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 | Electron Rocket Lab × remove | Proton K/DM-2 Khrunichev State Research and Production Space Center × remove |
|---|---|---|---|
| Flights | 35 | 91 | 110 |
| Success rate | 100% | 95.6% | 93.6% |
| Thrust | 2,260 kN | 162 kN | — |
| Height | 53 m | 18 m | — |
| Diameter | 4 m | 1.2 m | — |
| Launch mass | 285 t | 13 t | — |
| LEO capacity | 10,000 kg | 300 kg | — |
| GTO capacity | 4,100 kg | — | — |
| Launch cost | $90M | $6M | — |
| Reusable | No | No | No |
| Stages | 2 | 3 | — |