RD-263
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. Out of Production. Four RD-263 engines combined into RD-264 system.
Chamber Pressure: 206.00 bar. Oxidizer to Fuel Ratio: 2.67.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-36M 15A14
- Propellants
- N2O4/UDMH
- Stages
- R-36M-1
- Agency
- Glushko bureau