Response of a Aluminum Honeycomb Subjected to Hypervelocity Impacts

被引：8

作者：

Nitta, Kumi ^{[1
]}

Higashide, Masumi ^{[1
]}

Kitazawa, Yukito ^{[2
,3
]}

Takeba, Atushi ^{[4
]}

Katayama, Masahide ^{[4
]}

Matsumoto, Haruhisa ^{[2
]}

机构：

[1] Japan Aerosp Explorat Agcy, Aerosp Res & Dev Directorate, Chofu, Tokyo, Japan

[2] Japan Aerosp Explorat Agcy, Aerosp Res & Dev Directorate, Tsukuba, Ibaraki, Japan

[3] IHI Corp, Aerosp Res & Dev Aeroengn & Space Operat, Koto Ku, Tokyo, Japan

[4] ITOCHU Technosolut, Sci & Engn Syst Div, Tokyo, Japan

来源：

PROCEEDINGS OF THE 12TH HYPERVELOCITY IMPACT SYMPOSIUM | 2013年 / 58卷

关键词：

Orbital Debris; Hydrucude AUTODYN; Twu-Stage Light Gas Gun; Numerical simulation; space craft;

D O I：

10.1016/j.proeng.2013.05.082

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

We investigated the effect of hypervelocity impacts of nticrometeoroids and small-scale orbital space debris (M/OD) on space structures by comparing numerical simulation results obtained using the At TODYN-2D hydrocode with the results of experiments using a two stage light gas gun. The response of an aluminum honeycomb structure to 6 km/s high-velocity impacts is shown and discussed. AUTODYN-2D, which is used for impact analysis of complex physical systems including fluid and solid materials, was used to simulate impacts at 2-15 km/s. Material models used in the simulation to allow investigation of phenomena over a wide range of impact velocities, including shock-induced vaporization, are also presented and discussed. (C) 2013 The Authors. Published by Elsevier Ltd.

引用

页码：709 / 714

页数：6

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