Design of CubeSat propulsion system using hydrogen peroxide monopropellant thruster

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dc.contributor.authorLee, Seunghoko
dc.contributor.authorYoon, Wonjaeko
dc.contributor.authorKwon, Sejinko
dc.date.accessioned2020-10-26T02:55:17Z-
dc.date.available2020-10-26T02:55:17Z-
dc.date.created2020-10-23-
dc.date.created2020-10-23-
dc.date.issued2020-10-12-
dc.identifier.citation71th International Astronautical Congress (IAC)-
dc.identifier.urihttp://hdl.handle.net/10203/276981-
dc.languageEnglish-
dc.publisherInternational Astronautical Federation (IAF)-
dc.titleDesign of CubeSat propulsion system using hydrogen peroxide monopropellant thruster-
dc.typeConference-
dc.identifier.scopusid2-s2.0-85100938636-
dc.type.rimsCONF-
dc.citation.publicationname71th International Astronautical Congress (IAC)-
dc.identifier.conferencecountryEI-
dc.identifier.conferencelocationVirtual-
dc.contributor.localauthorKwon, Sejin-
dc.contributor.nonIdAuthorLee, Seungho-
dc.contributor.nonIdAuthorYoon, Wonjae-
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AE-Conference Papers(학술회의논문)
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