| 固体火箭发动机纤维缠绕壳体贮存性能试验研究 |
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| 引用本文： | 徐金洲,谢丽宽,许涛,邢耀国.固体火箭发动机纤维缠绕壳体贮存性能试验研究[J].海军航空工程学院学报,2008,23(6):619-622. |
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| 作者姓名： | 徐金洲 谢丽宽 许涛 邢耀国 |
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| 作者单位： | 西安120信箱海军代表室,西安,710025;海军航空工程学院飞行器工程系,山东,烟台,264001 |
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| 摘 要： | 通过设计、制作Ф200缩比模拟试验件，对缩比模拟试验件进行加速老化，然后对加速老化试验前后的试验件进行外气密试验、轴压破坏试验、内压爆破试验，探究复合材料壳体的贮存使用性能。
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| 关 键 词： | 固体火箭发动机 纤维 壳体 贮存 |
Experimental Investigation on the Storage Life of Filament-Wound Composite Case for Solid Rocket Motor |
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| XU Jin-zhou,XIE Li-kuan,XU Tao and XING Yao-guo.Experimental Investigation on the Storage Life of Filament-Wound Composite Case for Solid Rocket Motor[J].Journal of Naval Aeronautical Engineering Institute,2008,23(6):619-622. |
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| Authors: | XU Jin-zhou XIE Li-kuan XU Tao and XING Yao-guo |
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| Institution: | XU Jin-zhou1,XIE Li-kuan1,XU Tao1,XING Yao-guo2 (1.Naval Representatives Office in Xi\'an 120P.O.Box,Xi\'an 710025,China,2.Department of Airborne Vehicle Engineering,NAAU,Yantai Sh,ong 264001,China) |
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| Abstract: | The Ф200 specimen part was designed and manufactured, then was studied by accelerated aging test. The aging specimen was tested by external gas proof test, bulking test and the internal burst test. The composite case storage life was predicted. |
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| Keywords: | solid rocket motor filament case storage |
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