M-V-2

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Model: M-V-2. Gross Mass: 34,470 kg (75,990 lb). Empty Mass: 3,410 kg (7,510 lb). Thrust (vac): 1,245.287 kN (279,952 lbf). Isp: 288 sec. Burn time: 71 sec. Propellants: Solid. Isp(sl): 203 sec. Diameter: 2.50 m (8.20 ft). Span: 2.50 m (8.20 ft). Length: 6.80 m (22.30 ft). Country: Japan. No Engines: 1. Motor: M24. Status: Active. Cost $ : 12.000 million. First Flight: 1997. Last Flight: 2006. No Launched: 10. Other designations: M-24. Used on Launch Vehicles: M-V. 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.