S-3D

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S-3D

Part of LR79

S-3D
Credit: Boeing / Rocketdyne

Rocketdyne LOx/Kerosene rocket engine. Jupiter Booster. Gas generator, pump-fed. Thrust later 150,000 lbs. Thrust and specific impulse values are at sea level. First flight 1957.

Date: 1955. Thrust: 600.10 kN (134,908 lbf). Specific impulse: 247 s. Specific impulse sea level: 247 s.

Thrust (sl): 600.100 kN (134,908 lbf). Thrust (sl): 61,200 kgf. Propellant Formulation: Lox/RP-1.

Country: USA. Launch Vehicles: Jupiter IRBM. Propellants: Lox/Kerosene. Agency: Rocketdyne.

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