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Tramontane
SEPR solid rocket engine. Out of production. Used on Berenice launch vehicle. First flight 1962. Berenice third stage.

AKA: Berenice-3;SEPR 200. Status: Out of production. Thrust: 50.00 kN (11,240 lbf). Gross mass: 280 kg (610 lb). Unfuelled mass: 124 kg (273 lb). Specific impulse: 220 s. Burn time: 6.70 s. Height: 2.35 m (7.70 ft). Diameter: 0.34 m (1.10 ft).



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

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