| 高温树脂基复合材料在超声速导弹弹体上的应用 |
| |
| 引用本文： | 刘萝威%曹运红.高温树脂基复合材料在超声速导弹弹体上的应用[J].宇航材料工艺,2002,32(5):15-19. |
| |
| 作者姓名： | 刘萝威%曹运红 |
| |
| 作者单位： | 1. 北京动力机械研究所,北京,100074
2. 北京海鹰科技情报研究所,北京,100074 |
| |
| 摘 要： | 描述了超声速导弹弹体的热环境，高温树脂基复合材料基体候选树脂，重点介绍了双马来酰亚胺，聚酰亚胺树脂和氰酸酯的性能及最新进展，最后描述了高温树脂基复合材料在超声速度导弹弹体上的应用研究。
|
| 关 键 词： | 树脂基复合材料 超声速导弹 双马来酰亚胺 聚酰亚胺树脂 氰酸酯 材料性能 |
High-temperature Resistant Resin Matrix Composite Applications to Supersonic Missile Airframes |
| |
| Liu Luowei.High-temperature Resistant Resin Matrix Composite Applications to Supersonic Missile Airframes[J].Aerospace Materials & Technology,2002,32(5):15-19. |
| |
| Authors: | Liu Luowei |
| |
| Institution: | Liu Luowei ( Research Institute of Beijing Power Machine Beijing 100074 ) Cao Yunhong ( Beijing Sea Eagle Scientific & Technological Information Institute Beijing 100074 ) |
| |
| Abstract: | Some high temperature resistant composites with resin matrixes of bismaleimide(BMI), polyimide(PI) resins and cyanate ester(CE) for supersonic air intercept missile (AIM) airframes are introduced.Applications of the composites to supersonic missile airframes are reviewed, and their properties and latest development are presented with emphases. |
| |
| Keywords: | Missile airframe Resin matrix composite Supersonic missile Bismaleimide(BMI) Polyimide(PI) resin Cyanate ester(CE) |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《宇航材料工艺》浏览原始摘要信息 |
| 点击此处可从《宇航材料工艺》下载免费的PDF全文 |
