RD-262
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko N2O4/UDMH rocket engine. Tsyklon 3 stage 2. In production. Based on RD-252 First flight 1977.
Chambers: 2. Engine: 728 kg (1,604 lb). Chamber Pressure: 89.50 bar. Area Ratio: 46.1. Thrust to Weight Ratio: 131.86. Oxidizer to Fuel Ratio: 2.6.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- Tsiklon-3
- Propellants
- N2O4/UDMH
- Stages
- Tsyklon 3-2
- Agency
- Glushko bureau