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75-ton-class liquid engine

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.

75-ton-class liquid engine
Korea Aerospace Research Institute (KARI) · Korea Open Government License Type 1 (KOGL Type 1); source indication is required. Attribution and source are preserved separately from the rights statement; no endorsement implied. · Source

Identity

Aliases
75-ton-class liquid engineNURI 75-ton-class engineKSLV-II 75-ton-class liquid engineKARI 75-ton liquid engine
Domains
spaceflight
Identity Level
generic-system
Kind
liquid-rocket-engine
Name
75-ton-class liquid engine
Status
active

Details

Description
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.
Developers
Manufacturers
Propellants
keroseneliquid oxygen
Rocket Specs
Cycle
gas-generator
Sea Level Thrust Kn
674.7
Vacuum Specific Impulse S
304.8

Links

Assets & Meta

Creation Time
July 29, 2026 at 08:03:16 UTC
Updated Time
August 22, 2026 at 08:10:13 UTC

Other

Sources
  • Accessed Date
    2026-08-21
    Note
    KARI's dedicated NURI Engine page identifies the 75-ton-class engine as a domestically developed open-cycle liquid engine using kerosene and liquid oxygen. It reports 674.7 kN sea-level thrust and 304.8 s vacuum specific impulse, describes turbopumps and gas generators, and documents four first-stage and one second-stage installations; the normalized cycle field records the gas-generator architecture.
    Publisher
    Korea Aerospace Research Institute
    Title
    NURI Engine — 75-ton-class liquid engine