RD-0110
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. Soyuz 11A511, Molniya-M 8K78M. Precursor RD-0107 used in 11A57 Voskhod stage 2. Modified to increase reliability. First flight 1964.
Chambers: 4. Engine: 408 kg (899 lb). Chamber Pressure: 68.20 bar. Area Ratio: 82.2. Propellant Formulation: Lox/RG-1. Thrust to Weight Ratio: 74.46. Oxidizer to Fuel Ratio: 2.2.
Related
- Country
- Russia
- Launch Vehicles
- Soyuz 11A511, Molniya 8K78M, Soyuz-U, Soyuz-U2, Soyuz M
- Propellants
- Lox/Kerosene
- Agency
- Kosberg bureau
Photo Gallery
RD-0110
Credit: KBKhA
RD-0110O
Credit: KBKhA
RD-0110
Credit: © Mark Wade
