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Belier II engine
Sud solid rocket engine. Used in single-stage Belier II and as Centaure 2B second stage.

AKA: Belier II;Centaure 2B-2. Status: Retired 1981. Thrust: 20.00 kN (4,496 lbf). Gross mass: 300 kg (660 lb). Unfuelled mass: 80 kg (176 lb). Burn time: 23 s. Height: 2.90 m (9.50 ft). Diameter: 0.31 m (1.01 ft).



Subtopics

Vega engine Sud solid rocket engine. Belier III first stage.

Venus engine Sud solid rocket engine. Centaure 2C first stage.

Country: France. Launch Vehicles: Centaure 2A, Centaure 2B, Centaure 2C, Dragon 2B. Propellants: Solid. Stages: Belier II engine. Agency: Sud.

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