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

Qing Zhen Li; Zhong Hua Du; Kang Kang Wang

doi:10.4028/www.scientific.net/AMR.690-693.20

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 690-693An Experimental Study of High-Velocity Impact on...

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

Abstract:

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.

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Periodical:

Advanced Materials Research (Volumes 690-693)

Pages:

20-24

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.690-693.20

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Online since:

May 2013

Authors:

Qing Zhen Li, Zhong Hua Du, Kang Kang Wang

Keywords:

Aluminum Foam, Composite Shield Structure, Cylindrical Debris, High-Velocity Impact

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References

[1] Kiureghian A D, Geysekns P V, Khalessi M R,Probabilistic accessment of debris impact damage on orbital structures, J. International Journal of Impact Engineering. (1997) 571–588.

DOI: 10.1016/s0734-743x(96)00045-0

Google Scholar

[2] Lambert M, Hypervelocity impacts and damage laws, J. Advancement in Space Research.(1997) 369–378.

Google Scholar

[3] Whipple, F.L, Meteoritesand Space Travel, J.Astronomical Journal.52 (1947) 137.

Google Scholar

[4] Shao Xianzhong, Multi-layer composite protective structure of anti-penetration characteristics of hypervelocity debris, D.University of science and technology of China. (2009)

Google Scholar

[5] Yang Shaowei,Resistance to penetration performance of the new concrete composite protective layer, D.Harbin industrial university. (2009) 14–16.

Google Scholar