HIMES engine

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HIMES engine

Part of LE-5 engine

Mitsubishi LOx/LH2 rocket engine. Design 1999. Used on H-2 HIMES launch vehicle.

AKA: HIMES. Status: Design 1999. Thrust: 137.30 kN (30,866 lbf). Specific impulse: 452 s. Specific impulse sea level: 340 s. Burn time: 167 s.

Thrust (sl): 103.300 kN (23,223 lbf). Thrust (sl): 10,531 kgf.

Country: Japan. Launch Vehicles: H-II HIMES. Propellants: Lox/LH2. Stages: HIMES. Agency: Mitsubishi.

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