DOK-10
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev monopropellant rocket engine. In Production. Pressure-fed monopropellant engine. Thermal decomposition of hydrazine by an iridium-based catalyst, which heated to increase stability. 40,000 ignitions
Engine: 0.60 kg (1.32 lb). Chamber Pressure: 10.00 bar. Area Ratio: 46. Thrust to Weight Ratio: 1.7.
Related
- Family
- Monopropellant
- Country
- Russia
- Agency
- Isayev bureau
- Bibliography
- 350