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R-16-2

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z R-16-2 Part of Kosmos A-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: 882.10 kN (198,304 lbf). Gross mass: 27,000 kg (59,000 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 293 s. Burn time: 80 s. Height: 13.00 m (42.00 ft). Diameter: 2.40 m (7.80 ft). Span: 2.40 m (7.80 ft). Country: Ukraine. Engines: RD-219. Launch Vehicles: R-16, R-16U. Propellants: Nitric acid/UDMH. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

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