DC Field | Value | Language |
---|---|---|
dc.contributor.author | Moon, Yongjun | ko |
dc.contributor.author | Kwon, Sejin | ko |
dc.date.accessioned | 2014-09-01T06:41:23Z | - |
dc.date.available | 2014-09-01T06:41:23Z | - |
dc.date.created | 2014-06-10 | - |
dc.date.created | 2014-06-10 | - |
dc.date.issued | 2014-06 | - |
dc.identifier.citation | ACTA ASTRONAUTICA, v.99, pp.153 - 157 | - |
dc.identifier.issn | 0094-5765 | - |
dc.identifier.uri | http://hdl.handle.net/10203/189133 | - |
dc.description.abstract | Minimum-mass propulsion specifications using a H2O2/kerosene bipropellant rocket system for a small lunar lander were derived. A multivariable optimization was conducted with propulsion specifications and propellant consumptions obtained by solving optimal control problems for a lunar soft landing. In this paper, the optimal specifications, trajectory, and mass budget are presented. | - |
dc.language | English | - |
dc.publisher | PERGAMON-ELSEVIER SCIENCE LTD | - |
dc.title | Lunar soft landing with minimum-mass propulsion system using H2O2/kerosene bipropellant rocket system | - |
dc.type | Article | - |
dc.identifier.wosid | 000335612000014 | - |
dc.identifier.scopusid | 2-s2.0-84896527343 | - |
dc.type.rims | ART | - |
dc.citation.volume | 99 | - |
dc.citation.beginningpage | 153 | - |
dc.citation.endingpage | 157 | - |
dc.citation.publicationname | ACTA ASTRONAUTICA | - |
dc.identifier.doi | 10.1016/j.actaastro.2014.02.003 | - |
dc.embargo.liftdate | 9999-12-31 | - |
dc.embargo.terms | 9999-12-31 | - |
dc.contributor.localauthor | Kwon, Sejin | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | H2O2/kerosene bipropellant rocket system | - |
dc.subject.keywordAuthor | Propulsion specifications | - |
dc.subject.keywordAuthor | Lunar soft landing | - |
dc.subject.keywordAuthor | Design optimization | - |
dc.subject.keywordAuthor | Optimal control | - |
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