RD-2
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko Nitric acid/Kerosene rocket engine. experimental. Developed 1945-47. The RD-2 was based on the RD-1 engine. Used chemical ignition.
Throttled thrust(vac): 2.000 kN (450 lbf). Engine: 71 kg (156 lb). Chamber Pressure: 20.60 bar. Thrust to Weight Ratio: 8.61.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/Kerosene
- Agency
- Glushko bureau
- Bibliography
- 342