Melanie

Melanie

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Engine Model: Melanie. Designer: SEPR. Gross Mass: 32 kg (70 lb). Empty Mass: 10 kg (22 lb). Propellants: Solid. Thrust(vac): 11.100 kN (2,495 lbf). Isp: 227 sec. Burn time: 4.40 sec. Diameter: 0.22 m (0.72 ft). Length: 2.95 m (9.67 ft). Chambers: 1. Country: France. Status: Out of production. First Flight: 1962.

22 kg propellant. Empty mass estimated.

Melanie used on Rocket Stages

Used on stage: Melanie. on launch vehicle: Antares.

Used on stage: Melanie. on launch vehicle: Berenice.

Used on stage: Melanie. on launch vehicle: Daniel.

Used on stage: Melanie. on launch vehicle: Monica.

Used on stage: Prosper. on launch vehicle: Monica.

Bibliography:

Serra, Jean-Jacques, Rockets in Europe, Web Address when accessed: http://www.univ-perp.fr/fuseurop/index_e.htm.

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