RD-0155
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: KBKhA
Kosberg LOx/Kerosene rocket engine. Engine proposed to replace RD-107 in Onega and Avrora versions of the Soyuz launch vehicle.
The engine consists of two chambers, a fixed inner chamber and a gimbaled outer chamber. Chamber pressure in the fixed chamber, 180 kg/m2; in the gimbaled chamber, 160 kg/m2.
Chambers: 2. Thrust (sl): 902.500 kN (202,890 lbf). Thrust (sl): 92,000 kgf. Engine: 1,150 kg (2,530 lb). Chamber Pressure: 176.00 bar.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Agency
- Kosberg bureau
- Bibliography
- 4484