8D415K

Government Designation: 8D415K. Designer: Kosberg. Developed in: 1960-. Application: Concept for N-1. Propellants: Lox/Kerosene. Thrust(vac): 1,471.000 kN (330,693 lbf). Chambers: 1. Country: Russia. Status: Developed 1960-. First Flight: 1966.

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.

Bibliography and Further Reading

Siddiqi, Asif A, Soviet Space Web Page, 1999 via Dietrich Haeseler. Asif Siddiqi presents material that could not be fit into his monumental 'Challenge to Apollo'. Accessed at: http://home.earthlink.net/~cliched/main_space.html.

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