RD-0242M
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. Reusable for 6 ignitions total. Throttling to 80%.
Adaptation to western market . 15 ignitions tested with one single engine.
Engine: 185 kg (407 lb). Chamber Pressure: 153.00 bar. Thrust to Weight Ratio: 54.07.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/MMH
- Agency
- Kosberg bureau