## 留言板

 引用本文: 郝峰, 昌敏, 唐硕等 . 不同动力型式的巡飞弹总体参数对比分析[J]. 北京航空航天大学学报, 2016, 42(8): 1612-1618.
HAO Feng, CHANG Min, TANG Shuoet al. Comparative analysis on primary parameters of loitering munitions of different propulsion systems[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8): 1612-1618. doi: 10.13700/j.bh.1001-5965.2015.0490(in Chinese)
 Citation: HAO Feng, CHANG Min, TANG Shuoet al. Comparative analysis on primary parameters of loitering munitions of different propulsion systems[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8): 1612-1618. (in Chinese)

## 不同动力型式的巡飞弹总体参数对比分析

##### doi: 10.13700/j.bh.1001-5965.2015.0490

###### 通讯作者: 唐硕,Tel.:029-88492788,E-mail:stang@nwpu.edu.cn
• 中图分类号: V221.8;TB553

## Comparative analysis on primary parameters of loitering munitions of different propulsion systems

• 摘要: 动力系统选型是影响巡飞弹战技指标中的航时、巡飞速度、航程以及任务载荷重量系数的关键因素之一。基于能量守恒推导出电动力螺旋桨、活塞式螺旋桨动力与喷气式动力3类动力型式的巡飞弹总体参数估算公式，利用敏度分析的思想逐个研究各动力型式性能参数对巡飞弹战技指标的影响程度与影响规律，并从能源供给的角度对比3类动力型式所用燃料的等效比能量特性，梳理出影响各动力型式差异的根源，为巡飞弹顶层设计阶段的动力系统与作战使用之间适配选型提供有效的指导原则。

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##### 出版历程
• 收稿日期:  2015-07-20
• 刊出日期:  2016-08-20

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