SEPR 740

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SEPR 740

SEPR solid rocket engine. Out of production. Used on Berenice, Titus. First flight 1962. Berenice second stage.

AKA: Berenice-2. Status: Out of production. Date: 1962. Thrust: 91.70 kN (20,615 lbf). Gross mass: 1,050 kg (2,310 lb). Unfuelled mass: 310 kg (680 lb). Specific impulse: 230 s. Burn time: 18 s. Height: 3.20 m (10.40 ft). Diameter: 0.57 m (1.87 ft).

Country: France. Launch Vehicles: Berenice, Titus. Propellants: Solid. Stages: SEPR 740. Agency: ONERA, SEPR. Bibliography: 572.

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