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 Family
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.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use