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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.

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Last update 12 March 2001.
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