액체 추진제 로켓엔진의 혼합비 안정기Mixture Ratio Stabilizer for Liquid Propellant Rocket Engine

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dc.contributor.author권세진ko
dc.contributor.author정태규ko
dc.date.accessioned2013-03-06T15:38:55Z-
dc.date.available2013-03-06T15:38:55Z-
dc.date.created2012-03-19-
dc.date.created2012-03-19-
dc.date.issued2008-07-
dc.identifier.citation한국항공우주학회지, v.36, no.7, pp.703 - 711-
dc.identifier.issn1225-1348-
dc.identifier.urihttp://hdl.handle.net/10203/87458-
dc.description.abstractIn this paper, stabilizer which maintains the mixture ratio of gas generator of LRE has been introduced. Design criterion for the ideal performance of stabilizer was derived. Significant parameters on the performance of stabilizer were identified through mathematical model and gas generator system analysis. Also, simulation and test results of the gas generator system showed fair agreement, thus proving the validity of the mathematical model of the stabilizer.-
dc.languageKorean-
dc.publisher한국항공우주학회-
dc.title액체 추진제 로켓엔진의 혼합비 안정기-
dc.title.alternativeMixture Ratio Stabilizer for Liquid Propellant Rocket Engine-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume36-
dc.citation.issue7-
dc.citation.beginningpage703-
dc.citation.endingpage711-
dc.citation.publicationname한국항공우주학회지-
dc.identifier.kciidART001261420-
dc.contributor.localauthor권세진-
dc.contributor.nonIdAuthor정태규-
dc.subject.keywordAuthorStabilizer(안정기)-
dc.subject.keywordAuthorMixture ratio(혼합비)-
dc.subject.keywordAuthorThrust control(추력제어)-
dc.subject.keywordAuthorLRE(액체 로켓엔진)-
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AE-Journal Papers(저널논문)
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