Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Thor Delta E1 McDonnell Douglas × remove | Long March 2D China Aerospace Science and Technology Corporation × remove | Soyuz U Russian Federal Space Agency (ROSCOSMOS) × remove |
|---|---|---|---|
| Flights | 17 | 100 | 714 |
| Success rate | 94.1% | 99% | 97.2% |
| Thrust | 1,450 kN | 2,962 kN | — |
| Height | 28 m | 38.3 m | 51.1 m |
| Diameter | 2.44 m | 3.35 m | 2.95 m |
| Launch mass | 68 t | 232 t | 313 t |
| LEO capacity | 540 kg | 3,500 kg | 6,900 kg |
| GTO capacity | 150 kg | 0 kg | — |
| Launch cost | — | $30M | — |
| Reusable | No | No | No |
| Stages | 4 | 2 | 3 |