R-16-1

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R-16-1

Part of Kosmos-1

Nitric acid/UDMH propellant rocket stage. Range 12,000 km. TsNIIMash has 1:10 structural simulation model. Two stage ICBM with nitric acid oxidizer. Developed 1956-1961. Entered service 1961. Chief designer Yangel. Source: Placard, TsNIIMash.

Status: Retired 1972. Thrust: 2,609.50 kN (586,639 lbf). Gross mass: 110,000 kg (240,000 lb). Unfuelled mass: 10,000 kg (22,000 lb). Specific impulse: 289 s. Specific impulse sea level: 246 s. Burn time: 106 s. Height: 16.00 m (52.00 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).

Country: Ukraine. Engines: RD-217, RD-218. Launch Vehicles: R-16, R-16U. Propellants: Nitric acid/UDMH.

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