This page no longer updated from 31 October 2001. Latest version can be found at S5.80.1100-0

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.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .