This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Isayev. Used on spacecraft: LK-700. Propellants: N2O4/UDMH Thrust(vac): 1,670 kgf. Thrust(vac): 16.40 kN. Chambers: 1. Country: USSR. Status: Study 1968. References: 443 . Comments: Three of these engines used for midcourse corrections and soft lunar landing in Block 11 and Block 1V stages of LK-700 manned spacecraft.
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Last update 12 March 2001.
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© Mark Wade, 2001 .