This page no longer updated from 31 October 2001. Latest version can be found at Izotov LK-700

Designer: Izotov. Developed in: 1966-69. Application: LK-700. Used on spacecraft: LK-700. Propellants: N2O4/UDMH Thrust(vac): 13,400 kgf. Thrust(vac): 131.00 kN. Chambers: 1. Country: Russia. Status: Developed 1966-69.
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Last update 12 March 2001.
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© Mark Wade, 2001 .