Bell 8081 Government Designation: XLR81-BA. Designer: Bell. Propellants: Nitric acid/UDMH. Thrust(vac): 71.200 kN (16,006 lbf). Isp: 285 sec. Burn time: 240 sec. Mass Engine: 130 kg (280 lb). Diameter: 1.52 m (4.98 ft). Chambers: 1. Chamber Pressure: 10.00 bar. Area Ratio: 45.00. Oxidizer to Fuel Ratio: 2.55. Thrust to Weight Ratio: 55.82. Country: USA. Status: Out of production. First Flight: 1960. Last Flight: 1968. Flown: 156. Bell 8081 used on Rocket Stages Used on stage: Agena B. on launch vehicle: Atlas LV-3A / Agena B. Used on stage: Agena B. on launch vehicle: SLV-3 Atlas / Agena B. Used on stage: Agena B. on launch vehicle: Thor Agena B. Used on stage: Agena B. on launch vehicle: Thor Agena B SLV-2A (B). Used on stage: Agena B. on launch vehicle: Thor Agena D. Bell 8081 used on Spacecraft Used on: Agena B.                   Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted.

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