| 导弹与固体火箭-冲压组合发动机协调设计 |
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| 引用本文： | 汪家芸,张振鹏,曲志强.导弹与固体火箭-冲压组合发动机协调设计[J].航空学报,1988,9(2):25-34. |
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| 作者姓名： | 汪家芸 张振鹏 曲志强 |
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| 作者单位： | 北京航空学院
(汪家芸，张振鹏)，北京航空学院(曲志强) |
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| 摘 要： | 本文综合导弹和固冲组合发动机的相互影响,提出了导弹与固冲组合发动机的协调设计方法。文中选取导弹发射重量和理论脱靶量为设计指标,应用多目标数学规划确定导弹总体参数和固冲发动机结构面积比。本文所用方法及程序可用于方案论证和改型研宄。
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| 收稿时间： | 1987-03-10; |
THE INTEGRATED DESIGN OF MISSILE WITH SOLID ROCKET -RAMJET COMBINATION |
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| Wang Jiayun,Zhan Zhangpeng and Qu Ziqiang.THE INTEGRATED DESIGN OF MISSILE WITH SOLID ROCKET -RAMJET COMBINATION[J].Acta Aeronautica et Astronautica Sinica,1988,9(2):25-34. |
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| Authors: | Wang Jiayun Zhan Zhangpeng and Qu Ziqiang |
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| Institution: | Beijing Institute of Aeronautics and Astronautics |
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| Abstract: | The present paper describes the interaction of the missile with the solid rocket-ramjet.A method for integrated design is also prenseted. In this paper the missile launching weight and the theoretical miss distance are taken as design criteria. The principal missile parameters and the area ratios of the rocket-ramjet structure can be determined by applying the multi-objective programming theory.The method and program developed in this study can de used for missile Conceptual design and for further design modification. |
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| Keywords: | missile solid rocket motor ramjet engine composite engine design |
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