01442nam a2200301 c 4500001001300000005001500013008004100028040001100069041001300080052002600093245025500119300003200374545007000406545004100476545004300517545004300560653022200603700001900825700001400844700004800858700001400906773014200920856002001062900001401082900001501096900001501111900001401126KSI00011609020040213234722031204s2001    ulka          000   kor    a0110010 akorbeng01a558.05b한642c29(6)00a열해석 및 part stress analysis를 이용한 위성용 전장품 설계에 관한 연구=x(A)study on the review of design of electronic equipments for satellite using thermal & part stress analysis/d서현석,e신창환,e김태경,e최석원  ap. 105-111:b삽도;c26 cm  a서현석, 한국항공우주산업㈜bsgorilla@xmail.kari.re.kr  a신창환, 연세대학교 대학원  a김태경, 한국항공우주산업㈜  a최석원, 한국항공우주연구원  a열해석aPart stress analysisaJunction temperatureaAmbient temperatureaEEE partaThermalaElectricaElectronic & electro-magnetic 소자a접합온도a주변온도a인공위성a전장품aEquipmentsaSatellite1 a김태경4aut1 a신창환1 a최석원,g崔錫原,d1962-0KAC2018514481 a서현석0 t韓國航空宇宙學會誌.d韓國航空宇宙學會.g29卷 6號(2001년 9월), p. 105-111q29:6<105w(011001)KSE199509707,x1225-134840u3328177aKd00010aKim, T.K.10aShin, C.H.10aChoi, S.W.10aSeo, H.S.