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LACE stage
Part of LE-5B Family
Liquid Air/LH2 propellant rocket stage. .

AKA: LACE;Liquid Air Cycle Engine. Status: Design 1999. Thrust: 147.00 kN (33,046 lbf). Gross mass: 8,000 kg (17,600 lb). Unfuelled mass: 2,000 kg (4,400 lb). Specific impulse: 1,200 s. Specific impulse sea level: 1,200 s. Burn time: 470 s. Height: 8.00 m (26.20 ft). Diameter: 2.40 m (7.80 ft). Span: 2.40 m (7.80 ft).

Cost $ : 10.000 million.



Country: Japan. Engines: LACE/LE-5. Launch Vehicles: H-II HIMES. Propellants: Liquid Air/LH2.

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