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11D416
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Designer: Isayev. Propellants: N2O4/UDMH. Thrust(vac): 16.400 kN (3,687 lbf). Chambers: 1. Country: USSR. Status: Study 1968. Three of these engines used for midcourse corrections and soft lunar landing in Block 11 and Block 1V stages of LK-700 manned spacecraft.
Bibliography and Further Reading - Yeteyev, Ivan, Operezhaya vremya, Ocherki, Moscow, 1999.. Collection of articles involving the life and works of Chief Designer Chelomei and the Khrunichev factory.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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