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| Specification | Proton-M Khrunichev State Research and Production Space Center × remove | Proton K/DM-2 Khrunichev State Research and Production Space Center × remove |
|---|---|---|
| Flights | 1 | 110 |
| Success rate | 100% | 93.6% |
| Thrust | 10,532 kN | — |
| Height | 58.2 m | — |
| Diameter | 7.4 m | — |
| Launch mass | 705 t | — |
| LEO capacity | 23,000 kg | — |
| GTO capacity | 6,920 kg | — |
| Launch cost | $65M | — |
| Reusable | No | No |
| Stages | 3 | — |