DMT-600 MMH
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev N2O4/MMH rocket engine. Hermes. In Production. Version of DMT-600 using MMH in place of UDMH, adaptation to western market (was discussed for European Hermes space plane project). 6,000 ignitions
Engine: 4.20 kg (9.20 lb). Chamber Pressure: 9.00 bar. Area Ratio: 46.5. Thrust to Weight Ratio: 14.57. Oxidizer to Fuel Ratio: 1.65.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/MMH
- Agency
- Isayev bureau
- Bibliography
- 350