| 横向机动控制固体火箭发动机的冲量效率(英文) |
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| 引用本文： | 张平,张玉成.横向机动控制固体火箭发动机的冲量效率(英文)[J].北京理工大学学报,1990(Z1). |
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| 作者姓名： | 张平 张玉成 |
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| 作者单位： | 北京理工大学飞行器工程系
(张平)，北京理工大学飞行器工程系(张玉成) |
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| 摘 要： | 对安装在旋转飞行器上实现横向机动控制的固体火箭发动机的冲量效率进行了分析,导出了计算冲量效率的解析式,并对计算结果进行了讨论。用本方法获得的冲量效率的计算值与参考文献提供的数值十分接近。
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| 关 键 词： | 固体火箭发动机 冲量控制 计算方法/旋转飞行器 |
Impulse Efficiency of a Solid Rocket Motor for Lateral Maneuver Control |
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| Zhang Ping Zhang Yucheng.Impulse Efficiency of a Solid Rocket Motor for Lateral Maneuver Control[J].Journal of Beijing Institute of Technology(Natural Science Edition),1990(Z1). |
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| Authors: | Zhang Ping Zhang Yucheng |
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| Affiliation: | Department of Flight Vehicle Engineering |
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| Abstract: | The impulse efficiency of a solid rocket motor installed on a spinning flight vehicle for lateral maneuver control is analyzed . Analytical formulas for calculating the impulse efficiency in general cases have been derived . The results from calculation are discussed and have been verified to be very close to the values from references . |
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| Keywords: | solid propellant rocket engines impulse control calculating method/spinning flight vehicle |
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