M-23-Mu Designer: Nissan. Gross Mass: 13,100 kg (28,800 lb). Empty Mass: 2,800 kg (6,100 lb). Propellants: Solid. Thrust(vac): 524.000 kN (117,799 lbf). Thrust(sl): 404.500 kN (90,935 lbf). Isp: 285 sec. Isp (sea level): 220 sec. Burn time: 70 sec. Diameter: 1.41 m (4.62 ft). Length: 6.19 m (20.30 ft). Chambers: 1. Country: Japan. First Flight: 1969. Last Flight: 1995. Flown: 24. M-23-Mu used on Rocket Stages Used on stage: Mu-3S-2. on launch vehicle: Mu-3.                   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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