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| Specification | UR-500 Khrunichev State Research and Production Space Center × remove | Proton K/DM-2 Khrunichev State Research and Production Space Center × remove |
|---|---|---|
| Flights | 4 | 110 |
| Success rate | 75% | 93.6% |
| Thrust | 8,847 kN | — |
| Height | 46.28 m | — |
| Diameter | 4.15 m | — |
| Launch mass | 595 t | — |
| LEO capacity | 8,400 kg | — |
| GTO capacity | — | — |
| Launch cost | — | — |
| Reusable | No | No |
| Stages | 2 | — |