| 固体运载火箭弹道设计与优化 |
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| 引用本文： | 张嵩,黄坚定.固体运载火箭弹道设计与优化[J].固体火箭技术,1997,20(1):1-5. |
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| 作者姓名： | 张嵩 黄坚定 |
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| 作者单位： | 中国航天工业总公司四院四十一所!西安，710025 |
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| 摘 要： | 本文针对采用固体火箭发动机卫星的陆基多级固体运载火箭弹道进行了详细的阐述，提出了适合固体运载火箭弹道计算和弹道优化的方法，该方法适用于方案论证和初步弹道计算。
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| 关 键 词： | 火箭弹道 运载火箭 最优设计 |
Calculation and Optimization of Solid Launch Vehicle Trajectory |
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| Zhang Song, Huang Jianding, Huang Zuyin.Calculation and Optimization of Solid Launch Vehicle Trajectory[J].Journal of Solid Rocket Technology,1997,20(1):1-5. |
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| Authors: | Zhang Song Huang Jianding Huang Zuyin |
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| Abstract: | The trajectory of land multiple stages solid launch vehicle used in launching satellites is discussed.A method of trajectory calculation and optimization for solid launch vehicle is presented. The method is suitable for scheme design and preliminary trajectory calculation. |
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| Keywords: | Rocket trajectory Launch vehicle Optimum design |
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