Soyuz 2.1v Volga
Soyuz familyProgress Rocket Space CenterRetired
The Soyuz-2.1v is a Russian expendable carrier rocket. It was derived from the Soyuz-2.1b, and is a member of the R-7 family of rockets.
Specifications
- Thrust
- 1,746 kN
- Height
- 44 m
- Diameter
- 3 m
- Launch mass
- 158 t
- Stages
- 2
- LEO capacity
- 2,850 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
9flightswith a definitive outcome
88.9%success rate8 of 9
1failureincluding partial failures
7success streakcurrent
First flight December 28, 2013 · latest February 5, 2025 · 03:59 UTC
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Soyuz 2.1v flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2013 | 1 | 0 | 1 |
| 2014 | 0 | 0 | 0 |
| 2015 | 0 | 1 | 1 |
| 2016 | 0 | 0 | 0 |
| 2017 | 1 | 0 | 1 |
| 2018 | 0 | 0 | 0 |
| 2019 | 2 | 0 | 2 |
| 2020 | 0 | 0 | 0 |
| 2021 | 0 | 0 | 0 |
| 2022 | 2 | 0 | 2 |
| 2023 | 1 | 0 | 1 |
| 2024 | 0 | 0 | 0 |
| 2025 | 1 | 0 | 1 |