Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | H-IIA 202 Mitsubishi Heavy Industries × remove | Soyuz U Russian Federal Space Agency (ROSCOSMOS) × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove |
|---|---|---|---|
| Flights | 35 | 714 | 122 |
| Success rate | 100% | 97.2% | 94.3% |
| Thrust | 2,260 kN | — | 2,713 kN |
| Height | 53 m | 51.1 m | 39.27 m |
| Diameter | 4 m | 2.95 m | 3 m |
| Launch mass | 285 t | 313 t | 189 t |
| LEO capacity | 10,000 kg | 6,900 kg | 4,100 kg |
| GTO capacity | 4,100 kg | — | — |
| Launch cost | $90M | — | $15M |
| Reusable | No | No | No |
| Stages | 2 | 3 | 3 |