📊 Analysis
Statistics & insights on rockets and organizations — technology, history, numbers.
Soyuz-FG Fregat
RetiredProgress Rocket Space Center
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.
Key figures
Total launches
10
Successes
10
Failures
0
Success rate
100.0 %
Success streak
10
Maiden flight
Jun 2, 2003
Reusable
No
Shortest launch interval ⓘ
49d 1h
Planned launches
0
Technology
Length
4.95 m
Diameter
2.68 m
Launch mass
305 t
Stages
3
LEO (low Earth orbit)
7,100 kg
Engines & propellant
| Boosters | 4× RD-107A | Kerosin / Flüssigsauerstoff |
| 1st stage | 1× RD-108A (Zentralblock) | Kerosin / Flüssigsauerstoff |
| 2nd stage | RD-0110 / RD-0124 | Kerosin / Flüssigsauerstoff |
| Kick stage | Fregat (optional) | UDMH / Stickstofftetroxid |
Engine and propellant data from curated sources: Wikipedia — Sojus (Rakete)
Launches per year
of which in our database: 10
Successes Failures Other/planned
History & events
Sources
- Launch Library 2 (The Space Devs)
- Wikipedia