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): 2.940 kN (661 lbf). Chambers: 1. Country: Russia. Status: Developed 1990s.

Thrust chamber from KTDU-80 / S5.80 converted to burn Lox/Kerosene.  
 
 
 
 
 
 
 
 

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