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).