액체로켓엔진 부품의 배치에 따른 성능해석

초록

Liquid rocket engine is consists of various components according to cycle, and its performance varies depending on the arrangement of the parts of the engine. Consequently liquid rocket engine arrangement of components must be considered in the design process. In this research, major components have been selected that comprise the gas-generator cycle engine and constituting analysis module. By applying constitutive module to the engine system, it is ascertained that specific impulse and thrust-to-weight are changed depending on the arrangement of turbo-pump and turbine.