RD-0142
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg LOx/LNG rocket engine. stage 2. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Obviously variant of RD-0141 with larger nozzle.
Engine: 2,058 kg (4,537 lb). Thrust to Weight Ratio: 116.56.
Related
- Country
- Russia
- Propellants
- Lox/LNG
- Agency
- Kosberg bureau
- Bibliography
- 403