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SEPR P191
Part of Emma
Matra solid rocket engine.

AKA: Emma-0. Status: Retired 1963. Thrust: 14.80 kN (3,327 lbf). Gross mass: 20 kg (44 lb). Unfuelled mass: 13 kg (28 lb). Burn time: 1.00 s. Height: 0.80 m (2.62 ft). Diameter: 0.13 m (0.42 ft).

Matra solid rocket engine. Emma zero stage.



Country: France. Launch Vehicles: Emma. Propellants: Solid. Stages: SEPR P191.

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