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11D423

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Status: Development ended 1968. Date: 1963-67. Thrust: 134.00 kN (30,124 lbf). Specific impulse: 326 s.

Krasniy Oktyabr Joint Stock Company, St. Petersburg, built this engine for the ascent stage of Chelomei's LK-700S manned lunar project. The engines for UR-100 stage 2 and LK-700 were probably identical, or at least had same designation. Other LK-700 drawings give the engine designation as 15D13 with a slightly different thrust, indicating a modified design was considered late in development.