Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Delta 5920-8 McDonnell Douglas × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove |
|---|---|---|---|
| Flights | 1 | 105 | 122 |
| Success rate | 100% | 98.1% | 94.3% |
| Thrust | 3,468 kN | 2,366 kN | 2,713 kN |
| Height | 34 m | 39.7 m | 39.27 m |
| Diameter | 2.44 m | 3 m | 3 m |
| Launch mass | 201 t | 182 t | 189 t |
| LEO capacity | 3,848 kg | 2,820 kg | 4,100 kg |
| GTO capacity | 1,405 kg | — | — |
| Launch cost | $34.22M | $12M | $15M |
| Reusable | No | No | No |
| Stages | 3 | 3 | 3 |