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 | Voskhod Soviet Space Program × remove | Electron Rocket Lab × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|---|
| Flights | 35 | 299 | 91 | 105 |
| Success rate | 100% | 95.7% | 95.6% | 98.1% |
| Thrust | 2,260 kN | — | 162 kN | 2,366 kN |
| Height | 53 m | — | 18 m | 39.7 m |
| Diameter | 4 m | — | 1.2 m | 3 m |
| Launch mass | 285 t | — | 13 t | 182 t |
| LEO capacity | 10,000 kg | — | 300 kg | 2,820 kg |
| GTO capacity | 4,100 kg | — | — | — |
| Launch cost | $90M | — | $6M | $12M |
| Reusable | No | No | No | No |
| Stages | 2 | — | 3 | 3 |