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SB-310
Part of S-310
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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