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RD-264
Part of RD-215 Family
Glushko N2O4/UDMH rocket engine. R-36M / RS-20A (SS-18 Mod 1) stage 1. Consists of four RD-263 engines. Used on Dnepr launch vehicle. First flight 1986.

AKA: 11D119. Date: 1969-73. Number: 42 . Thrust: 4,521.00 kN (1,016,361 lbf). Unfuelled mass: 3,600 kg (7,900 lb). Specific impulse: 318 s. Specific impulse sea level: 293 s. Height: 2.15 m (7.05 ft). Diameter: 3.03 m (9.92 ft).

Chambers: 4. Engine: 3,600 kg (7,900 lb). Chamber Pressure: 206.00 bar. Thrust to Weight Ratio: 128.05. Oxidizer to Fuel Ratio: 2.67.

Family: Storable liquid. Country: Russia. Launch Vehicles: R-36M 15A14, R-36MU 15A18, Dnepr. Propellants: N2O4/UDMH. Stages: R-36M2-1. Agency: Glushko bureau. More at: 7514. Bibliography: 315, 323, 342.



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