The Soyuz TMA-3 vehicle launches from the Baikonur Cosmodrome
|Function||Orbital carrier rocket|
|Country of origin|| Soviet Union
|Height||34.54 metres (113.3 ft)|
|Diameter||2.95 metres (9 ft 8 in)|
|Mass||297,800 kilograms (657,000 lb)|
|7,050 kilograms (15,500 lb)|
|Launch sites||LC-1/5 & 31/6, Baikonur
|First flight||23 December 1982|
|Last flight||3 or 29 September 1995|
The Soyuz-U2 (GRAU index 11A511U2) was a Soviet, later Russian, carrier rocket. It was derived from the Soyuz-U, and a member of the R-7 family of rockets. It featured increased performance compared to the baseline Soyuz-U, due to the use of syntin propellant, as opposed to RP-1 paraffin, used on the Soyuz-U.
The increased payload of the Soyuz-U2 allowed heavier spacecraft to be launched, while lighter spacecraft could be placed in higher orbits, compared to those launched by Soyuz-U rockets. In 1996, it was announced that the Soyuz-U2 had been retired, as the performance advantage gained through the use of syntin did not justify the additional cost of its production. The final flight had occurred in the previous year.
The Soyuz-U2 was primarily used to launch Yantar reconnaissance satellites, and Soyuz and Progress spacecraft to the Mir space station. Due to the similarity between the Soyuz-U and U2, the exact number of Soyuz-U2 launches is in doubt, with estimates ranging from 66 to 92 launches. It is also unclear how many launches failed, however most sources suggest there were either zero or two failures.
See also 
|Wikimedia Commons has media related to: Soyuz (rocket)|
- Wade, Mark. "Soyuz 11A511U2". Encyclopedia Astronautica. Retrieved 2008-12-24.
- "Soyuz-U2 (Russian Federation), SPACE LAUNCH VEHICLES - ORBITAL". Jane's. Retrieved 2008-12-24.
- Krebs, Gunter. "Soyuz-U2 (11A511U2)". Gunter's Space Page. Retrieved 2008-12-24.
- McDowell, Jonathan. "R-7 family". Launch Lists. Jonathan's Space Page. Retrieved 2008-12-24.
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