Compare rockets
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| Specification | H-II Mitsubishi Heavy Industries × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove | Proton K/DM-2 Khrunichev State Research and Production Space Center × remove |
|---|---|---|---|
| Flights | 7 | 122 | 110 |
| Success rate | 85.7% | 94.3% | 93.6% |
| Thrust | — | 2,713 kN | — |
| Height | 49 m | 39.27 m | — |
| Diameter | 4 m | 3 m | — |
| Launch mass | 260 t | 189 t | — |
| LEO capacity | 10,060 kg | 4,100 kg | — |
| GTO capacity | 3,930 kg | — | — |
| Launch cost | — | $15M | — |
| Reusable | No | No | No |
| Stages | 2 | 3 | — |