| 摘要 |
PROBLEM TO BE SOLVED: To provide a guided missile capable of exerting high mobility with a simple constitution without degrading turning performance due to increase of mass of airframe, reducing a flying distance due to thrust loss, and creating a danger to the circumference by falling objects in controlling the attitude by using a thrust deflector under a condition of low dynamic pressure.SOLUTION: A propulsion device 3 giving propulsion force, and a nozzle 4 disposed behind it for deflecting the propulsion force are disposed inside of a body 2 of the guided missile 1 in a state of being offset from a central axis of the body. The nozzle 4 is deflected by a nozzle driving section 5 inside of the body 2, and its deflection angle is controlled by a guide control section 6 inside of the body. Thus, optional control force can be generated by one nozzle 4, and the mobility of the missile can be improved with the simple constitution without degrading the turning performance due to increase of the mass of the airframe, and reducing the flying distance due to thrust loss even under the condition of low dynamic pressure. |
