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.

    본 발명은 미사일 기만기에 관한 것으로, 일측면에 따르면 추진력을 얻어 발사되는 기체, 발사된 상기 기체에 수용된 상태에서 상기 기체와 분리되고 팽창되며, 상대방 미사일의 주파수 신호를 반사시켜 기만신호를 송출하는 리플렉터를 구비한 기만모듈 및 상기 기만모듈이 상기 기체로부터 분리되고, 팽창 및 전개되도록 제어하는 제어모듈을 포함하는 미사일 기만기가 개시된다.


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    Title :

    MISSILE DECOY


    Additional title:

    미사일 기만기


    Contributors:
    KAM MIN GYU (author) / YOON KI CHEON (author)

    Publication date :

    2016-07-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B63G OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS , Angriffs- oder Verteidigungsanordnungen auf Schiffen / F41H Panzerung , ARMOUR



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