M-V-3

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Model: M-V-3. Gross Mass: 11,000 kg (24,000 lb). Empty Mass: 1,000 kg (2,200 lb). Thrust (vac): 294.000 kN (66,093 lbf). Isp: 301 sec. Burn time: 102 sec. Propellants: Solid. Isp(sl): 0 sec. Diameter: 2.20 m (7.20 ft). Span: 2.20 m (7.20 ft). Length: 3.60 m (11.80 ft). Country: Japan. No Engines: 1. Motor: M34. Status: Active. Cost $ : 6.000 million. First Flight: 1997. Last Flight: 2006. No Launched: 10. Other designations: M-34. 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.