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A Study for Liquid Rocket Engine System Layout and Assembly  

Ryu Chul-Sung (한국항공우주연구원 엔진그룹)
Chung Yong-Hyun (한국항공우주연구원 엔진그룹)
Oh Myung-Hwan ((주)로템/기술연구소/연구개발7팀)
Nam Kyoung-O ((주)로템/기술연구소/연구개발7팀)
Moon Jong-Hoon ((주)로템/기술연구소/연구개발7팀)
Seol Woo-Seok (한국항공우주연구원 엔진그룹)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.8, no.4, 2004 , pp. 102-108 More about this Journal
Abstract
A layout of regenerative liquid rocket engine using turbo pump has been designed for development of high performance liquid rocket engine. each components of engine system was placed by considering assembly and characteristic. first stage engine system is controled by one plane of axis gimballing and composed of four engine assembly to cluster with launch vehicle. second stage engine system is controled by two plane of axis gimballing and composed of one engine assembly. assembly and disassembly Processes and required program have been developed. various shape of instruments were also developed for carrying out assembly and disassembly process efficiently.
Keywords
Liquid Rocket Engine; Layout; System Assembly;
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  • Reference
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