RD-252
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
NPO Enerogmash Museum, November 1992
Credit: © Dietrich Haeseler
Glushko N2O4/UDMH rocket engine. R-36-0 stage 2; Tsyklon 2 stage 2. In production. Used modified chamber from RD-219, nozzle is conventional, so performance is higher. First flight 1965.
Chambers: 2. Engine: 715 kg (1,576 lb). Chamber Pressure: 89.50 bar. Area Ratio: 46.1. Thrust to Weight Ratio: 134.12. Oxidizer to Fuel Ratio: 2.6.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-36O 8K69, Tsiklon-2
- Propellants
- N2O4/UDMH
- Stages
- R-36-2, R-36-0-2, Tsyklon 2-2
- Agency
- Glushko bureau