Isayev TKS attitude

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Engine Model: Isayev TKS attitude. Designer: Isayev. Developed in: 1972-77. Application: TKS, Almaz. Propellants: N2O4/UDMH. Thrust(vac): 390 N (80 lbf). Country: Russia. Status: In Production. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.