MT-135

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Model: MT-135JA-1. Thrust (vac): 12.000 kN (2,697 lbf). Propellants: Solid. Diameter: 0.14 m (0.45 ft). Length: 3.30 m (10.80 ft). Country: Japan. No Engines: 1. Motor: MT-135. Status: Active. First Flight: 1964. Last Flight: 2001. No Launched: 903. Used as: MT-135. Release conditions: Nissan. Used on Launch Vehicles: MT-135. 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.