SEP 901 (original) (raw)

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SEP 901

Sud/SEP solid rocket engine. MSBS M112 first stage.

AKA: MSBS M112-1. Status: Retired 1968. Thrust: 440.00 kN (98,910 lbf). Gross mass: 10,000 kg (22,000 lb). Height: 4.50 m (14.70 ft). Diameter: 1.51 m (4.95 ft).

Country: France. Launch Vehicles: SSBS S112, MSBS M112, SSBS S01. Propellants: Solid. Stages: SEP 901. Agency: SEPR, Sud.

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