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 | Space Shuttle National Aeronautics and Space Administration × remove | Voskhod Soviet Space Program × remove | Electron Rocket Lab × remove |
|---|---|---|---|---|
| Flights | 35 | 135 | 299 | 91 |
| Success rate | 100% | 98.5% | 95.7% | 95.6% |
| Thrust | 2,260 kN | 28,200 kN | — | 162 kN |
| Height | 53 m | 56.1 m | — | 18 m |
| Diameter | 4 m | 8 m | — | 1.2 m |
| Launch mass | 285 t | 2,030 t | — | 13 t |
| LEO capacity | 10,000 kg | 27,500 kg | — | 300 kg |
| GTO capacity | 4,100 kg | — | — | — |
| Launch cost | $90M | $450M | — | $6M |
| Reusable | No | Yes | No | No |
| Stages | 2 | 2 | — | 3 |