| 高压强固体火箭发动机性能/成本优化设计 |
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| 引用本文： | 李晓斌,解红雨,青龙,张为华,陈雅琴,孙兵.高压强固体火箭发动机性能/成本优化设计[J].固体火箭技术,2004,27(1):16-19. |
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| 作者姓名： | 李晓斌 解红雨 青龙 张为华 陈雅琴 孙兵 |
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| 作者单位： | 1. 国防科技大学航天与材料工程学院,长沙,410073
2. 中国航天科工集团公司六院,呼和浩特,010000 |
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| 摘 要： | 建立了翼柱形装药固体火箭发动机在高工作压强下的性能、成本计算模型。采用混合编码遗传算法进行了性能/成本优化设计。所得优化设计结果表明，按费用优化设计技术可行，可为高压强固体火箭发动机方案设计提供依据。
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| 关 键 词： | 高压强固体火箭发动机 工作性能 成本 优化设计 遗传算法 |
| 文章编号： | 1006-2793(2004)01-0016-04 |
| 修稿时间： | 2003年10月8日 |
Optimization design of performance and cost for high-pressure solid rocket motors |
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| LI Xiao-bin,XIE Hong-yu,QING Long,ZHANG Wei-hua,CHEN Ya-qin,SUN Bing//. College of Aerospace and Material Engineering,National Univ. of Defense Technology,Changsha,China.Optimization design of performance and cost for high-pressure solid rocket motors[J].Journal of Solid Rocket Technology,2004,27(1):16-19. |
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| Authors: | LI Xiao-bin XIE Hong-yu QING Long ZHANG Wei-hua CHEN Ya-qin SUN Bing// College of Aerospace and Material Engineering National Univ of Defense Technology Changsha China |
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| Institution: | LI Xiao-bin~1,XIE Hong-yu~1,QING Long~1,ZHANG Wei-hua~1,CHEN Ya-qin~2,SUN Bing~2//1. College of Aerospace and Material Engineering,National Univ. of Defense Technology,Changsha410073,China, 2.The Sixth Research Academy of CASIC,Huhhot010000,China. |
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| Abstract: | The performance and cost calculation models of the high-pressure solid rocket motor with finocyl grain were set up and the performance and cost optimization design organized by using composite binary-coded and real-coded genetic arithmetic. The optimization results show that the optimization design to cost is technologically feasible and the optimization result can give directions to preliminary design of high-pressure solid rocket motors. |
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| Keywords: | solid propellant rocket engine high pressure cost model genetic arithmetic optimization design |
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