RD-0245
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg N2O4/UDMH rocket engine. R-29RM / RSM-54 (SS-N-23) stage 1 vernier. Out of Production. Four-chamber steering engine in system RD-0243 driven by turbine exhaust gas. First flight 1985.
Chambers: 4. Chamber Pressure: 147.00 bar. Area Ratio: 14. Oxidizer to Fuel Ratio: 2.6.
Subtopics
- RD-0245-HC Kosberg LOx/Kerosene rocket engine. Design concept 1990's. Proposed variant of RD-0245 engine using LOX-kerosene instead of N2O4/UDMH as propellants.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-29RM
- Propellants
- N2O4/UDMH
- Agency
- Kosberg bureau