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RS-74
RS-74
RS-74
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: 1,112.00 kN (249,987 lbf). Specific impulse: 379 s. Specific impulse sea level: 379 s.

Thrust (sl): 1,112.000 kN (249,987 lbf). Thrust (sl): 113,400 kgf.



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

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