The Soyuz-U2 was a Soviet, later Russian, carrier rocket. It was derived from the Soyuz-U, and a member of the R-7 family of rockets. It featured increased performance compared with the baseline Soyuz-U, due to the use of syntin propellant, as opposed to RP-1 paraffin, used on the Soyuz-U.
Specifications
- Thrust
- —
- Height
- 34.54 m
- Diameter
- 2.95 m
- Launch mass
- 298 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- 7,050 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
71
Launches with a definitive outcome
Success rate
100%
71 of 71
Current success streak
71
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- Soyuz-U2 | Soyuz TM-22 — Success
- Soyuz-U2 | Soyuz TM-21 — Success
- Soyuz-U2 | Soyuz TM-20 — Success
- Soyuz-U2 | Soyuz TM-19 — Success
- Soyuz-U2 | Soyuz TM-18 — Success