Corrugation Stuffed Shield for Spacecraft and Its Performance

A corrugation stuffed shield system protecting spacecrafts against meteoroid and orbital debris (M/OD) is presented. The semi-empirical ballistic limit equations (BLEs)defining the protection capability of the shield system are given, an d the shielding performance is also discussed. The corrugation stuffed shield (CSS) is more effective than stuffed Whipple shield for M/OD protection,and its shielding performance will be improved significantly as increasing the impact angle. Orbital debris up to 1cm in diameter can be shielded effectively as increasing the impact angle to 25° at the corrugated angle of 30°. The results are significant to spacecraft design.

作 者： LIU You-ying WANG Hai-fu   作者單位： State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081,China  刊 名： 北京理工大學(xué)學(xué)報(bào)（英文版）  EI 英文刊名： JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY  年，卷(期)： 2006 15(4)  分類(lèi)號(hào)： V414  關(guān)鍵詞： spacecraft   shield system   orbital debris   meteoroid  

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