RD-0124M1
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg LOx/Kerosene rocket engine. Developed 1998-. Proposed single chamber variant of RD-0124. Obviously same turbopumps, but one single chamber with larger nozzle extension compared to RD-0124M.
Engine: 393 kg (866 lb). Chamber Pressure: 157.00 bar. Thrust to Weight Ratio: 76.33.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Agency
- Kosberg bureau