DOT-5
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. 550,000 ignitions
Engine: 0.90 kg (1.98 lb). Chamber Pressure: 3.80 bar. Area Ratio: 60. Thrust to Weight Ratio: .56.
Related
- Family
- Monopropellant
- Country
- Russia
- Agency
- Isayev bureau
- Bibliography
- 350