HIMES

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Engine Model: HIMES. Designer: Mitsubishi. Propellants: Lox/LH2. Thrust(vac): 137.300 kN (30,866 lbf). Thrust(sl): 103.300 kN (23,223 lbf). Isp: 452 sec. Isp (sea level): 340 sec. Burn time: 167 sec. Chambers: 1. Country: Japan. Status: Design 1999. HIMES used on Rocket Stages Used on stage: HIMES. on launch vehicle: H-2. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.