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Ariane 5-0 P241

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Ariane 5-0 P241
Part of Ariane 5-0 P230 Family
SEP solid rocket engine. First flight 2002. Solid propellant rocket stage. Increased propellant loading (+2.43 metric tons), lighter welded case (-1.6 metric tons) compared to earlier versions.
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AKA: Ariane 5 EAP; P241. Status: In development. Date: 1996-2002. Number: 18 . Thrust: 6,470.00 kN (1,454,510 lbf). Gross mass: 278,330 kg (613,610 lb). Unfuelled mass: 38,200 kg (84,200 lb). Specific impulse: 275 s. Specific impulse sea level: 250 s. Burn time: 130 s. Height: 31.60 m (103.60 ft). Diameter: 3.05 m (10.00 ft).

Country: France. Launch Vehicles: Ariane 5ECA, Ariane 5ES, Ariane 5 EC-B. Propellants: Solid. Stages: Ariane 5-0 P241.

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