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RD-222
Part of RD-253 Family
Glushko Nitric acid/UDMH rocket engine. missile stage 1 (stage 2 used RD-223). Developed 1960-61. Precursor to RD-253.

Status: Developed 1960-61. Date: 1960-61. Thrust: 1,634.00 kN (367,337 lbf). Unfuelled mass: 980 kg (2,160 lb). Specific impulse: 302 s. Specific impulse sea level: 272 s. Height: 3.47 m (11.38 ft). Diameter: 1.46 m (4.79 ft).

Engine: 980 kg (2,160 lb). Chamber Pressure: 147.00 bar. Area Ratio: 26.3. Propellant Formulation: AK27P/UDMH. Thrust to Weight Ratio: 170.02. Oxidizer to Fuel Ratio: 2.92.



Family: Storable liquid. Country: Russia. Propellants: Nitric acid/UDMH. Agency: Glushko bureau. Bibliography: 320.

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