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Soyuz·Russian Federal Space Agency (ROSCOSMOS)

Soyuz STA Fregat

retired
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Specifications

Status
retired
Height
46.3 m
Diameter
2.95 m
Mass
312,000 kg
Stages
3
Thrust
4,144 kN
Payload to LEO
7,020 kg
Payload to GTO
2,810 kg
First flight
2011-12-17
Total launches
8
Success / Fail
8 / 0

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.

Propulsion

Boosters

4×RD-107A838 kN
RP-1 / LOX · gas-generator
NPO Energomash / KuznetsovIsp 320s (vac)since 2004four boosters

First stage

RD-108A792 kN
RP-1 / LOX · gas-generator
NPO Energomash / KuznetsovIsp 315s (vac)since 2001core

Third stage

RD-0110298 kN
RP-1 / LOX · gas-generator
KBKhAIsp 326s (vac)since 1967Blok I

Payloads it launched

17 loaded
CSO 2
LEO
FALCON EYE 2
LEO
CSO-1
Payload
SES-15
GEO
MICROSCOPE
LEO
SENTINEL-1B
LEO
AAUSAT 4
LEO
OUFTI-1
LEO
E-ST@R-II
LEO
SENTINEL-1A
LEO
PLEIADES 1B
LEO
PLEIADES 1A
LEO
ELISA W23
LEO
ELISA W11
LEO
SSOT
LEO
ELISA E24
LEO
ELISA E12
LEO