다단 고체연료 우주발사체의 비행궤적 해석 : 궤적 최적화와 유도Flight trajectory analysis of multi-staged launcher using solid propellant : trajectory optimization and guidance

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dc.contributor.advisor탁민제-
dc.contributor.advisorTahk, Min-Jea-
dc.contributor.author진재현-
dc.contributor.authorJin, Jae-Hyun-
dc.date.accessioned2011-12-12T07:15:47Z-
dc.date.available2011-12-12T07:15:47Z-
dc.date.issued1992-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=59946&flag=dissertation-
dc.identifier.urihttp://hdl.handle.net/10203/26526-
dc.description학위논문(석사) - 한국과학기술원 : 항공우주공학과, 1992.2, [ [iii], 44 p. ]-
dc.languagekor-
dc.publisher한국과학기술원-
dc.title다단 고체연료 우주발사체의 비행궤적 해석-
dc.title.alternativeFlight trajectory analysis of multi-staged launcher using solid propellant : trajectory optimization and guidance-
dc.typeThesis(Master)-
dc.identifier.CNRN59946/325007-
dc.description.department한국과학기술원 : 항공우주공학과,-
dc.identifier.uid000901546-
dc.contributor.localauthor탁민제-
dc.contributor.localauthorTahk, Min-Jea-
dc.title.subtitle궤적 최적화와 유도-
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AE-Theses_Master(석사논문)
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