RDMT-400
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
NII Mash N2O4/UDMH rocket engine. Almaz, Kvant, Kristall, Spektr, Priroda. In Production. Low-thrust attitude control thruster. Used in Isayev 11D458 engine.
Engine: 2.50 kg (5.50 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 16.4.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Stages
- Proton KM-4 Briz M, Rokot-3 Briz
- Agency
- NII Mash
- Bibliography
- 336