RD-0255
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: KBKhA
Kosberg N2O4/UDMH rocket engine. R-36M2 / RS-20V (SS-18 Mod-4) stage 2. Comprises of single-chamber main engine RD-0256 plus four-chamber steering engines RD-0257. Development based on RD-0228 with thrust increase by 11%. First flight 1986.
Chambers: 1 + 4.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- Dnepr
- Propellants
- N2O4/UDMH
- Stages
- R-36M2-2
- Agency
- Kosberg bureau