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 | Space Shuttle National Aeronautics and Space Administration × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|---|
| Flights | 1 | 135 | 122 | 105 |
| Success rate | 0% | 98.5% | 94.3% | 98.1% |
| Thrust | 887 kN | 28,200 kN | 2,713 kN | 2,366 kN |
| Height | 28.9 m | 56.1 m | 39.27 m | 39.7 m |
| Diameter | 1.61 m | 8 m | 3 m | 3 m |
| Launch mass | 60 t | 2,030 t | 189 t | 182 t |
| LEO capacity | 645 kg | 27,500 kg | 4,100 kg | 2,820 kg |
| GTO capacity | — | — | — | — |
| Launch cost | $10.5M | $450M | $15M | $12M |
| Reusable | No | Yes | No | No |
| Stages | 5 | 2 | 3 | 3 |