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LE-5B
LOx/LH2 propellant rocket stage. Lower cost version of H-2 second stage.

Status: In production. Thrust: 137.00 kN (30,798 lbf). Gross mass: 19,600 kg (43,200 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 447 s. Burn time: 534 s. Height: 9.20 m (30.10 ft). Diameter: 4.00 m (13.10 ft). Span: 4.00 m (13.10 ft).

Subtopics
HIMES LOx/LH2 propellant rocket stage. .
LACE stage Liquid Air/LH2 propellant rocket stage. .
LE-5EC LOx/LH2 propellant rocket stage. .
Country: Japan. Engines: LE-5B engine. Launch Vehicles: H-IIA 212, H-IIA 202, H-IIA 2024, H-IIA 2022, H-IIA 204. Propellants: Lox/LH2.
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