Ariane 5-2 L7 Astris
Engine · Germany
Original archive entry. The text, images and links below are kept as they were written.
MBB N2O4/MMH rocket engine. In Production. Used on Ariane 5 launch vehicle. First flight 1996.
Engine: 110 kg (240 lb). Chamber Pressure: 10.35 bar. Area Ratio: 83.31. Thrust to Weight Ratio: 25.4545454545455. Oxidizer to Fuel Ratio: 2.05. Coefficient of Thrust vacuum: 1.72266671908665.
Related
- Family
- Storable liquid
- Country
- Germany
- Launch Vehicles
- Ariane 5
- Propellants
- N2O4/MMH
- Stages
- Ariane 5-2
- Agency
- MBB