Development and validation of high-performance hypergolic hybrid rocket fuel ignitor with hydrogen peroxide

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dc.contributor.authorJeong, Junyeongko
dc.contributor.authorBhosale, Vikas Khanduko
dc.contributor.authorYun, Yongtaeko
dc.contributor.authorKwon, Sejinko
dc.date.accessioned2020-09-18T05:03:42Z-
dc.date.available2020-09-18T05:03:42Z-
dc.date.created2020-09-02-
dc.date.issued2019-10-24-
dc.identifier.citation70th International Astronautical Congress (IAC)-
dc.identifier.urihttp://hdl.handle.net/10203/276303-
dc.languageEnglish-
dc.publisherInternational Astronautical Federation (IAF)-
dc.titleDevelopment and validation of high-performance hypergolic hybrid rocket fuel ignitor with hydrogen peroxide-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationname70th International Astronautical Congress (IAC)-
dc.identifier.conferencecountryUS-
dc.identifier.conferencelocationWalter E. Washington Convention Center-
dc.contributor.localauthorKwon, Sejin-
dc.contributor.nonIdAuthorJeong, Junyeong-
dc.contributor.nonIdAuthorBhosale, Vikas Khandu-
dc.contributor.nonIdAuthorYun, Yongtae-
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AE-Conference Papers(학술회의논문)
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