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H-2A-2
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Gross Mass: 19,600 kg (43,200 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 137.000 kN (30,798 lbf). Isp: 447 sec. Burn time: 534 sec. Propellants: Lox/LH2. Diameter: 4.00 m (13.10 ft). Span: 4.00 m (13.10 ft). Length: 9.20 m (30.10 ft). Country: Japan. No Engines: 1. Engine: LE-5B. Status: In production. First Flight: 2001. Last Flight: 2006. No Launched: 10. Lower cost version of H-2 second stage.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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