DOT-25
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 a wire catalyst, which is electrically heated to 620 K. 60,000 ignitions
Engine: 1.30 kg (2.80 lb). Chamber Pressure: 4.50 bar. Area Ratio: 55. Thrust to Weight Ratio: 1.96.
Related
- Family
- Monopropellant
- Country
- Russia
- Agency
- Isayev bureau
- Bibliography
- 350