Shock Response Prediction of Low Altitude Earth Observation Satellite During Launch Vehicle Separation Using an Empirical Model

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dc.contributor.authorLee, D.-O-
dc.contributor.authorHan, Jae-Hung-
dc.contributor.authorWoo, S.-H-
dc.contributor.authorKim, J.-H-
dc.date.accessioned2013-03-27T07:14:56Z-
dc.date.available2013-03-27T07:14:56Z-
dc.date.created2012-02-06-
dc.date.issued2009-11-05-
dc.identifier.citationAsia-Pacific International Symposium on Aerospace Technology(APISAT) 2009, v., no., pp. --
dc.identifier.urihttp://hdl.handle.net/10203/160269-
dc.languageENG-
dc.publisherJSASS, KSAS, CSAA, RAeS-
dc.titleShock Response Prediction of Low Altitude Earth Observation Satellite During Launch Vehicle Separation Using an Empirical Model-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationnameAsia-Pacific International Symposium on Aerospace Technology(APISAT) 2009-
dc.identifier.conferencecountryJapan-
dc.identifier.conferencecountryJapan-
dc.contributor.localauthorHan, Jae-Hung-
dc.contributor.nonIdAuthorLee, D.-O-
dc.contributor.nonIdAuthorWoo, S.-H-
dc.contributor.nonIdAuthorKim, J.-H-
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AE-Conference Papers(학술회의논문)
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