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RD-263
Status: Out of Production. Date: 1969-73. Thrust: 1,155.00 kN (259,654 lbf). Specific impulse: 318 s. Specific impulse sea level: 293 s.
Chamber Pressure: 206.00 bar. Oxidizer to Fuel Ratio: 2.67.
Family: Storable liquid. Country: Russia. Launch Vehicles: R-36M 15A14. Propellants: N2O4/UDMH. Stages: R-36M-1. Agency: Glushko bureau. Bibliography: 323, 7512.
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