S5.80.1100-0

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S5.80.1100-0

Part of S5.80

Isayev LOx/Kerosene rocket engine. Soyuz-2 Blok LM. Developed 1990s. Thrust chamber from KTDU-80 / S5.80 converted to burn LOx/Kerosene.

Status: Developed 1990s. Date: 1990s. Thrust: 2.94 kN (661 lbf).

Country: Russia. Propellants: Lox/Kerosene. Agency: Isayev bureau.

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