Head to head
Atlas V 551 vs Soyuz 2.1b
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
Side by side
| Metric | Atlas V 551 | Soyuz 2.1b |
|---|---|---|
| Flights flown | 23 | 25 |
| Success rate | 100% | 100% |
| Payload to LEO (kg) | 18,850 | 8,200 |
| Payload to GTO (kg) | 8,890 | 3,250 |
| Launch cost | $153M | $80M |
| Cost per kg to LEO | $8,117 | $9,756 |
| Length (m) | 59.7 | 46.3 |
| Diameter (m) | 3.8 | 2.95 |
| Launch mass (t) | 573 | 312 |
| Stages | 2 | 3 |
Atlas V 551
100% success rate23 of 23 flown
2006peak 2025 · 5 flights2026
Soyuz 2.1b
100% success rate25 of 25 flown
2008peak 2021 · 4 flights2026
Atlas V 551 is built by United Launch Alliance of the United States (company profile on Space Index).Soyuz 2.1b is built by Progress Rocket Space Center of Russia (company profile on Space Index).
Full specifications and the complete launch history for each: Atlas V 551 · Soyuz 2.1b.
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.