H-1-3 Designer: Nissan. Propellants: Solid. Thrust(vac): 77.000 kN (17,310 lbf). Isp: 291 sec. Isp (sea level): 220 sec. Burn time: 68 sec. Diameter: 1.34 m (4.39 ft). Length: 2.34 m (7.67 ft). Chambers: 1. Country: Japan. First Flight: 1986. Last Flight: 1992. Flown: 9.00. H-1-3 used on Rocket Stages Used on stage: H-1-3. on launch vehicle: H-1.                   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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