KDU-414
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/UDMH rocket engine. Molniya 1, Mars 1, Venera 1, Zond 2-3 maneuvering engine. Out of Production. Spacecraft maneuvering engine.
Engine: 61 kg (134 lb). Chamber Pressure: 11.80 bar. Propellant Formulation: AK20F/UDMH. Thrust to Weight Ratio: 3.27. Oxidizer to Fuel Ratio: 2.6.
Related
- Family
- Storable liquid
- Country
- Russia
- Spacecraft
- Venera 1VA, Mars 2MV-4, Molniya-1, Mars 3MV-4A
- Propellants
- Nitric acid/UDMH
- Agency
- Isayev bureau