RD-108-11D512P
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 11A511U2-1. Out of production. A 1-2 second specific impulse increase was made possible by the use of synthetic fuel Sintin and a modified mixing head. First flight 1982.
This was a very complicated modification. Diameter is per chamber.
Chambers: 4. Thrust (sl): 788.400 kN (177,239 lbf). Thrust (sl): 80,400 kgf.
Related
- Country
- Russia
- Launch Vehicles
- Soyuz-U2
- Propellants
- Lox/Kerosene
- Stages
- Soyuz 11A511U2-1
- Agency
- Glushko bureau