Padside

Soyuz 2.1v

Soyuz family · Ministry of Defence of the Russian Federation · Retired

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Specifications

Thrust
Height
44 m
Diameter
3 m
Launch mass
158 t
Stages
2
Launch cost
LEO capacity
2,850 kg
GTO capacity
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
4
Launches with a definitive outcome
Success rate
100%
4 of 4
Current success streak
4
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