| 固体导弹反喷干扰分析及再入体姿态扰动的解决措施 |
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| 引用本文： | 胡全成.固体导弹反喷干扰分析及再入体姿态扰动的解决措施[J].战术导弹技术,1994(4):9-13. |
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| 作者姓名： | 胡全成 |
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| 作者单位： | 066基地设计所 |
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| 摘 要： | 定性分析了固体战术地地导弹推力终止时反向喷流的气动干扰。提出了消除再入体姿态扰动的两条措施,这两条措施应用于实际中使扰动基本消失。
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| 关 键 词： | 面对面导弹 导弹 推力反向 大气扰动 姿态控制 |
THRUST REVERSAL INTERFERENCE ANALYSES OF SOLID MISSILE AND MEASURES FOR SOLVING ATTITUDE DISTURBANCE OF REENTRY BODY |
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| Hu Quaneheng The Institute of,Base.THRUST REVERSAL INTERFERENCE ANALYSES OF SOLID MISSILE AND MEASURES FOR SOLVING ATTITUDE DISTURBANCE OF REENTRY BODY[J].Tactical Missile Technology,1994(4):9-13. |
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| Authors: | Hu Quaneheng The Institute of Base |
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| Affiliation: | Hu Quaneheng The Institute of 066 Base |
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| Abstract: | Aerodynamic interference of reverse jet for solid tactical ground to ground missile is analysed qualitatively.Two measures for eliminating attitude disturbance of reentry body are put forward and applied in practice. |
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| Keywords: | Ground to ground missile Thrust reversal Atmospheric disturbance Attitude control |
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