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RD-263


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z RD-263 Part of RD-215 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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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