Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Antares 230 Northrop Grumman Space Systems × remove | Voskhod Soviet Space Program × remove | Soyuz U Russian Federal Space Agency (ROSCOSMOS) × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|---|
| Flights | 5 | 299 | 714 | 105 |
| Success rate | 100% | 95.7% | 97.2% | 98.1% |
| Thrust | 3,844 kN | — | — | 2,366 kN |
| Height | 42.5 m | — | 51.1 m | 39.7 m |
| Diameter | 3.9 m | — | 2.95 m | 3 m |
| Launch mass | 286 t | — | 313 t | 182 t |
| LEO capacity | 7,800 kg | — | 6,900 kg | 2,820 kg |
| GTO capacity | — | — | — | — |
| Launch cost | — | — | — | $12M |
| Reusable | No | No | No | No |
| Stages | 3 | — | 3 | 3 |