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Test and Evaluation Methods for the Modification and Installation of Directed Infrared Countermeasures to an Aircraft

지향성적외선방해장비(DIRCM)를 항공기에 개조 장착하기 위한 시험평가 방안

  • Byeongheon Lee (Avionics System Engineering Team, Hanwha System) ;
  • Juhan Lee (Avionics System Engineering Team, Hanwha System) ;
  • Youngil Kim (Avionics System Engineering Team, Hanwha System) ;
  • Sungil Lee (Avionics System Engineering Team, Hanwha System) ;
  • Younggon Kim (Avionics System Engineering Team, Hanwha System) ;
  • Jangwook Hur (Department of Mechanical Systems Engineering, Kumoh National University Institute of Technology)
  • 이병헌 (한화시스템(주) 항공시스템기술팀) ;
  • 이주한 (한화시스템(주) 항공시스템기술팀) ;
  • 김영일 (한화시스템(주) 항공시스템기술팀) ;
  • 이성일 (한화시스템(주) 항공시스템기술팀) ;
  • 김영곤 (한화시스템(주) 항공시스템기술팀) ;
  • 허장욱 (금오공과대학교 기계시스템공학과)
  • Received : 2024.08.20
  • Accepted : 2024.11.05
  • Published : 2024.12.05

Abstract

Testing and evaluation is essential for the modification and installation DIRCM onto an aircraft. DIRCM is an optical device that deceives infrared guided missiles. There are many things to consider when installing DIRCM on an aircraft and operating it. In order to verify the function and performance of DIRCM, the characteristics of the linkage equipment were presented, and the expected flight sortie was proposed by specifying the test and evaluation methods, items, and detailed test conditions.

Keywords

References

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