This page no longer updated from 31 October 2001. Latest version can be found at 8D415K

Government Designation: 8D415K. Designer: Kosberg. Developed in: 1960-. Application: Concept for N-1. Propellants: Lox/Kerosene Thrust(vac): 150,000 kgf. Thrust(vac): 1,471.00 kN. Chambers: 1. Country: Russia. Status: Developed 1960-. First Flight: 1966. References: 344 . Comments: Designed for use in N-1. Development canceled when Korolev turned to Kuznetsov for R-9 and N-1 engines after continuous rows with Glushko over performance and propellant types.
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Last update 12 March 2001.
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© Mark Wade, 2001 .