SEP 900

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Model: MSBS M112-1. Gross Mass: 10,000 kg (22,000 lb). Thrust (vac): 440.000 kN (98,910 lbf). Propellants: Solid. Diameter: 1.51 m (4.95 ft). Length: 4.50 m (14.70 ft). Country: France. No Engines: 1. Motor: SEP 901. Status: Retired 1968. First Flight: 1965. Last Flight: 1968. No Launched: 23. Used as: P-10. Other designations: P-10. Release conditions: Sud/SEP. Model: SSBS S01-2. Gross Mass: 10,000 kg (22,000 lb). Thrust (vac): 440.000 kN (98,910 lbf). Propellants: Solid. Diameter: 1.51 m (4.95 ft). Length: 4.70 m (15.40 ft). Country: France. No Engines: 1. Motor: SEP 903. Status: Retired 1977. First Flight: 1965. Last Flight: 1977. No Launched: 33. Used as: P-10. Other designations: P-10. Release conditions: SEP. Model: MSBS M2-1. Gross Mass: 10,000 kg (22,000 lb). Thrust (vac): 450.000 kN (101,160 lbf). Burn time: 50 sec. Propellants: Solid. Diameter: 1.51 m (4.95 ft). Length: 4.50 m (14.70 ft). Country: France. No Engines: 1. Motor: SEP 904. Status: Retired 1980. First Flight: 1967. Last Flight: 1980. No Launched: 32. Used as: P-10. Other designations: P-10. Release conditions: Sud/SEP. Used on Launch Vehicles: MSBS. SSBS. 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.