P241 Designer: SEP. Developed in: 1996-2002. Gross Mass: 278,330 kg (613,610 lb). Empty Mass: 38,200 kg (84,200 lb). Propellants: Solid. Thrust(vac): 6,470.000 kN (1,454,510 lbf). Isp: 275 sec. Isp (sea level): 250 sec. Burn time: 130 sec. Diameter: 3.05 m (10.00 ft). Length: 31.60 m (103.60 ft). Chambers: 1. Country: France. Status: In development. First Flight: 2002. Last Flight: 2006. Flown: 18. P241 used on Rocket Stages Used on stage: Ariane 5 EAP. on launch vehicle: Ariane 5 EC-A. Used on stage: Ariane 5 EAP. on launch vehicle: Ariane 5 EC-B. Used on stage: Ariane 5 EAP. on launch vehicle: Ariane 5 V.                   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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