发明名称 Modular rocket system
摘要 In one aspect, a modular rocket system comprises a guidance module defining a nose, the guidance module including a guidance system for guiding the modular rocket system toward a target. A flight control module is removably attachable to the guidance module and includes a plurality of airfoils, the airfoils being moveable between a retracted state and an extended state. A munition module is removably attached to the flight control module and includes a hollow interior configured to carry a payload material. A rocket module is attached to the munition module and includes a rocket motor configured to propel the modular rocket system. In a further aspect, a modular rocket system having a plurality of interchangeable modules is provided.
申请公布号 US9194678(B2) 申请公布日期 2015.11.24
申请号 US201313870340 申请日期 2013.04.25
申请人 Wilcox Industries Corp. 发明人 Teetzel James W.;Celona Marc J.;Lemire Gary M.
分类号 F42B15/01;F42B15/10;G05D1/00;G05D1/10;F42B15/36;F42B15/00 主分类号 F42B15/01
代理机构 McLane, Middleton, Professional Association 代理人 McLane, Middleton, Professional Association
主权项 1. A modular rocket system, comprising: a guidance module defining a nose, said guidance module including a guidance system for guiding said modular rocket system toward a target; a flight control module removably attachable to the guidance module, said flight control module including a plurality of airfoils, said airfoils being moveable between a retracted state and an extended state; a munition module removably attached to the flight control module, said munition module including a hollow interior configured to carry a payload material; and a rocket module attached to the munition module, said rocket module including a rocket motor configured to propel the modular rocket system.
地址 Newington NH US