Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Mu-3S-II Institute of Space and Astronautical Science × remove | Proton K/DM-2 Khrunichev State Research and Production Space Center × remove |
|---|---|---|
| Flights | 8 | 110 |
| Success rate | 87.5% | 93.6% |
| Thrust | 1,930 kN | — |
| Height | 27.8 m | — |
| Diameter | 1.41 m | — |
| Launch mass | 61 t | — |
| LEO capacity | 800 kg | — |
| GTO capacity | — | — |
| Launch cost | — | — |
| Reusable | No | No |
| Stages | 4 | — |