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Soyuz·Russian Federal Space Agency (ROSCOSMOS)

Soyuz STB Fregat-MT

retired
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Specifications

Status
retired
Height
46.3 m
Diameter
2.95 m
Mass
310,000 kg
Stages
3
Thrust
4,144 kN
Payload to LEO
8,200 kg
Payload to GTO
3,250 kg
First flight
2012-10-12
Total launches
5
Success / Fail
5 / 0

The Soyuz-ST-A and ST-B were modified versions of the Soyuz-2 rocket, designed to launch from the Guiana Space Centre (CSG) in French Guiana. Developed as part of a European Space Agency (ESA) programme to add a medium-lift launch vehicle to complement the light-lift Vega and heavy-lift Ariane 5 rockets.

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

9 loaded
METOP-C
LEO
HISPASAT 36W-1
GEO
GAIA
Deep Space
O3B FM5
O3b · MEO
O3B FM4
O3b · MEO
O3B PFM
O3b · MEO
O3B FM2
O3b · MEO
GSAT0104 (GALILEO-FM4)
MEO
GSAT0103 (GALILEO-FM3)
Galileo · MEO