Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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Design Verification of ECS Condenser Icing Protection System by Flight Test of T-50 Advanced Trainer

T-50 비행시험을 통한 환경제어계통 콘덴서 빙결방지 설계 검증

  • 남용석 (국방기술품질원 항공센터) ;
  • 김윤희 (국방기술품질원 항공센터) ;
  • 송석봉 (국방기술품질원 항공센터) ;
  • 서동연 (한국항공우주산업(주)) ;
  • 손원익 (한국항공우주산업(주)) ;
  • 박성순 (국방과학연구소)
  • Published : 2008.09.30
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Abstract

T-50 ECS(environment control system) was designed to have freezing protection for the condenser. However during the ground and flight test, the freezing problem was occurred. This paper deals with the analysis of the freezing problem and introduces anti-freezing design using ADI(Active De-Icing) logic to solve the condenser freezing problem of T-50 ECS

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