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S-3D


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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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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