RDMT-135
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
NII Mash N2O4/UDMH rocket engine. Salyut, Mir, Soyuz-T and -TM, Progress, Kosmos-satellites. In Production. Low-thrust attitude control thruster.
Engine: 1.20 kg (2.60 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 11.66.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Agency
- NII Mash