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