RDMT-200K
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
NII Mash GOX/Kerosene rocket engine. Buran. Out of Production. Low-thrust attitude control thruster. Mass in ref. NIIMash 95 given as only 2.5 kg.
Engine: 5.50 kg (12.10 lb). Thrust to Weight Ratio: 3.63.
Related
- Country
- Russia
- Propellants
- GOX/Kerosene
- Agency
- NII Mash
- Bibliography
- 336