2011
DOI: 10.1299/kikaic.77.4534
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Analysis of Shock Response for Satellite Separation

Abstract: When a satellite separates from the rocket in space, large shocks occur in the satellite's body structure. To evaluate * 原稿受付 2011 年 6 月 13 日 *1 正員,三菱電機 (株) 先端技術総合研究所(〒661-8661 兵庫県尼崎市塚口本町 8-1-1) *2 三菱電機 (株) 鎌倉製作所 *3 正員, (独) 宇宙航空研究開発機構

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