Back to rockets

Soyuz STA Fregat

Soyuz STA Fregat

Soyuz family · built by Progress Rocket Space Center · maiden flight 2011-12-17

Profile data last updated: 2026-08-15T20:08:04.839063+00:00 | 7531-09-01

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.

Specifications

46.3 mLength
2.95 mDiameter
312 tLaunch mass
3Stages

Payload Capacity

7020 kgTo LEO
2810 kgTo GTO

Lifetime Launch Record

As reported by Launch Library 2 across this rocket's entire history, not just the launches tracked on this site.

8Total launches
8Successful
0Failed
0Upcoming

Launches Tracked on This Site

8In our archive
100.0%Success rate
Dec 17, 2011 02:03 UTCEarliest tracked
Dec 29, 2020 16:42 UTCMost recent
MissionDateStatus
Soyuz STA/Fregat | CSO-2 Dec 29, 2020 16:42 UTC Success
Soyuz STA/Fregat | Falcon Eye 2 Dec 02, 2020 01:33 UTC Success
Soyuz STA/Fregat | CSO-1 Dec 19, 2018 16:37 UTC Success
Soyuz STA/Fregat | SES-15 May 18, 2017 11:54 UTC Success
Soyuz STA/Fregat | Sentinel-1B Apr 25, 2016 21:02 UTC Success
Soyuz STA/Fregat | Sentinel-1A Apr 03, 2014 21:02 UTC Success
Soyuz STA/Fregat | Pléiades-HR 1B Dec 02, 2012 02:02 UTC Success
Soyuz STA/Fregat | Pléiades-HR 1A, FASat-Charlie (SSOT), 4 x ELISA Dec 17, 2011 02:03 UTC Success

Wikipedia