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H-2-1
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Gross Mass: 98,100 kg (216,200 lb). Empty Mass: 11,900 kg (26,200 lb). Thrust (vac): 1,077.996 kN (242,343 lbf). Isp: 446 sec. Burn time: 346 sec. Propellants: Lox/LH2. Isp(sl): 349 sec. Diameter: 4.00 m (13.10 ft). Span: 4.00 m (13.10 ft). Length: 28.00 m (91.00 ft). Country: Japan. No Engines: 1. Engine: LE-7. Cost $ : 80.000 million. First Flight: 1994. Last Flight: 1999. No Launched: 7. No Failed: 1. Other designations: LE-7.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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