| 全复合材料发动机壳体与喷管连接结构 |
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| 引用本文： | 华增功.全复合材料发动机壳体与喷管连接结构[J].固体火箭技术,1992(4):8-14. |
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| 作者姓名： | 华增功 |
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| 作者单位： | 四院四十一所 西安710000 |
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| 摘 要： | 结合国外先进固体发动机纤维缠绕壳体与喷管连接的技术,分析了实现全复合材料固体发动机壳体-喷管的连接方式,技术途径,并提出了有关设计参数,可供设计人员参考.
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| 关 键 词： | 火箭发动机 纤维缠绕壳体 喷管 |
JOINTING BETWEEN CHAMBER AND NOZZLE OF AN ALL-COMPOSITE SOLID ROCKET MOTER |
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| Hua Zenggong.JOINTING BETWEEN CHAMBER AND NOZZLE OF AN ALL-COMPOSITE SOLID ROCKET MOTER[J].Journal of Solid Rocket Technology,1992(4):8-14. |
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| Authors: | Hua Zenggong |
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| Abstract: | Based on the foreign jointing technique between the advanced filament-wound chamber and nozzle, the paper analyzes the jointing modes between chamber and nozzle of an all-composite solid rocket motor and technical approaches, and puts forward the relevant design parameters to give a refrence to designers. |
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| Keywords: | Solid rocket engine Filament-wound chamber C/C nozzle Mcchanical jointing Design |
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