Venus engine

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Venus engine

Part of Belier II engine

Sud solid rocket engine. Centaure 2C first stage.

AKA: Centaure 2C-1. Status: Retired 1981. Thrust: 44.00 kN (9,891 lbf). Gross mass: 200 kg (440 lb). Unfuelled mass: 66 kg (145 lb). Burn time: 4.30 s. Height: 2.00 m (6.50 ft). Diameter: 0.28 m (0.91 ft).

Country: France. Launch Vehicles: Centaure 1, Centaure 2A, Centaure 2B, Centaure 2C. Propellants: Solid. Stages: Venus engine. Agency: Sud.

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