S-3D
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
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.
Thrust (sl): 600.100 kN (134,908 lbf). Thrust (sl): 61,200 kgf. Propellant Formulation: Lox/RP-1.
Related
- Country
- USA
- Launch Vehicles
- Jupiter IRBM
- Propellants
- Lox/Kerosene
- Agency
- Rocketdyne