Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Thor Delta J McDonnell Douglas × remove | Proton K/DM-2 Khrunichev State Research and Production Space Center × remove | Electron Rocket Lab × remove |
|---|---|---|---|
| Flights | 1 | 110 | 91 |
| Success rate | 100% | 93.6% | 95.6% |
| Thrust | 1,452 kN | — | 162 kN |
| Height | 31 m | — | 18 m |
| Diameter | 2.44 m | — | 1.2 m |
| Launch mass | 69 t | — | 13 t |
| LEO capacity | 260 kg | — | 300 kg |
| GTO capacity | 263 kg | — | — |
| Launch cost | $16.6M | — | $6M |
| Reusable | No | No | No |
| Stages | 4 | — | 3 |