RD-268
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko N2O4/UDMH rocket engine. MR-UR-100 / RS-16 (SS-17) stage 1. Out of Production. First flight 1976. Modification of RD-263 engine. First flight 1990.
Thrust (sl): 1,147.000 kN (257,855 lbf). Thrust (sl): 117,000 kgf. Engine: 770 kg (1,690 lb). Chamber Pressure: 226.00 bar. Thrust to Weight Ratio: 163.63. Oxidizer to Fuel Ratio: 2.67.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- MR-UR-100
- Propellants
- N2O4/UDMH
- Stages
- MR-UR-100 St 1, Perimetr Stage 1
- Agency
- Glushko bureau