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RD-220
Glushko Nitric acid/UDMH rocket engine. missile stage 1 (stage 2 used RD-221). Developed 1960-.

Status: Developed 1960-. Date: 1960-. Thrust: 1,074.00 kN (241,444 lbf). Unfuelled mass: 760 kg (1,670 lb). Specific impulse: 306 s. Specific impulse sea level: 270 s. Height: 2.60 m (8.50 ft). Diameter: 1.29 m (4.23 ft).

Engine: 760 kg (1,670 lb). Chamber Pressure: 147.00 bar. Area Ratio: 31.8. Propellant Formulation: AK27P/UDMH. Thrust to Weight Ratio: 144.1. Oxidizer to Fuel Ratio: 2.8.

Subtopics
RD-221 Glushko Nitric acid/UDMH rocket engine. missile stage 2 (stage 1 used RD-220). Developed 1960-.
Family: Storable liquid. Country: Russia. Propellants: Nitric acid/UDMH. Agency: Glushko bureau. Bibliography: 320.
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