M-3B-Mu Designer: Nissan. Gross Mass: 3,590 kg (7,910 lb). Empty Mass: 490 kg (1,080 lb). Propellants: Solid. Thrust(vac): 132.100 kN (29,697 lbf). Isp: 294 sec. Burn time: 85 sec. Diameter: 1.50 m (4.90 ft). Length: 2.68 m (8.79 ft). Chambers: 1. Chamber Pressure: 42.00 bar. Area Ratio: 52.00. Country: Japan. First Flight: 1969. Last Flight: 1995. Flown: 24. M-3B-Mu used on Rocket Stages Used on stage: Mu-3S-3. 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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