RD-0144
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg LOx/LNG rocket engine. upper stage. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Radiation cooled nozzle extension.
Engine: 250 kg (550 lb). Thrust to Weight Ratio: 60.
Subtopics
- RD-0145 Kosberg LOx/LNG rocket engine. upper stage. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Four-chamber variant of RD-0144.
Related
- Country
- Russia
- Propellants
- Lox/LNG
- Agency
- Kosberg bureau
- Bibliography
- 403