Padside

Soyuz-U-PVB

Soyuz family · Progress Rocket Space Center · Retired

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A Russian orbital launch vehicle. A version of the Soyuz-U with safety modifications to prevent and resist fires in all stages and the upper stage avionics compartment.

Specifications

Thrust
Height
51 m
Diameter
3 m
Launch mass
313 t
Stages
2
Launch cost
LEO capacity
6,900 kg
GTO capacity
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
74
Launches with a definitive outcome
Success rate
97.3%
72 of 74
Current success streak
12
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