RS-76
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. Space Shuttle Reusable First Stage. Ox-Rich staged combustion, pump-fed. Thrust and specific impulse values are at sea level.
Thrust (sl): 4,002.000 kN (899,685 lbf). Thrust (sl): 408,100 kgf. Propellant Formulation: Lox/RP-1 or JP-8.
Related
- Country
- USA
- Propellants
- Lox/Kerosene
- Agency
- Rocketdyne