RD-191
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko LOx/Kerosene rocket engine. Proposed for stage 1 of Angara. Single chamber from 4-chamber RD-170 would have been cheap and fast to develop. Only reached the draft project stage by 2003. Gimbaling +/- 8 degree in two planes.
Engine: 3,230 kg (7,120 lb). Chamber Pressure: 257.00 bar. Area Ratio: 37. Thrust to Weight Ratio: 64.56. Oxidizer to Fuel Ratio: 2.6.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Stages
- Angara UM
- Agency
- Glushko bureau