推力矢量
推力矢量（thrust vectoring；thrust vector control；TVC）是指飞行器将其推力从它的发动机平行方向引向其它方向的技术。推力矢量技术除了可以提供垂直起降或短距起降能力外，还能在空战中为飞机提供额外的机动力。推力矢量一般用可以转动的向量喷嘴或者扰流片来实现。
此项技术广泛使用于火箭及导弹上。对于大气层外飞行的火箭和弹道导弹，空气动力控制面是无效的，因此推力矢量是姿态控制的主要手段。
推力矢量方法
火箭和导弹
参考资料
- ^ United States.; Congress. Senate. Committee on Appropriations. Subcommittee on Department of Defense. Department of Defense appropriations for fiscal year 1984: hearings before a subcommittee of the Committee on Appropriations, United States Senate, Ninety-eighth Congress, first session. U.S. Government Printing Office. 1984: 789.
参考文献
- Wilson, Erich A., "An Introduction to Thrust-Vectored Aircraft Nozzles", ISBN 978-3-659-41265-3
外部链接
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