RD-264
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko N2O4/UDMH rocket engine. R-36M / RS-20A (SS-18 Mod 1) stage 1. Consists of four RD-263 engines. Used on Dnepr launch vehicle. First flight 1986.
Chambers: 4. Engine: 3,600 kg (7,900 lb). Chamber Pressure: 206.00 bar. Thrust to Weight Ratio: 128.05. Oxidizer to Fuel Ratio: 2.67.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-36M 15A14, R-36MU 15A18, Dnepr
- Propellants
- N2O4/UDMH
- Stages
- R-36M2-1
- Agency
- Glushko bureau