B-2C
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. Atlas Booster. Gas generator, pump-fed. Thrust and specific impulse values are at sea level. First flight 1958.
Thrust (sl): 1,374.000 kN (308,887 lbf). Thrust (sl): 140,110 kgf. Propellant Formulation: Lox/RP-1.
Related
- Country
- USA
- Launch Vehicles
- Atlas A
- Propellants
- Lox/Kerosene
- Agency
- Rocketdyne