RD-704
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko LOx/Kerosene/LH2 tripropellant engine. Developed 1990's. 452 s. Tripropellant engine, single chamber, derived from RD-701 project. Chamber pressure 294 / 124 bar. First flight 1999.
Mass excluding sensors, gimbal actuators and heat shield. Mass excluding sensors, gimbal actuators and heat shield.
Throttled thrust(vac): 782.000 kN (175,800 lbf). Thrust (sl): 1,720.100 kN (386,694 lbf). Thrust (sl): 175,403 kgf. Engine: 2,422 kg (5,339 lb). Chamber Pressure: 294.00 bar. Thrust to Weight Ratio: 82.77.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene/LH2, Lox/LH2
- Agency
- Glushko bureau