Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Antares 130 Orbital Sciences Corporation × remove | Electron Rocket Lab × remove | Space Shuttle National Aeronautics and Space Administration × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|---|
| Flights | 1 | 91 | 135 | 105 |
| Success rate | 0% | 95.6% | 98.5% | 98.1% |
| Thrust | 3,265 kN | 162 kN | 28,200 kN | 2,366 kN |
| Height | 41.9 m | 18 m | 56.1 m | 39.7 m |
| Diameter | 3.9 m | 1.2 m | 8 m | 3 m |
| Launch mass | 286 t | 13 t | 2,030 t | 182 t |
| LEO capacity | 5,100 kg | 300 kg | 27,500 kg | 2,820 kg |
| GTO capacity | — | — | — | — |
| Launch cost | — | $6M | $450M | $12M |
| Reusable | No | No | Yes | No |
| Stages | 2 | 3 | 2 | 3 |