This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Lotarev. Application: An-225. Used on stages: An-225. Used on launch vehicles: Interim HOTOL, MAKS. Propellants: Air/Kerosene Thrust(vac): 23,396 kgf. Thrust(vac): 229.40 kN. Isp: 9,000 sec. Isp (sea level): 8,000 sec. Burn time: 3,375 sec. Mass Engine: 4,500 kg. Chambers: 1. Country: Ukraine. Status: Out of Production. References: 303 .
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Last update 12 March 2001.
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© Mark Wade, 2001 .