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LE-5EC
Part of LE-5B Family
LOx/LH2 propellant rocket stage. .

Status: Retired 1999. Thrust: 121.50 kN (27,314 lbf). Gross mass: 16,700 kg (36,800 lb). Unfuelled mass: 2,700 kg (5,900 lb). Specific impulse: 452 s. Burn time: 600 s. Height: 10.60 m (34.70 ft). Diameter: 4.00 m (13.10 ft). Span: 4.00 m (13.10 ft).

Cost $ : 30.000 million.



Country: Japan. Engines: LE-5A. Launch Vehicles: H-II, H-II (2S). Propellants: Lox/LH2.

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