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RS-25

Engine
The Aerojet Rocketdyne RS-25, also known as the Space Shuttle Main Engine, is a liquid-fuel cryogenic rocket engine that was used on NASA's Space Shuttle and is used on the Space Launch System. Wikipedia
Chamber pressure: 2,994 psi (20.64 MPa)
Cycle: Fuel-rich dual-shaft staged combustion
Length: 168 inches (4.3 m)
Mass flow: 1,134.26 lb/s (514.49 kg/s)
Mixture ratio: 6.03:1