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Melanie
SEPR solid rocket engine. Out of production. 22 kg propellant. Empty mass estimated. Used on Berenice launch vehicle. First flight 1962.

AKA: Melanie-1;Prosper. Status: Out of production. Thrust: 11.10 kN (2,495 lbf). Gross mass: 32 kg (70 lb). Unfuelled mass: 10 kg (22 lb). Specific impulse: 227 s. Burn time: 4.40 s. Height: 1.60 m (5.20 ft). Diameter: 0.16 m (0.52 ft).



Country: France. Launch Vehicles: Monica I, Daniel, OPd-56-39-22D, Monica IV, Antares, Berenice. Propellants: Solid. Stages: Melanie. Agency: ATEF, ONERA, SEPR. Bibliography: 572.

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