H-2-1 (original) (raw)

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H-2-1

Part of Thor DM-19

LOx/LH2 propellant rocket stage. .

AKA: LE-7. Status: Retired 1999. Thrust: 1,078.00 kN (242,343 lbf). Gross mass: 98,100 kg (216,200 lb). Unfuelled mass: 11,900 kg (26,200 lb). Specific impulse: 446 s. Specific impulse sea level: 349 s. Burn time: 346 s. Height: 28.00 m (91.00 ft). Diameter: 4.00 m (13.10 ft). Span: 4.00 m (13.10 ft).

Cost $ : 80.000 million.

Country: Japan. Engines: LE-7. Launch Vehicles: H-II, H-II (2S), H-II HIMES. Propellants: Lox/LH2.

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