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H-2-2
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Gross Mass: 16,700 kg (36,800 lb). Empty Mass: 2,700 kg (5,900 lb). Thrust (vac): 121.500 kN (27,314 lbf). Isp: 452 sec. Burn time: 600 sec. Propellants: Lox/LH2. Diameter: 4.00 m (13.10 ft). Span: 4.00 m (13.10 ft). Length: 10.60 m (34.70 ft). Country: Japan. No Engines: 1. Engine: LE-5A. Cost $ : 30.000 million. First Flight: 1994. Last Flight: 1999. No Launched: 7. Other designations: LE-5EC.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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