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조종실 온도 영향성 검증을 위한 캐노피 투명체 코팅 연구
남용석,김태환,김윤희,우성조,김명호,Nam, Yongseog,Kim, Taehwan,Kim, Yunhi,Woo, Seongjo,Kim, Myungho 항공우주시스템공학회 2008 항공우주시스템공학회지 Vol.2 No.2
Under the non-operating exposure condition in the hot area, the T-50 cockpit temperature is expected over the requirement according to T-50 environmental criteria. So it is necessary to protect the cockpit from the high temperature condition during the non-operating exposure because the high temperature of the cockpit may result in the cockpit equipment malfunction. In this study, the transparency coating is selected as the method for protecting the cockpit from the high temperature exposure and analyzed the effect on the cockpit heat load attenuation. Some kinds of cockpit coating were reviewed and selected and the analysis was performed about the effect before and after coating application under 1% hot day condition based on the T-50 FSD hot soaking test data. The result of analysis show transparency coating is so effective to attenuate the heat load of T-50 cockpit.