Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | H-II Mitsubishi Heavy Industries × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove | Voskhod Soviet Space Program × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove |
|---|---|---|---|---|
| Flights | 7 | 105 | 299 | 122 |
| Success rate | 85.7% | 98.1% | 95.7% | 94.3% |
| Thrust | — | 2,366 kN | — | 2,713 kN |
| Height | 49 m | 39.7 m | — | 39.27 m |
| Diameter | 4 m | 3 m | — | 3 m |
| Launch mass | 260 t | 182 t | — | 189 t |
| LEO capacity | 10,060 kg | 2,820 kg | — | 4,100 kg |
| GTO capacity | 3,930 kg | — | — | — |
| Launch cost | — | $12M | — | $15M |
| Reusable | No | No | No | No |
| Stages | 2 | 3 | — | 3 |