RD-0244
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-29RM / RSM-54 (SS-N-23) stage 1. Out of Production. Main engine in system RD-0243. Staged combustion cycle. Submerged in propellant tank. First flight 1985.
Chamber Pressure: 275.00 bar. Area Ratio: 2. Oxidizer to Fuel Ratio: 2.6.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-29RM
- Propellants
- N2O4/UDMH
- Stages
- R-29-1
- Agency
- Kosberg bureau