| 导弹气动热防护材料设计 |
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| 引用本文： | 韩民,薛耀辉,李建生.导弹气动热防护材料设计[J].弹箭与制导学报,2006,26(3):59-60. |
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| 作者姓名： | 韩民 薛耀辉 李建生 |
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| 作者单位： | 中国兵器工业第203研究所,西安710065 |
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| 摘 要： | 以低温消融吸热／隔热机理为理论指导。研究一种特定耐热等级的气动热防护材料。通过配方设计。确定以环氧改性有机硅树脂为基体。以硼酸盐等为体质填料，按一定配比配制一种新型气动热防护涂料。试验证明，该涂料制备的气动热防护涂层具有良好的热防护性能，涂层在试验过程中形态未发生破坏。
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| 关 键 词： | 低温消融吸热／隔热机理 气动热防护涂料 配方设计 |
| 收稿时间： | 2005-11-29 |
| 修稿时间： | 2005年11月29 |
The Design of an Aero-dynamic Heat-resistant Material for Missile |
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| HAN Min,XUE Yao-hui,LI Jian-sheng.The Design of an Aero-dynamic Heat-resistant Material for Missile[J].Journal of Projectiles Rockets Missiles and Guidance,2006,26(3):59-60. |
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| Authors: | HAN Min XUE Yao-hui LI Jian-sheng |
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| Abstract: | According to the low temperature melting decalescence/heat insulation mechanism, a given grade aero-dynamic heat-resistant coating was studied in this paper. Based on analysis and test, the silicone matrix resins modified by epoxy and borate etc was selected, which were confected an aero-dynamic heat-resist coating. The coating owns excellent performance and its shape was hold in the test. |
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| Keywords: | low temperature melting decalescence/heat insulation aero-dynamic heat-resistant coating fill design |
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