This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Kosberg. Used on spacecraft: LK-700. Propellants: N2O4/UDMH Thrust(vac): 23,500 kgf. Thrust(vac): 230.50 kN. Chambers: 1. Country: USSR. Status: Study 1968. References: 443 . Comments: Engine used in Block 1 and Block 11 stages of LK-700 manned lunar lander.
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Last update 12 March 2001.
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© Mark Wade, 2001 .