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公开(公告)号:US3690596A
公开(公告)日:1972-09-12
申请号:US3690596D
申请日:1969-05-02
申请人: US AIR FORCE
发明人: DURRAN DONALD A , PLATUS DANIEL H
CPC分类号: F42B10/30
摘要: A spin control system for a reentry vehicle has a plurality of fins located around the periphery of the vehicle. The fins are rotated by a mass which moves under the action of centrifugal force to move a pair of pins in cam slots located on the fin support shafts to thereby rotate the fins to decrease the cant angle from a preset value at zero roll.
摘要翻译: 用于再入式车辆的旋转控制系统具有位于车辆周边周围的多个翅片。 翼片由离心力作用下移动的质量块旋转,以使位于翅片支撑轴上的凸轮槽中的一对销移动,从而使翅片旋转,从而将倾斜角度从零卷起的预设值减小。