Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | H-IIA 204 Mitsubishi Heavy Industries × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove | Voskhod Soviet Space Program × remove | Electron Rocket Lab × remove |
|---|---|---|---|---|
| Flights | 5 | 122 | 299 | 91 |
| Success rate | 100% | 94.3% | 95.7% | 95.6% |
| Thrust | 2,260 kN | 2,713 kN | — | 162 kN |
| Height | 53 m | 39.27 m | — | 18 m |
| Diameter | 4 m | 3 m | — | 1.2 m |
| Launch mass | 445 t | 189 t | — | 13 t |
| LEO capacity | — | 4,100 kg | — | 300 kg |
| GTO capacity | 6,000 kg | — | — | — |
| Launch cost | $90M | $15M | — | $6M |
| Reusable | No | No | No | No |
| Stages | 2 | 3 | — | 3 |