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Soyuz STA

8FLIGHTS
100%SUCCESS
8STREAK
Dec 2011FIRST FLIGHT
NOREUSABLE
HEIGHT46.3 m
DIAMETER2.95 m
LAUNCH MASS312 kg
STAGES3

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.

7,020 kg
TO LEO
15,479 lbs
2,810 kg
TO GTO
6,196 lbs
Height46.3 m (152 ft)
Diameter2.95 m (9.7 ft)
Launch Mass312 kg (688 lbs)
Stages3