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SEP 904
Part of MSBS M2
Sud/SEP solid rocket engine. MSBS M2 first stage.

AKA: MSBS M2-1. Status: Retired 1980. Thrust: 450.00 kN (101,160 lbf). Gross mass: 10,000 kg (22,000 lb). Burn time: 50 s. Height: 4.50 m (14.70 ft). Diameter: 1.51 m (4.95 ft).

Country: France. Launch Vehicles: MSBS M011, MSBS M012, MSBS M013, MSBS M1, MSBS M2, MSBS M20. Propellants: Solid. Stages: SEP 904. Agency: SEPR, Sud.
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