RD-108-8D727
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: © Mark Wade
Glushko LOx/Kerosene rocket engine. Molniya 1, Molniya 8K78M-1. OKB Glushko. Used on Molniya 8K78L, 8K78M and 11A57 Stage 1. Propellants kerosene (RG-1 or T-1) / LOx. Diameter is per chamber. First flight 1964.
Chambers: 4. Engine: 1,230 kg (2,710 lb). Chamber Pressure: 53.60 bar. Thrust to Weight Ratio: 80.97. Oxidizer to Fuel Ratio: 2.39.
Related
- Country
- Russia
- Launch Vehicles
- Molniya 8K78M
- Propellants
- Lox/Kerosene
- Stages
- Molniya 8K78M-1
- Agency
- Glushko bureau
Photo Gallery
R-7 aft end
Credit: © Mark Wade
