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astronautix.com R-16 Stage 2


Gross Mass: 27,000 kg. Empty Mass: 3,000 kg. Thrust (vac): 89,950 kgf. Isp: 293 sec. Burn time: 80 sec. Propellants: Nitric acid/UDMH Diameter: 2.4 m. Span: 2.4 m. Length: 13.0 m. No Engines: 1. RD-219 Status: Hardware. Comments: 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.
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Last update 12 March 2001.
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© Mark Wade, 2001 .