발사체 자세제어를 위한 100, 250 N 급 상용 과산화수소 단일추진제 추력기 개발Development of 100, 250 N Commercial H2O2 Monopropellant Thruster for Space Launch Vehicles

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dc.contributor.author안성용-
dc.contributor.author권세진-
dc.date.accessioned2010-03-25T08:40:03Z-
dc.date.available2010-03-25T08:40:03Z-
dc.date.created2012-02-06-
dc.date.issued2009-11-19-
dc.identifier.citation한국추진공학회 추계학술대회, v., no., pp. --
dc.identifier.urihttp://hdl.handle.net/10203/17339-
dc.languageKOR-
dc.language.isokoen
dc.publisher한국추진공학회-
dc.title발사체 자세제어를 위한 100, 250 N 급 상용 과산화수소 단일추진제 추력기 개발-
dc.title.alternativeDevelopment of 100, 250 N Commercial H2O2 Monopropellant Thruster for Space Launch Vehicles-
dc.typeConference-
dc.subject.alternativeHydrogen Peroxideen
dc.subject.alternativeThrusteren
dc.subject.alternativeMonopropellanten
dc.type.rimsCONF-
dc.citation.publicationname한국추진공학회 추계학술대회-
dc.identifier.conferencecountrySouth Korea-
dc.identifier.conferencecountrySouth Korea-
dc.contributor.localauthor권세진-
dc.contributor.nonIdAuthor안성용-

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