RD-0139
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg LOx/LNG rocket engine. stage 1. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Gas generator cycle with turbine gas injection into supersonic nozzle.
Engine: 1,544 kg (3,403 lb). Thrust to Weight Ratio: 134.58.
Related
- Country
- Russia
- Propellants
- Lox/LNG
- Agency
- Kosberg bureau
- Bibliography
- 403