Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Delta II 6920-10 McDonnell Douglas × remove | Space Shuttle National Aeronautics and Space Administration × remove | Vostok 8A92M RKK Energiya × remove |
|---|---|---|---|
| Flights | 2 | 135 | 93 |
| Success rate | 100% | 98.5% | 98.9% |
| Thrust | 3,790 kN | 28,200 kN | 3,996 kN |
| Height | 39 m | 56.1 m | 30.84 m |
| Diameter | 2.44 m | 8 m | 2.99 m |
| Launch mass | 219 t | 2,030 t | 282 t |
| LEO capacity | — | 27,500 kg | 3,800 kg |
| GTO capacity | — | — | — |
| Launch cost | — | $450M | — |
| Reusable | No | Yes | No |
| Stages | 3 | 2 | 2 |