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

Status: Design 1999. Thrust: 274.00 kN (61,597 lbf). Gross mass: 13,600 kg (29,900 lb). Unfuelled mass: 3,100 kg (6,800 lb). Specific impulse: 452 s. Specific impulse sea level: 340 s. Burn time: 167 s. Height: 13.60 m (44.60 ft). Diameter: 2.40 m (7.80 ft). Span: 9.25 m (30.34 ft).

No Engines: 2.



Country: Japan. Engines: HIMES engine. Launch Vehicles: H-II HIMES. Propellants: Lox/LH2.

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