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SB-310
Part of S-310 Family
ISAS solid rocket engine.

AKA: Mu-3C-0. Status: Retired 1984. Thrust: 95.00 kN (21,356 lbf). Gross mass: 500 kg (1,100 lb). Unfuelled mass: 190 kg (410 lb). Burn time: 7.40 s. Height: 5.80 m (19.00 ft). Diameter: 0.31 m (1.01 ft).

ISAS solid rocket engine. Mu-3C zero stage.



Country: Japan. Launch Vehicles: Lambda 2, Lambda 3, Lambda 3H, Lambda 4S, Mu-1, Mu-3D, Lambda 4T, Mu-4S, Lambda 4SC, Mu-3C, ETV, Mu-3H, Mu-3S. Propellants: Solid. Stages: SB-310. Agency: ISAS.

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