Bell 8096 Agena in orbit Credit - NASA Media Gallery Government Designation: YLR81-BA. Designer: Bell. Propellants: Nitric acid/UDMH. Thrust(vac): 71.200 kN (16,006 lbf). Isp: 293 sec. Burn time: 265 sec. Mass Engine: 132 kg (291 lb). Diameter: 1.52 m (4.98 ft). Chambers: 1. Chamber Pressure: 35.00 bar. Area Ratio: 45.00. Oxidizer to Fuel Ratio: 2.55. Thrust to Weight Ratio: 54.98. Country: USA. Status: Out of production. First Flight: 1963. Last Flight: 1987. Flown: 175. Bell 8096 used on Rocket Stages Used on stage: Agena D. on launch vehicle: Atlas / Agena D SLV-3A. Used on stage: Agena D. on launch vehicle: Atlas LV-3A / Agena D. Used on stage: Agena D. on launch vehicle: SLV-3 Atlas / Agena D. Used on stage: Agena D. on launch vehicle: Thor Agena D SLV-2A. Used on stage: Agena D. on launch vehicle: Thorad Agena D SLV-2G. Used on stage: Agena D. on launch vehicle: Titan 3B. Bell 8096 used on Spacecraft Used on: Agena D.                   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.

Encyclopedia Astronautica topic index 0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z Enter your search terms   Web www.astronautix.com Submit search form