发明名称 Aircraft missile-hit survivability using infrared lamp and sacrificial support structure
摘要 An aircraft missile vulnerability reduction system based on missile hit acceptance whereby a targeted aircraft's most critical components are protected by a preprogrammed, missile-attracting infrared decoy strategically positioned on a sacrificial portion of the aircraft's structure. The decoy is optimally located based on vulnerability analyses and includes multiple modes of operation that configure to instantaneous survivability needs. The system is capable of providing aircraft survivability against shoulder launched man-portable air defense systems missiles during low-level mission flight scenarios.
申请公布号 US6267039(B1) 申请公布日期 2001.07.31
申请号 US20000501288 申请日期 2000.02.09
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 CZARNECKI GREGORY J.
分类号 B64D1/04;F41H11/02;(IPC1-7):B64D1/04 主分类号 B64D1/04
代理机构 代理人
主权项
地址