DOK-50
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: 1.10 kg (2.40 lb). Chamber Pressure: 8.00 bar. Area Ratio: 42. Thrust to Weight Ratio: 4.63.
Related
- Family
- Monopropellant
- Country
- Russia
- Agency
- Isayev bureau
- Bibliography
- 350