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College of Engineering(공과대학)School of Mechanical and Aerospace Engineering(기계항공공학부)Dept. of Mechanical Engineering(기계공학과)ME-Conference Papers(학술회의논문)

Development of a Novel Deployment Hinge Mechanism for a Spacecraft Using Axiomatic Design

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dc.contributor.authorJeong, JWko
dc.contributor.authorYoo, YIko
dc.contributor.authorLim, JHko
dc.contributor.authorKim, KWko
dc.contributor.authorLee, Jungjuko
dc.date.accessioned2013-08-22T05:32:13Z-
dc.date.available2013-08-22T05:32:13Z-
dc.date.created2013-07-31-
dc.date.created2013-07-31-
dc.date.created2013-07-31-
dc.date.issued2011-09-
dc.identifier.citationADME 2011 - International Conference on Advanced Design and Manufacturing Engineering-
dc.identifier.urihttp://hdl.handle.net/10203/176202-
dc.languageEnglish-
dc.publisherGuangdong University of Technology-
dc.titleDevelopment of a Novel Deployment Hinge Mechanism for a Spacecraft Using Axiomatic Design-
dc.typeConference-
dc.identifier.wosid000303483500169-
dc.identifier.scopusid2-s2.0-80053017790-
dc.type.rimsCONF-
dc.citation.publicationnameADME 2011 - International Conference on Advanced Design and Manufacturing Engineering-
dc.identifier.conferencecountryCC-
dc.contributor.localauthorLee, Jungju-
dc.contributor.nonIdAuthorJeong, JW-
dc.contributor.nonIdAuthorYoo, YI-
dc.contributor.nonIdAuthorLim, JH-
dc.contributor.nonIdAuthorKim, KW-
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ME-Conference Papers(학술회의논문)
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