| BTT－固冲导弹总体一体化设计方法研究 |
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| 引用本文： | 高鹏飞,孙杏初,等.BTT－固冲导弹总体一体化设计方法研究[J].战术导弹技术,1991(4):17-25. |
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| 作者姓名： | 高鹏飞 孙杏初 |
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| 作者单位： | 北京航空航天大学
(高鹏飞，孙杏初)，北京航空航天大学(白文林) |
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| 摘 要： | 从BTT-固冲导弹的特点:固冲发动机、导弹外形及控制系统具有强耦合的性质出发,分析了相互影响因素及建立计算模型时的特点。提出了一种BTT-固冲导弹总体一体化设计方法。
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| 关 键 词： | 导弹 总体结构 固冲发动机 转弯飞行 设计 计算机辅助设计 |
A STUDY OF DESIGN PROCEDURE FOR BANK-TO-TURN MISSILE WITH INTEGRATED ROCKET RAMJET |
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| Gao Pengfei Sun Xingchu Bai Wenlin Beijing University of Aeronautics and Astronautics.A STUDY OF DESIGN PROCEDURE FOR BANK-TO-TURN MISSILE WITH INTEGRATED ROCKET RAMJET[J].Tactical Missile Technology,1991(4):17-25. |
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| Authors: | Gao Pengfei Sun Xingchu Bai Wenlin Beijing University of Aeronautics and Astronautics |
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| Affiliation: | Gao Pengfei Sun Xingchu Bai Wenlin Beijing University of Aeronautics and Astronautics |
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| Abstract: | Bank-to-Turn missile with integrated rocket ramjet has a character that engine, airframe and control system are strongly coupled. The mutual effecting factors and the special problems of setting up the mathematical model have been analysed. At last, a design procedure of Bank-to-Turn missile with integrated rocket ramjet is presented. |
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| Keywords: | Missile Design Integrated rocket ramjet ~*Bank-to-Turn |
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