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Soyuz 2.1a Fregat-M

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Next flightSoyuz 2.1a/Fregat-M | MKA Kinosputnik, KOEN and othersNov 19

The 2.1a version includes conversion from analog to digital flight control system and uprated engines on the booster and the first stage with improved injection systems. The new digital flight control and telemetry systems allow the rocket to launch from a fixed rather than angled launch platform and adjust its heading in flight. A digital control system also enables the launch of larger commercial satellites with wider and longer payload fairings such as the ST-type fairing. These fairings introduce too much aerodynamic instability for the old analog system to handle.

Soyuz 2.1a Fregat-M vehicle

Specifications

Thrust
4,149 kN
Height
46.3 m
Diameter
2.95 m
Launch mass
312 t
Stages
3
Launch cost
$80M
LEO capacity
7,020 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

20flightswith a definitive outcome
95%success rate19 of 20
1failureincluding partial failures
10success streakcurrent

First flight October 19, 2010 · latest April 3, 2026 · 06:28 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 2.1a/Fregat-M flights per year
Soyuz 2.1a/Fregat-M flights per year
YearSuccessfulFailedTotal
2010202
2011303
2012202
2013101
2014101
2015000
2016000
2017011
2018202
2019101
2020101
2021101
2022202
2023101
2024101
2025000
2026101

Flights

5 of 20

All 20 flights