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SEPR P163
Part of Emma Family
Matra solid rocket engine. Emma first stage.

AKA: Emma-1. Status: Retired 1963. Thrust: 1.40 kN (315 lbf). Gross mass: 50 kg (110 lb). Unfuelled mass: 11 kg (24 lb). Burn time: 37 s. Height: 1.70 m (5.50 ft). Diameter: 0.13 m (0.42 ft).



Country: France. Launch Vehicles: Emma. Propellants: Solid. Stages: SEPR P163.

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