| 摘要 |
A method and system for aiding an aircraft pilot to avoid being struck by a heat seeking missile includes the steps of providing a mass of water and a missile detector for detecting an incoming heat seeking missile. The water is contained in a tank that extends around an exhaust plume and is adapted to eject water onto and into the housing. The cooling water is ejected out of the tank and into the exhaust plume to thereby cool the exhaust plume and disrupt the guidance system of an incoming missile.
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