This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Isayev. Developed in: 1972-77. Application: TKS, Almaz. Used on spacecraft: TKS, Almaz. Propellants: N2O4/UDMH Thrust(vac): 40 kgf. Thrust(vac): 0.39 kN. Country: Russia. Status: In Production.
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Last update 12 March 2001.
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© Mark Wade, 2001 .