This page no longer updated from 31 October 2001. Latest version can be found at RDKS-100

Designer: Dushkin. Developed in: 1946-51. Application: Sanger. Propellants: Lox/Kerosene Thrust(vac): 100,000 kgf. Thrust(vac): 980.00 kN. Isp: 285 sec. Chambers: 1. Country: Russia. Status: Developed 1946-51.
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Last update 12 March 2001.
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© Mark Wade, 2001 .