Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Minotaur V Orbital Sciences Corporation × remove | Proton K/DM-2 Khrunichev State Research and Production Space Center × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove |
|---|---|---|---|
| Flights | 1 | 110 | 122 |
| Success rate | 100% | 93.6% | 94.3% |
| Thrust | 1,600 kN | — | 2,713 kN |
| Height | 23.9 m | — | 39.27 m |
| Diameter | 2.35 m | — | 3 m |
| Launch mass | 36 t | — | 189 t |
| LEO capacity | 1,735 kg | — | 4,100 kg |
| GTO capacity | 0 kg | — | — |
| Launch cost | — | — | $15M |
| Reusable | No | No | No |
| Stages | 5 | — | 3 |