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公开(公告)号：US07800032B1
公开(公告)日：2010-09-21
申请号：US11606763
申请日：2006-11-30
IPC分类号： F42B15/01
CPC分类号： F42B10/143 , F42B10/64
摘要： Provided is a detachable aerodynamic missile stabilizing system for a missile flying at low flight speeds. The system includes a housing adapted to couple to couple to the missile. Extending outward from the housing is at least one grid fin. Specifically the grid fin extends from the housing such that it is transverse to a longitudinal axis of the housing and the missile. The grid fin provides a plurality of apertures. The apertures are parallel to the longitudinal axis of the housing and the missile. A coupler is adapted to detachably couple the housing to the missile. A method of use is also provided.
摘要翻译： 提供了一种用于以低飞行速度飞行的导弹的可拆卸气动导弹稳定系统。 该系统包括适于耦合到导弹的壳体的壳体。 从房屋向外延伸至少有一个格栅。 具体地，网格翅片从壳体延伸，使得其横向于壳体和导弹的纵向轴线。 网格翅片提供多个孔。 这些孔平行于壳体和导弹的纵向轴线。 耦合器适于将壳体可拆卸地耦合到导弹。 还提供了一种使用方法。
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公开(公告)号：US20100219285A1
公开(公告)日：2010-09-02
申请号：US11606763
申请日：2006-11-30
IPC分类号： F42B10/14
CPC分类号： F42B10/143 , F42B10/64
摘要： Provided is a detachable aerodynamic missile stabilizing system for a missile flying at low flight speeds. The system includes a housing adapted to couple to couple to the missile. Extending outward from the housing is at least one grid fin. Specifically the grid fin extends from the housing such that it is transverse to a longitudinal axis of the housing and the missile. The grid fin provides a plurality of apertures. The apertures are parallel to the longitudinal axis of the housing and the missile. A coupler is adapted to detachably couple the housing to the missile. A method of use is also provided.
摘要翻译： 提供了一种用于以低飞行速度飞行的导弹的可拆卸气动导弹稳定系统。 该系统包括适于耦合到导弹的壳体的壳体。 从房屋向外延伸至少有一个格栅。 具体地，网格翅片从壳体延伸，使得其横向于壳体和导弹的纵向轴线。 网格翅片提供多个孔。 这些孔平行于壳体和导弹的纵向轴线。 耦合器适于将壳体可拆卸地耦合到导弹。 还提供了一种使用方法。
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