RDKS-100

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Engine Model: RDKS-100. Designer: Dushkin. Developed in: 1946-51. Application: Sanger. Propellants: Lox/Kerosene. Thrust(vac): 980.000 kN (220,310 lbf). Isp: 285 sec. Chambers: 1. Country: Russia. Status: Developed 1946-51. 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.