DC Field | Value | Language |
---|---|---|
dc.contributor.author | Ann, Seungjun | ko |
dc.contributor.author | Cho, Namhoon | ko |
dc.contributor.author | Kim, Youdan | ko |
dc.contributor.author | Shin, Sangjun | ko |
dc.contributor.author | Ahn, Jaemyung | ko |
dc.date.accessioned | 2018-12-20T06:50:27Z | - |
dc.date.available | 2018-12-20T06:50:27Z | - |
dc.date.created | 2018-03-09 | - |
dc.date.created | 2018-03-09 | - |
dc.date.created | 2018-03-09 | - |
dc.date.created | 2018-03-09 | - |
dc.date.issued | 2018-12 | - |
dc.identifier.citation | ADVANCES IN SPACE RESEARCH, v.62, no.12, pp.3281 - 3297 | - |
dc.identifier.issn | 0273-1177 | - |
dc.identifier.uri | http://hdl.handle.net/10203/248265 | - |
dc.description.abstract | This 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.language | English | - |
dc.publisher | ELSEVIER SCI LTD | - |
dc.title | Response Surface Modeling-Based Analysis on Launch Vehicle Capability | - |
dc.type | Article | - |
dc.identifier.wosid | 000454966000002 | - |
dc.identifier.scopusid | 2-s2.0-85044341077 | - |
dc.type.rims | ART | - |
dc.citation.volume | 62 | - |
dc.citation.issue | 12 | - |
dc.citation.beginningpage | 3281 | - |
dc.citation.endingpage | 3297 | - |
dc.citation.publicationname | ADVANCES IN SPACE RESEARCH | - |
dc.identifier.doi | 10.1016/j.asr.2018.03.007 | - |
dc.contributor.localauthor | Ahn, Jaemyung | - |
dc.contributor.nonIdAuthor | Ann, Seungjun | - |
dc.contributor.nonIdAuthor | Cho, Namhoon | - |
dc.contributor.nonIdAuthor | Kim, Youdan | - |
dc.contributor.nonIdAuthor | Shin, Sangjun | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | Trajectory optimization | - |
dc.subject.keywordAuthor | Multi-stage launch vehicle | - |
dc.subject.keywordAuthor | Launch vehicle capability | - |
dc.subject.keywordAuthor | Small satellite | - |
dc.subject.keywordAuthor | Delta V analysis | - |
dc.subject.keywordPlus | TRAJECTORY OPTIMIZATION | - |
dc.subject.keywordPlus | ASCENT TRAJECTORIES | - |
dc.subject.keywordPlus | PERFORMANCE | - |
dc.subject.keywordPlus | METHODOLOGY | - |
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