Head to head

Long March 2F/G vs Soyuz 2.1b/Fregat-M

Two vehicles in the same payload class. Every figure below comes from the same two sources for both rockets, and a row appears only when both publish the input.

Payload to low Earth orbit

Relative

Long March 2F/G: 8,399 kg

Soyuz 2.1b/Fregat-M: 8,200 kg

Side by side

7 comparable figures

The highlighted value wins the row. Rows where neither direction is better, like length or stage count, highlight nothing.

MetricLong March 2F/GSoyuz 2.1b/Fregat-M
Flights flown2236
Success rate100%100%
Payload to LEO (kg)8,3998,200
Length (m)6246.3
Diameter (m)3.3510.3
Launch mass (t)464313
Stages24

Long March 2F/G

Flight record
100% success rate22 of 22 flown
2011peak 2022 · 3 flights2026

Maiden flight 2011-10-31. Still flying.

Soyuz 2.1b/Fregat-M

Flight record
100% success rate36 of 36 flown
2017peak 2021 · 8 flights2026

Maiden flight 2008-07-26. Still flying.

Long March 2F/G is built by China Aerospace Science and Technology Corporation of China.Soyuz 2.1b/Fregat-M is built by Progress Rocket Space Center of Russia (company profile on Space Index).

Full specifications and the complete launch history for each: Long March 2F/G · Soyuz 2.1b/Fregat-M.

Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.