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Soyuz STA Fregat

Soyuz familyProgress Rocket Space CenterRetired

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 Fregat vehicle

Specifications

Thrust
4,146 kN
Height
46.3 m
Diameter
2.95 m
Launch mass
312 t
Stages
3
LEO capacity
7,020 kg
GTO capacity
2,810 kg
SSO capacity
4,230 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

8flightswith a definitive outcome
100%success rate8 of 8
0failuresincluding partial failures
8success streakcurrent

First flight December 17, 2011 · 02:03 UTC · latest December 29, 2020

Counted from padside's own launch record, the same basis as the stats page.

Flights per year

  • Successful
  • Failed
Show the numbers for Soyuz STA flights per year
Soyuz STA flights per year
YearSuccessfulFailedTotal
2011101
2012101
2013000
2014101
2015000
2016101
2017101
2018101
2019000
2020202

Flights

5 of 8

All 8 flights