01457nam a2200253 c 4500001001300000005001500013008004100028040001100069041001300080052001900093245017800112300003200290545007400322545006400396545006400460653033400524700005300858700004800911700004800959773014201007900001901149900001901168900001601187KSI00012446920040205234734031205s2002    ulka          000   kor    a0110010 akorbeng01a558.05b한64200a연성하중해석을 이용한 위성체 구조부재의 최적화=xOptimization of spacecraft structure by using coupled load analysis/d황도순,e이영신,e김인걸  ap. 106-113:b삽도;c26 cm  a황도순, 정회원, 한국항공우주연구원bdshwang@kari.re.kr  a이영신, 정회원, 충남대학교 기계설계공학과  a김인걸, 정회원, 충남대학교 항공우주공학과  aCoupled load analysisaCLAa연성하중해석aSpacecraft structurea위성체 구조aOptimizationa최적화aLaunch vehiclea발사체aComponent mode synthesisa부분구조합성법aCraig-bampton modela크레이그-뱀튼 모델aOutput transformation matrixa출력변환행렬aStiffness requirementa강성요구조건1 a황도순,g黃度淳,d1962-0KAC2014197914aut1 a이영신,g李永臣,d1950-0KAC2018051101 a김인걸,g金仁杰,d1960-0KAC2016195160 t韓國航空宇宙學會誌.d韓國航空宇宙學會.g30卷 4號(2002년 6월), p. 106-113q30:4<106w(011001)KSE199509707,x1225-134810aHwang, Do-Soon10aLee, Young-Sin10aKim, In-Gul