Bell 8096
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: NASA
Bell Nitric acid/UDMH rocket engine. Out of production. Used in Agena stage on top of Thor, Atlas, and Titan launch vehicles. First flight 1963.
Engine: 132 kg (291 lb). Chamber Pressure: 35.00 bar. Area Ratio: 45. Propellant Formulation: RFNA/UDMH. Thrust to Weight Ratio: 54.9772727272727. Oxidizer to Fuel Ratio: 2.55. Coefficient of Thrust vacuum: .85. Restarts: 8.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- Thor SLV-2A Agena D, Atlas Agena D, Titan IIIB, Thorad SLV-2H Agena D, Titan 34B, Atlas F/Agena D
- Propellants
- Nitric acid/UDMH
- Stages
- Agena D
- Agency
- Bell
Photo Gallery
Agena Engine
Credit: Bell
Hustler Engine
Credit: Bell
