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RD-263
Part of RD-215 Family
Glushko N2O4/UDMH rocket engine. R-36M / RS-20A (SS-18 Mod 1) stage 1. Out of Production. Four RD-263 engines combined into RD-264 system.

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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