Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Start-1.2 Moscow Institute of Thermal Technology × remove | Space Shuttle National Aeronautics and Space Administration × remove | Long March 2D China Aerospace Science and Technology Corporation × remove |
|---|---|---|---|
| Flights | 1 | 135 | 100 |
| Success rate | 100% | 98.5% | 99% |
| Thrust | 500 kN | 28,200 kN | 2,962 kN |
| Height | 22.7 m | 56.1 m | 38.3 m |
| Diameter | 1.8 m | 8 m | 3.35 m |
| Launch mass | 47 t | 2,030 t | 232 t |
| LEO capacity | — | 27,500 kg | 3,500 kg |
| GTO capacity | — | — | 0 kg |
| Launch cost | — | $450M | $30M |
| Reusable | No | Yes | No |
| Stages | — | 2 | 2 |