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H-II HIMES
Part of H-2
Japanese orbital launch vehicle. Concept of H-2 augmented with Liquid-Air Cycle Engine boosters and advanced HIMES upper stage.

AKA: H-2 HIMES. Status: Design 1999. Thrust: 2,167.44 kN (487,260 lbf). Gross mass: 183,700 kg (404,900 lb). Height: 50.00 m (164.00 ft). Diameter: 4.00 m (13.10 ft).

Flyaway Unit Cost 1985$: 170.000 million.

Stage Data - H-2 HIMES



Family: orbital launch vehicle. Country: Japan. Engines: HIMES engine, LACE/LE-5, LE-7. Stages: H-2-1, HIMES, LACE stage. Agency: Mitsubishi.

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