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Chapter and Conference Paper
Characteristics of the Effective Cross-Sectional Area Reduction of the Turbine Nozzle Throat and Engine Performance of KSLV-II
The engines for the Korea Space Launch Vehicle-II (KSLV-II) are liquid oxygen/kerosene gas generator cycle engine. The turbine is driven by fuel rich gas of the gas generator. The turbine gas in kerosene-fuele...
