M34 Designer: Nissan. Gross Mass: 11,000 kg (24,000 lb). Empty Mass: 1,000 kg (2,200 lb). Propellants: Solid. Thrust(vac): 294.200 kN (66,139 lbf). Isp: 301 sec. Burn time: 102 sec. Diameter: 2.20 m (7.20 ft). Length: 3.60 m (11.80 ft). Chambers: 1. Chamber Pressure: 59.00 bar. Area Ratio: 96.00. Country: Japan. First Flight: 1997. Last Flight: 2006. Flown: 7.00. M34 used on Rocket Stages Used on stage: M-V-3. on launch vehicle: 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 - 2007 except where otherwise noted.

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