The KARI-developed 75-ton-class kerosene/LOX liquid engine is the open-cycle core engine of Nuri (KSLV-II). KARI identifies turbopumps, combustion chambers, gas generators, and valves as its principal subsystems; it reports 674.7 kN sea-level thrust and 304.8 s vacuum specific impulse, with four engines on Nuri's first stage and one on its second stage. This generic class record preserves the shared propulsion identity without asserting a distinct named stage variant.