M-3B-J Designer: Nissan. Gross Mass: 3,600 kg (7,900 lb). Empty Mass: 300 kg (660 lb). Propellants: Solid. Thrust(vac): 132.100 kN (29,697 lbf). Isp: 294 sec. Burn time: 87 sec. Diameter: 1.50 m (4.90 ft). Length: 2.70 m (8.80 ft). Chambers: 1. Area Ratio: 52.00. Country: Japan. Status: In development. First Flight: 1996. Last Flight: 1996. Flown: 1.00. M-3B-J used on Rocket Stages Used on stage: J-1-3. on launch vehicle: J-1. Used on stage: J-1-3. on launch vehicle: J-1 F2.                   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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