Design of Cooling Channels of Preburners for Small Liquid Rocket Engines with Computational Flow and Heat Transfer Analysis - koreascholar

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Design of Cooling Channels of Preburners for Small Liquid Rocket Engines with Computational Flow and Heat Transfer Analysis KCI 등재 SCOPUS

Moon, In-Sang, Lee, Seon-Mi, Moon, Il-Yoon, Yoo, Jae-Han, Lee, Soo-Yong

언어ENG
URLhttps://db.koreascholar.com/Article/Detail/267585

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Journal of Astronomy and Space Sciences

제28권 3호 (2011.09)
pp.233-239

한국우주과학회 (The Korean Space Science Society)

키워드

preburner stage combustion liquid rocket engine gas generator cooling channel oxygen rich combustion

저자

Lee, Soo-Yong( Korea Aerospace Research Institute) | Lee, Soo-Yong
Yoo, Jae-Han( Korea Aerospace Research Institute) | Yoo, Jae-Han
Moon, Il-Yoon( Korea Aerospace Research Institute) | Moon, Il-Yoon
Lee, Seon-Mi( Korea Aerospace Research Institute) | Lee, Seon-Mi
Moon, In-Sang(Korea Aerospace Research Institute)

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