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Conceptual Design for a Kerosene Fuel-rich Gas-generator of a Turbopump-fed Liquid Rocket Engine

Min Son Jaye Koo Won Kook Cho Eun Seok Lee

热科学学报（英文版）2012，Vol.21Issue(5)：428-434,7.

热科学学报（英文版）2012，Vol.21Issue(5)：428-434,7.DOI:10.1007/s11630-012-0564-z

Conceptual Design for a Kerosene Fuel-rich Gas-generator of a Turbopump-fed Liquid Rocket Engine

Min Son ¹Jaye Koo ²Won Kook Cho ³Eun Seok Lee³

作者信息

1. Graduate Student, Korea Aerospace University, Goyang, Republic of Korea
2. School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang, Republic of Korea
3. Korea Aerospace Research Institute, Daejeon, Republic of Korea
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摘要

关键词

Liquid rocket engine/Conceptual design/Fuel-rich gas-generator/Sensitivity analysis

Key words

Liquid rocket engine/Conceptual design/Fuel-rich gas-generator/Sensitivity analysis

引用本文复制引用

Min Son,Jaye Koo,Won Kook Cho,Eun Seok Lee..Conceptual Design for a Kerosene Fuel-rich Gas-generator of a Turbopump-fed Liquid Rocket Engine[J].热科学学报（英文版）,2012,21(5):428-434,7.

基金项目

This study was supported by the Output-oriented Project of the Collaborative Research Program with the Higher Education Partners of the Korea Aerospace Research Institute in 2009. （）

热科学学报（英文版）

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ISSN：1003-2169

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