Compare rockets
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| Specification | N-I Mitsubishi Heavy Industries × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove | Proton K/DM-2 Khrunichev State Research and Production Space Center × remove |
|---|---|---|---|
| Flights | 7 | 105 | 110 |
| Success rate | 85.7% | 98.1% | 93.6% |
| Thrust | — | 2,366 kN | — |
| Height | 34 m | 39.7 m | — |
| Diameter | 2.44 m | 3 m | — |
| Launch mass | 131 t | 182 t | — |
| LEO capacity | 1,200 kg | 2,820 kg | — |
| GTO capacity | 360 kg | — | — |
| Launch cost | — | $12M | — |
| Reusable | No | No | No |
| Stages | 3 | 3 | — |