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R-16 Stage 2
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Gross Mass: 27,000 kg (59,000 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 882.100 kN (198,304 lbf). Isp: 293 sec. Burn time: 80 sec. Propellants: Nitric acid/UDMH. Diameter: 2.40 m (7.80 ft). Span: 2.40 m (7.80 ft). Length: 13.00 m (42.00 ft). No Engines: 1. Engine: RD-219. First Flight: 1960. Last Flight: 1972. No Launched: 212. 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.
Used on Launch Vehicles:
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