| 摘要 |
<p>The present invention provides a missile decoy. The missile decoy includes: a body; a thrust section arranged on the front end of the body, and including a folded first rotor and a motor unit rotating the first rotor; a torque offsetting unit arranged on the rear end of the body, and including a folded second rotor; a decoy device arranged inside the body to receive a frequency signal from enemy′s missile and amplify and transmit the received frequency signal; an inertia measuring unit arranged inside the body; and a control unit configured to control the thrust section and the torque offsetting unit. Therefore, a response time up to the maximum output can be shortened as compared with a body using a jet engine, production properties can be improved, and costs can be reduced by providing the thrust section including rotor blades formed in an upper end of the body and the torque offsetting unit including tail booms formed at the lower end of the body. In addition, a great advantage can be obtained in view of costs, production properties, recycling properties, etc. as compared with a solid-propellent method, and the missile decoy can be made more compact than other bodies.</p> |
