This page no longer updated from 31 October 2001. Latest version can be found at 15D13

Designer: Klimov. Used on spacecraft: LK-700. Propellants: N2O4/UDMH Thrust(vac): 13,400 kgf. Thrust(vac): 131.40 kN. Chambers: 1. Country: USSR. Status: Study 1968. References: 443 . Comments: Main engine for midcourse Block 1V ascent/trans-earth injection stage of LK-700 manned spacecraft. See also 11D423.
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Last update 12 March 2001.
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