H-II (2S)

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H-II (2S)

Part of H-2

Japanese orbital launch vehicle. Three stage version consisting of 2 x H-II SSB boosters + 2 x H-II SRB boosters + core vehicle.

Payload: 3,930 kg (8,660 lb). Thrust: 4,600.00 kN (1,034,100 lbf). Gross mass: 281,000 kg (619,000 lb). Height: 49.00 m (160.00 ft). Diameter: 4.00 m (13.10 ft). Apogee: 40,000 km (24,000 mi).

Payload: 3,930 kg (8,660 lb) to a GTO.

Family: orbital launch vehicle. Country: Japan. Stages: H-2-1, LE-5EC, Castor 4AXL H-2A, H-2-0. Agency: Mitsubishi.

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