RD-190
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko LOx/LCH4 rocket engine. Riksha-0 stage 1. Developed 1996-. The RD-190 consists of 6 RD-169 engines. Each chamber can be gimbaled individually in two planes by +/- 8 degree.
Chambers: 6. Engine: 1,470 kg (3,240 lb). Chamber Pressure: 147.00 bar. Thrust to Weight Ratio: 69.36. Oxidizer to Fuel Ratio: 3.4.
Related
- Country
- Russia
- Launch Vehicles
- Riksha
- Propellants
- Lox/LCH4
- Agency
- Glushko bureau
- Bibliography
- 325