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| Specification | UR-500 Khrunichev State Research and Production Space Center × remove |
|---|---|
| Flights | 4 |
| Success rate | 75% |
| 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 |
| Stages | 2 |