MT-135

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Engine Model: MT-135. Designer: Nissan. Propellants: Solid. Thrust(vac): 12.000 kN (2,697 lbf). Diameter: 0.14 m (0.45 ft). Length: 3.30 m (10.80 ft). Country: Japan. MT-135 used on Rocket Stages Used on stage: MT-135. on launch vehicle: 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.