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http://dx.doi.org/10.6108/KSPE.2012.16.4.087

Modeling and Simulation of Combustion Chamber Test Facility Fuel Supply System  

Chung, Yong-Gahp (한국항공우주연구원 추진시험팀)
Lee, Kwang-Jin (한국항공우주연구원 추진시험팀)
Cho, Nam-Kyung (한국항공우주연구원 추진시험팀)
Han, Yeoung-Min (한국항공우주연구원 추진시험팀)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.16, no.4, 2012 , pp. 87-92 More about this Journal
Abstract
The propulsion system of space launch vehicle generates thrust by supplying oxidizer and fuel to combustion chamber. KSLV-II 2nd stage engine, currently under development by KARI, is to use liquid oxygen as a oxidizer and JET-A1 as a fuel. The 2nd stage pump-fed engine is mainly composed of combustion chamber, turbo-pump and engine supply system. To develop liquid propulsion engine, the development of combustion chamber must be preceded. For performance validation of the combustion chamber, the designed and manufactured combustion chamber should be tested in combustion chamber test facility (CCTF). The detailed design for the planned CCTF in Naro Space Center was conducted. The fuel supply system modeling using AMESim was performed based on the results of the detailed design, and the fuel supply characteristics was analyzed in this paper.
Keywords
Combustion Chamber Test Facility(CCTF); Fuel; Supply System; Hydraulic and Pneumatic; AMESim;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
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