Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Thor Delta A McDonnell Douglas × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|
| Flights | 2 | 122 | 105 |
| Success rate | 100% | 94.3% | 98.1% |
| Thrust | 667 kN | 2,713 kN | 2,366 kN |
| Height | 31 m | 39.27 m | 39.7 m |
| Diameter | 2.44 m | 3 m | 3 m |
| Launch mass | 50 t | 189 t | 182 t |
| LEO capacity | 250 kg | 4,100 kg | 2,820 kg |
| GTO capacity | 68 kg | — | — |
| Launch cost | $9.59M | $15M | $12M |
| Reusable | No | No | No |
| Stages | 3 | 3 | 3 |