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11D23
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Designer: Kosberg. Propellants: N2O4/UDMH. Thrust(vac): 230.500 kN (51,818 lbf). Chambers: 1. Country: USSR. Status: Study 1968. Engine used in Block 1 and Block 11 stages of LK-700 manned lunar lander.
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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