This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Bell 8096

Agena in orbit
Agena in orbit -

Credit: NASA. 30,272 bytes. 435 x 280 pixels.



Designer: Bell. Used on stages: Agena D. Used on launch vehicles: Atlas / Agena D SLV-3A, Atlas LV-3A / Agena D, LT Thor Agena D, SLV-3 Atlas / Agena D, TA Thor Agena D, Titan 34B, Titan 3B. Propellants: Nitric acid/UDMH Thrust(vac): 7,257 kgf. Thrust(vac): 71.20 kN. Isp: 300 sec. Burn time: 265 sec. Mass Engine: 132 kg. Diameter: 1.5 m. Chambers: 1. Chamber Pressure: 35.00 bar. Area Ratio: 45.00. Thrust to Weight Ratio: 54.98. Country: USA. Status: Out of Production. First Flight: 1963. Last Flight: 1987. Flown: 248.

Hustler EngineHustler Engine

Credit: Bell. 24,377 bytes. 332 x 396 pixels.



Agena EngineAgena Engine

Credit: Bell. 24,273 bytes. 397 x 248 pixels.



Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .