RD-107-8D728
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 0, Molniya 8K78M-0. OKB Glushko. Used on Molniya 8K78M and 11A57 Stage 0. Propellants kerosene (RG-1 or T-1) / LOx. Diameter is per chamber. First flight 1964.
Chambers: 4. Thrust (sl): 818.800 kN (184,074 lbf). Thrust (sl): 83,484 kgf. Engine: 1,145 kg (2,524 lb). Chamber Pressure: 58.60 bar. Thrust to Weight Ratio: 88.64.
Related
- Country
- Russia
- Launch Vehicles
- Molniya 8K78M
- Propellants
- Lox/Kerosene
- Stages
- Molniya 8K78M-0
- Agency
- Glushko bureau
Photo Gallery
R-7 aft end
Credit: © Mark Wade
