Soyuz family
Soyuz STA
The 2.1a version includes conversion from analog to digital flight control system and uprated engines on the booster and the first stage with improved injection systems. The new digital flight control and telemetry systems allow the rocket to launch from a fixed rather than angled launch platform and adjust its heading in flight. A digital control system also enables the launch of larger commercial satellites with wider and longer payload fairings such as the ST-type fairing. These fairings introduce too much aerodynamic instability for the old analog system to handle. This stage continues to use the RD-0110 engine. The 2.1a/ST version is sometimes called Soyuz ST-A.
Soyuz STA is built by Progress Rocket Space Center of Russia. Company background, funding, contracts and news for this operator are tracked on Space Index. It first flew on 17 December 2011 and last flew on 29 December 2020.
Flight record
Payload
| Low Earth orbit | 7,020kg |
|---|---|
| Sun-synchronous orbit | 4,230kg |
| Geostationary transfer orbit | 2,810kg |
Vehicle
| Stages | 3 |
|---|---|
| Length | 46.3m |
| Diameter | 2.95m |
| Launch mass | 312t |
| Maiden flight | 2011-12-17 |
| Reusable | No |
Pads used
Orbits delivered
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| 2020-12-29 | Soyuz STA/Fregat | CSO-2 | Soyuz Launch Complex | Sun-Synchronous Orbit | Success |
| 2020-12-02 | Soyuz STA/Fregat | Falcon Eye 2 | Soyuz Launch Complex | Sun-Synchronous Orbit | Success |
| 2018-12-19 | Soyuz STA/Fregat | CSO-1 | Soyuz Launch Complex | Sun-Synchronous Orbit | Success |
| 2017-05-18 | Soyuz STA/Fregat | SES-15 | Soyuz Launch Complex | Geostationary Transfer Orbit | Success |
| 2016-04-25 | Soyuz STA/Fregat | Sentinel-1B | Soyuz Launch Complex | Sun-Synchronous Orbit | Success |
| 2014-04-03 | Soyuz STA/Fregat | Sentinel-1A | Soyuz Launch Complex | Sun-Synchronous Orbit | Success |
| 2012-12-02 | Soyuz STA/Fregat | Pléiades-HR 1B | Soyuz Launch Complex | Success | |
| 2011-12-17 | Soyuz STA/Fregat | Pléiades-HR 1A, FASat-Charlie (SSOT), 4 x ELISA | Soyuz Launch Complex | Sun-Synchronous Orbit | Success |
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.
Further reading: Wikipedia