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SB-735 engine

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AKA: Mu-3S-0;SB-735. Status: Retired 1995. Number: 48 . Thrust: 327.80 kN (73,692 lbf). Gross mass: 5,100 kg (11,200 lb). Unfuelled mass: 1,080 kg (2,380 lb). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 38 s. Height: 8.25 m (27.06 ft). Diameter: 0.73 m (2.39 ft).

Nissan solid rocket engine. Used on Mu-3S launch vehicle. First flight 1969. Mu-3S zero stage.