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8D415K
Kosberg LOx/Kerosene rocket engine. Designed for use in N-1. Development canceled in 1960 when Korolev turned to Kuznetsov for R-9 and N-1 engines after continuous rows with Glushko over performance and propellant types. First flight was planned for 1966.

Status: Developed 1960-. Date: 1960-. Thrust: 1,471.00 kN (330,693 lbf).

Country: Russia. Launch Vehicles: N1, N1 1969. Propellants: Lox/Kerosene. Agency: Kosberg bureau. Bibliography: 344.
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