The Energy absorption profile for Spacecraft first bumper made of Carbon-Epoxy composite under hypervelocity impacts in Low Earth Orbit environment

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dc.contributor.authorBaluch, Abrar-Ul-Haq Khan-
dc.contributor.authorPark, Yurim-
dc.contributor.authorKim, Chun-Gon-
dc.contributor.authorMoon, Jin Bum-
dc.date.accessioned2014-12-08T08:46:10Z-
dc.date.available2014-12-08T08:46:10Z-
dc.date.created2014-10-12-
dc.date.issued2011-11-17-
dc.identifier.citationThe 8th Korea-Japan Joint Symposium on Composite Materials, v., no., pp. --
dc.identifier.urihttp://hdl.handle.net/10203/191836-
dc.languageENG-
dc.publisherThe Korean Society for Composite Materials-
dc.titleThe Energy absorption profile for Spacecraft first bumper made of Carbon-Epoxy composite under hypervelocity impacts in Low Earth Orbit environment-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationnameThe 8th Korea-Japan Joint Symposium on Composite Materials-
dc.identifier.conferencecountrySouth Korea-
dc.contributor.localauthorBaluch, Abrar-Ul-Haq Khan-
dc.contributor.localauthorPark, Yurim-
dc.contributor.localauthorKim, Chun-Gon-
dc.contributor.localauthorMoon, Jin Bum-
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AE-Conference Papers(학술회의논문)
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