This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Other Designations: S5.80.1100-0. Designer: Isayev. Developed in: 1990s. Application: Soyuz-2 Blok LM. Propellants: Lox/Kerosene Thrust(vac): 300 kgf. Thrust(vac): 2.94 kN. Chambers: 1. Country: Russia. Status: Developed 1990s. Comments: Thrust chamber from KTDU-80 / S5.80 converted to burn Lox/Kerosene.
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Last update 12 March 2001.
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© Mark Wade, 2001 .