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RD-0209
Part of RD-0202 Family
Kosberg N2O4/UDMH rocket engine. UR-200 stage 1. Developed 1961-65. Engine unit consisting of 1 RD-0211 for tank pressurization and three RD-0210. Modification of RD-0208 with tank pressurization. Further developed into RD--0211. First flight 1965.

Status: Developed 1961-65. Date: 1961-65.



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: UR-200-1. Agency: Kosberg bureau. Bibliography: 293, 7478.

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