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http://dx.doi.org/10.6108/KSPE.2018.22.2.125

Development Status and Plan of the High Performance Upper Stage Engine for a GEO KSLV  

Yu, Byungil (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
Lee, Kwang-Jin (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
Woo, Seongphil (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
Im, Ji-Hyuk (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
So, Younseok (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
Jeon, Junsu (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
Lee, Jungho (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
Seo, Daeban (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
Han, Yeoungmin (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
Kim, Jinhan (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.22, no.2, 2018 , pp. 125-130 More about this Journal
Abstract
The technology development of a high performance upper stage engine for a GEO(GEostationary Orbit) KSLV(Korea Space Launch Vehicle) is undergoing in Korea Aerospace Research Institute. KSLV is composed of an open cycle engine with gas generator, which is for a low orbit launch vehicle. However the future GEO launch vehicle requires a high performance upper stage engine with a high specific impulse. The staged combustion cycle engine is necessary for this mission. In this paper, current progress and future plan for staged combustion cycle engine development is described.
Keywords
Staged Combustion Cycle Engine; Liquid Rocket Engine; LOx; Kerosene; Gas Generator;
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