RD-0107
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Soyuz 11A511 Stage 2 engine displayed at Tsiolkovskiy Museum in Kaluga.
Credit: © Mark Wade
Kosberg LOx/Kerosene rocket engine. R-9, Molniya 8K78, Voskhod 11A57 stage 3. Out of Production. Gas generator cycle.
Chambers: 4. Engine: 410 kg (900 lb). Chamber Pressure: 68.20 bar. Propellant Formulation: Lox/T-1. Thrust to Weight Ratio: 74.09.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Stages
- Molniya 8K78-2
- Agency
- Kosberg bureau
Photo Gallery
RD-0107
Credit: KBKhA
