Space · launch vehicle
Soyuz STA Fregat
PRSC
RETIRED
At a glance
Launches
8
Success rate
100%
8 ok · 0 failed
Payload to LEO
7,020 kg
Payload to GTO
2,810 kg
Manufacturer
Progress Rocket Space CenterStatus
RetiredFirst flight
17 Dec 2011Reusable
NoHeight
46.3 mDiameter
2.95 mLaunch mass
312 tLiftoff thrust
—Stages
3Launch cost
—Booster landings
—Links
WikipediaAbout
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.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026
