| 摘要 |
The present invention relates to a missile decoy. According to one aspect of the present invention, disclosed is a missile decoy comprising: an airframe which is launched by obtaining thrust; a decoy module which is separated from the airframe and inflated in a state that the decoy module is received in the launched airframe and has a reflector for transmitting a decoy signal by reflecting the frequency signal of an opponent missile; and a control module which controls the decoy module to allow the decoy module to be separated from the airframe and inflated. Therefore, the present invention increases the staying time in the air by adding a parachute to the missile decoy. |
