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Characteristics of Liquid Rocket Engine Simulation System Using Control Valve  

Lee Joons-Youp (한국항공우주연구원 추진제어그룹)
Jung Tae-Kyu (한국항공우주연구원 추진제어그룹)
Han Sang-Yeop (한국항공우주연구원 추진제어그룹)
Kim Young-Mog (한국항공우주연구원 추진제어그룹)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.9, no.3, 2005 , pp. 74-84 More about this Journal
Abstract
This paper include the investigation of finding the system characteristics of facility by simulating open-type turbo-pump fed system, which has commercial control valves, using AMESIM (Advanced Modeling Environment Simulation) commercial software. After developing a flight-type control valve on the basis of the results, the system characteristics of facility for control and valve tests is estimated. Especially, one of purposes of this paper is to find PID value of each commercial control valve in the facility for system test. To find suitable control logic, PI and PID modes are also compared. This paper also introduces design parameters of valve and equipment for thrust control and TDS simulation, which are using control valves.
Keywords
P.I.D. Feedback Control; Thrust Control Valve; Fuel-Oxidize. Ratio Control Valve; Open Type Turbo-Pump Fed System; CC; CG; FCV; PCV;
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