This page no longer updated from 31 October 2001. Latest version can be found at RD-0209

Manufacturer Name: RD-0209. Designer: Kosberg. Developed in: 1961-65. Application: UR-200 stage 1. Used on stages: UR-200 stage 1. Propellants: N2O4/UDMH Chambers: 1. Country: Russia. Status: Developed 1961-65. First Flight: 1965. References: 293 . Comments: Engine unit (DU - dvigatelnaya ustanovka) consisting of 1 RD-0211 for tank pressurization and three RD-0210. Modification of RD-0208 with tank pressurization. Further developed into RD--0211.
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Last update 12 March 2001.
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© Mark Wade, 2001 .