LACE/LE-5

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LACE/LE-5

Part of LE-5 engine

Mitsubishi air augmented Liquid Air/LH2 rocket engine. Design 1999. Used on H-2 HIMES launch vehicle.

Status: Design 1999. Thrust: 147.10 kN (33,069 lbf). Specific impulse: 1,200 s. Specific impulse sea level: 600 s. Burn time: 470 s. Diameter: 2.40 m (7.80 ft).

Thrust (sl): 73.500 kN (16,523 lbf). Thrust (sl): 7,500 kgf.

Family: Air augmented rocket. Country: Japan. Launch Vehicles: H-II HIMES. Propellants: Liquid Air/LH2. Stages: LACE stage. Agency: Mitsubishi.

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