Launch Vehicle

Soyuz-FG Fregat

retired

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Specifications

Status: retired
Height: 4.95 m
Diameter: 2.68 m
Mass: 305,000 kg
Stages: 3
Thrust: 4,144 kN
Payload to LEO: 7,100 kg
First flight: 2003-06-02
Total launches: 10
Success / Fail: 10 / 0

The Soyuz FG is a medium-lift launch vehicle qualified for manned launches and used to deliver Soyuz Spacecraft to Orbit for Missions to the International Space Station.

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

Specifications

Propulsion

Boosters

First stage

Third stage

Payloads it launched