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 | Space Shuttle National Aeronautics and Space Administration × remove |
|---|---|---|---|
| Flights | 1 | 110 | 135 |
| Success rate | 0% | 93.6% | 98.5% |
| Thrust | 887 kN | — | 28,200 kN |
| Height | 28.9 m | — | 56.1 m |
| Diameter | 1.61 m | — | 8 m |
| Launch mass | 60 t | — | 2,030 t |
| LEO capacity | 645 kg | — | 27,500 kg |
| GTO capacity | — | — | — |
| Launch cost | $10.5M | — | $450M |
| Reusable | No | No | Yes |
| Stages | 5 | — | 2 |