images. Inspired by velocimetry methods such as Particle Image Velocimetry (PIV) [6] and Particle Tracking Velocimetry (PTV) [7] and building on past work [8], we describe the setup and algorithm used for measuring fragmentation data.


2018 ◽  
Author(s):  
Yu. Yu. Emurlaeva ◽  
I. A. Bataev ◽  
S. Tanaka ◽  
I. V. Ivanov ◽  
E. I. Tkachenko

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