Response Surface Modeling-Based Analysis on Launch Vehicle Capability

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dc.contributor.authorAnn, Seungjunko
dc.contributor.authorCho, Namhoonko
dc.contributor.authorKim, Youdanko
dc.contributor.authorShin, Sangjunko
dc.contributor.authorAhn, Jaemyungko
dc.date.accessioned2018-12-20T06:50:27Z-
dc.date.available2018-12-20T06:50:27Z-
dc.date.created2018-03-09-
dc.date.created2018-03-09-
dc.date.created2018-03-09-
dc.date.created2018-03-09-
dc.date.issued2018-12-
dc.identifier.citationADVANCES IN SPACE RESEARCH, v.62, no.12, pp.3281 - 3297-
dc.identifier.issn0273-1177-
dc.identifier.urihttp://hdl.handle.net/10203/248265-
dc.description.abstractThis paper proposes a framework to analyze the capacity of a launch vehicle systematically. Important mission requirements and flight parameters that influence the payload capacity of a given launch vehicle configuration are identified. The response surface models (RSM; the “analyzer”) for the launch capacity, coasting/burning arcs, and the velocity increment elements are developed. A series of trajectory optimization results, which are obtained with the “optimizer”, are used to determine the coefficients of the models. The case study to analyze the capacity of a low Earth orbit (LEO) launch vehicle configuration is conducted to demonstrate the validity of the proposed framework.-
dc.languageEnglish-
dc.publisherELSEVIER SCI LTD-
dc.titleResponse Surface Modeling-Based Analysis on Launch Vehicle Capability-
dc.typeArticle-
dc.identifier.wosid000454966000002-
dc.identifier.scopusid2-s2.0-85044341077-
dc.type.rimsART-
dc.citation.volume62-
dc.citation.issue12-
dc.citation.beginningpage3281-
dc.citation.endingpage3297-
dc.citation.publicationnameADVANCES IN SPACE RESEARCH-
dc.identifier.doi10.1016/j.asr.2018.03.007-
dc.contributor.localauthorAhn, Jaemyung-
dc.contributor.nonIdAuthorAnn, Seungjun-
dc.contributor.nonIdAuthorCho, Namhoon-
dc.contributor.nonIdAuthorKim, Youdan-
dc.contributor.nonIdAuthorShin, Sangjun-
dc.description.isOpenAccessN-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorTrajectory optimization-
dc.subject.keywordAuthorMulti-stage launch vehicle-
dc.subject.keywordAuthorLaunch vehicle capability-
dc.subject.keywordAuthorSmall satellite-
dc.subject.keywordAuthorDelta V analysis-
dc.subject.keywordPlusTRAJECTORY OPTIMIZATION-
dc.subject.keywordPlusASCENT TRAJECTORIES-
dc.subject.keywordPlusPERFORMANCE-
dc.subject.keywordPlusMETHODOLOGY-
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AE-Journal Papers(저널논문)
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