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H-2A LRB
Part of Thor DM-19 Family
LOx/LH2 propellant rocket stage. Two-engine version of H-2A-1 used as strap-on booster.

Status: In production. Thrust: 2,196.00 kN (493,680 lbf). Gross mass: 117,000 kg (257,000 lb). Unfuelled mass: 17,800 kg (39,200 lb). Specific impulse: 440 s. Specific impulse sea level: 338 s. Burn time: 193 s. Height: 36.70 m (120.40 ft). Diameter: 4.00 m (13.10 ft). Span: 4.00 m (13.10 ft).

No Engines: 2.

Country: Japan. Engines: LE-7A. Launch Vehicles: H-IIA 212. Propellants: Lox/LH2.



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