RS-2100

Engine · USA

Part of J-2

Original archive entry. The text, images and links below are kept as they were written.

Rocketdyne LOx/LH2 rocket engine. Next Generation Launch Vehicle Booster. Full flow staged combustion, pump-fed. Thrust and specific impulse values are at sea level.

Thrust (sl): 2,047.600 kN (460,319 lbf). Thrust (sl): 208,800 kgf.

Country: USA
Propellants: Lox/LH2
Agency: Rocketdyne

Related