RZ.2
Engine · UK
Original archive entry. The text, images and links below are kept as they were written.
Rolls Royce LOx/Kerosene rocket engine. Used on Europa launch vehicle. First flight 1964.
Thrust (sl): 735.500 kN (165,347 lbf). Thrust (sl): 75,000 kgf. Engine: 750 kg (1,650 lb). Chamber Pressure: 39.46 bar. Area Ratio: 8. Thrust to Weight Ratio: 113.71. Coefficient of Thrust vacuum: 1.7615758510983. Coefficient of Thrust sea level: 1.55883890228938.
Related
- Country
- UK
- Launch Vehicles
- Europa I
- Propellants
- Lox/Kerosene
- Stages
- Europa-1
- Agency
- Rolls Royce