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H-2A LRB
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Gross Mass: 117,000 kg (257,000 lb). Empty Mass: 17,800 kg (39,200 lb). Thrust (vac): 2,196.000 kN (493,680 lbf). Isp: 440 sec. Burn time: 193 sec. Propellants: Lox/LH2. Isp(sl): 338 sec. Diameter: 4.00 m (13.10 ft). Span: 4.00 m (13.10 ft). Length: 36.70 m (120.40 ft). Country: Japan. No Engines: 2. Engine: LE-7A. Status: In production. Two-engine version of H-2A-1 used as strap-on booster.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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