Bell 8081
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Bell Nitric acid/UDMH rocket engine. Out of production. Used on Agena B stage atop Thor and Atlas. First flight 1960.
Engine: 130 kg (280 lb). Chamber Pressure: 10.00 bar. Area Ratio: 45. Propellant Formulation: RFNA/UDMH. Thrust to Weight Ratio: 55.8230769230769. Oxidizer to Fuel Ratio: 2.55. Coefficient of Thrust vacuum: 2.99603430168432. Restarts: 2.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- Thor Agena B, Atlas Agena B, Thor Agena D, Thor SLV-2A Agena B
- Propellants
- Nitric acid/UDMH
- Stages
- Agena B
- Agency
- Bell