S5.45
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/UDMH rocket engine. correction engine for Zond-1, Venera-2-8, and others. Out of Production. Pressure-fed engine. Used as correction engine for spacecraft Zond-1, Vernera-8, and others.
Engine: 52 kg (114 lb). Chamber Pressure: 11.80 bar. Area Ratio: 16. Propellant Formulation: AK20F/UDMH. Thrust to Weight Ratio: 3846.15. Oxidizer to Fuel Ratio: 2.6.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/UDMH
- Agency
- Isayev bureau