RD-273

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RD-273

Part of RD-215

Glushko N2O4/UDMH rocket engine. Developed 1975-82. Upgrade of RD-263 in 1982 based on RD-263F project.

Status: Developed 1975-82. Date: 1975-82. Thrust: 1,238.00 kN (278,313 lbf). Specific impulse: 296 s. Specific impulse sea level: 296 s.

Chamber Pressure: 226.00 bar.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: Glushko bureau. Bibliography: 323, 7518.

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