RD-107-11D511P
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. Soyuz 11A511U2-0. Out of production. OKB Glushko. Used on 11A511U2 Stage 0. Propellants kerosene (RG-1) / LOx. Diameter is per chamber. First flight 1982.
Chambers: 4. Thrust (sl): 768.800 kN (172,833 lbf). Thrust (sl): 78,400 kgf.
Related
- Country
- Russia
- Launch Vehicles
- Soyuz-U2
- Propellants
- Lox/Kerosene
- Stages
- Soyuz 11A511U2-0
- Agency
- Glushko bureau
Photo Gallery
R-7 aft end
Credit: © Mark Wade
