A response surface model for the effects of the atmospheric drag on the Instantaneous Impact Point (IIP) of a rocket

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dc.contributor.authorSeo, Jeongjaeko
dc.contributor.authorAhn, Jaemyungko
dc.date.accessioned2019-04-16T00:51:16Z-
dc.date.available2019-04-16T00:51:16Z-
dc.date.created2013-05-22-
dc.date.created2013-05-22-
dc.date.issued2012-10-01-
dc.identifier.citation63rd International Astronautical Congress-
dc.identifier.urihttp://hdl.handle.net/10203/259460-
dc.languageEnglish-
dc.publisherInternational Astronautical Federation-
dc.titleA response surface model for the effects of the atmospheric drag on the Instantaneous Impact Point (IIP) of a rocket-
dc.typeConference-
dc.identifier.scopusid2-s2.0-84883536737-
dc.type.rimsCONF-
dc.citation.publicationname63rd International Astronautical Congress-
dc.identifier.conferencecountryIT-
dc.identifier.conferencelocationNaple, Italy-
dc.contributor.localauthorAhn, Jaemyung-
dc.contributor.nonIdAuthorSeo, Jeongjae-
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AE-Conference Papers(학술회의논문)
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