M-23-J Designer: Nissan. Gross Mass: 12,800 kg (28,200 lb). Empty Mass: 2,400 kg (5,200 lb). Propellants: Solid. Thrust(vac): 524.800 kN (117,980 lbf). Isp: 282 sec. Burn time: 73 sec. Diameter: 1.40 m (4.50 ft). Length: 2.70 m (8.80 ft). Chambers: 1. Area Ratio: 23.00. Country: Japan. Status: In development. First Flight: 1996. Last Flight: 1996. Flown: 1.00. M-23-J used on Rocket Stages Used on stage: J-1-2. on launch vehicle: J-1. Used on stage: J-1-2. 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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