J-1-3 Gross Mass: 3,600 kg (7,900 lb). Empty Mass: 300 kg (660 lb). Thrust (vac): 132.085 kN (29,694 lbf). Isp: 294 sec. Burn time: 87 sec. Propellants: Solid. Isp(sl): 0 sec. Diameter: 1.50 m (4.90 ft). Span: 1.50 m (4.90 ft). Length: 2.70 m (8.80 ft). Country: Japan. No Engines: 1. Engine: M-3B-J. Status: In development. First Flight: 1996. Last Flight: 1996. No Launched: 1. Other designations: M-3B. Used on Launch Vehicles: J-1. 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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