RD-0243
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 stage 1. Out of Production. Consisted of single-chamber main engine RD-0244 plus four-chamber steering engines RD-0245 driven by turbine exhaust gas. Engine submerged in propellant tank.
Chambers: 1 + 4. Engine: 853 kg (1,880 lb). Thrust to Weight Ratio: 98.73.
Subtopics
RD-0244 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.- RD-0244-HC Kosberg LOx/Kerosene rocket engine. Design concept 1990's. Proposed variant of RD-0244 engine using LOX-kerosene instead of N2O4/UDMH as propellants.
- RD R-29 (1) Makeyev N2O4/UDMH rocket engine.
- RD R-29R (1) Makeyev N2O4/UDMH rocket engine.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-29RM
- Propellants
- N2O4/UDMH
- Agency
- Kosberg bureau