SB-735 Designer: Nissan. Gross Mass: 5,100 kg (11,200 lb). Empty Mass: 1,080 kg (2,380 lb). Propellants: Solid. Thrust(vac): 327.800 kN (73,692 lbf). Thrust(sl): 296.700 kN (66,701 lbf). Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 38 sec. Diameter: 0.73 m (2.39 ft). Length: 8.25 m (27.06 ft). Chambers: 1. Country: Japan. First Flight: 1969. Last Flight: 1995. Flown: 48. SB-735 used on Rocket Stages Used on stage: Mu-3S-0. 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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