Stromboli

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Engine Model: Stromboli. Manufacturer Name: SEPR 739. Designer: SEPR. Developed in: 1962. Gross Mass: 1,885 kg (4,155 lb). Empty Mass: 645 kg (1,421 lb). Propellants: Solid. Thrust(vac): 143.000 kN (32,147 lbf). Isp: 235 sec. Burn time: 20 sec. Diameter: 0.56 m (1.83 ft). Length: 4.70 m (15.40 ft). Chambers: 1. Country: France. Status: Out of production. First Flight: 1962. Stromboli used on Rocket Stages Used on stage: Berenice. on launch vehicle: Berenice. Used on stage: Stromboli. on launch vehicle: Belier. Used on stage: Stromboli. on launch vehicle: Hatf II. Used on stage: Stromboli. on launch vehicle: Stromboli. Bibliography: Serra, Jean-Jacques, Rockets in Europe, Web Address when accessed: http://www.univ-perp.fr/fuseurop/index_e.htm. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.