| 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 |
US2015247714(A1) |
申请公布日期 |
2015.09.03 |
| 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;G05D1/10;G05D1/00 |
主分类号 |
F42B15/01 |
| 代理机构 |
|
代理人 |
|
| 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 |
US |
