RS-2100

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RS-2100

Part of J-2

RS-2100
Credit: Boeing / Rocketdyne

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.

Date: 1999. Thrust: 2,047.60 kN (460,319 lbf). Specific impulse: 384 s. Specific impulse sea level: 384 s.

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

Country: USA. Propellants: Lox/LH2. Agency: Rocketdyne.

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