LACE/LE-5 Designer: Mitsubishi. Propellants: Liquid Air/LH2. Thrust(vac): 147.100 kN (33,069 lbf). Thrust(sl): 73.500 kN (16,523 lbf). Isp: 1,200 sec. Isp (sea level): 600 sec. Burn time: 470 sec. Diameter: 2.40 m (7.80 ft). Chambers: 1. Country: Japan. Status: Design 1999. LACE/LE-5 used on Rocket Stages Used on stage: LACE. on launch vehicle: H-2 HIMES.                   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 - 2007 except where otherwise noted.

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