Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Start Moscow Institute of Thermal Technology × 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 | 0% | 93.6% | 94.3% |
| Thrust | 887 kN | — | 2,713 kN |
| Height | 28.9 m | — | 39.27 m |
| Diameter | 1.61 m | — | 3 m |
| Launch mass | 60 t | — | 189 t |
| LEO capacity | 645 kg | — | 4,100 kg |
| GTO capacity | — | — | — |
| Launch cost | $10.5M | — | $15M |
| Reusable | No | No | No |
| Stages | 5 | — | 3 |