RDMT-200
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
NII Mash N2O4/UDMH rocket engine. Almaz. In Production. Low-thrust attitude control thruster.
Engine: 2.00 kg (4.40 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 10.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Agency
- NII Mash
- Bibliography
- 336