RD-0242M1
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg N2O4/MMH rocket engine. Design concept 1998-. Proposed variant of RD-0242 engine for upper stages using MMH in place of UDMH (adaptation to western market). Reusable for 6 ignitions total. Throttling to 80%.
Engine: 229 kg (504 lb). Chamber Pressure: 153.00 bar. Thrust to Weight Ratio: 43.68.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/MMH
- Agency
- Kosberg bureau