KRD-61
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev N2O4/UDMH rocket engine. Luna Ye-8. Out of Production. Spacecraft maneuvering engine for ascent stage of Luna moon sample return missions. First flight 1969.
Engine: 42 kg (92 lb). Chamber Pressure: 92.20 bar. Thrust to Weight Ratio: 45.88. Oxidizer to Fuel Ratio: 1.84. Coefficient of Thrust sea level: 0.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Agency
- Isayev bureau