Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Delta 3920/PAM McDonnell Douglas × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|
| Flights | 6 | 122 | 105 |
| Success rate | 100% | 94.3% | 98.1% |
| Thrust | 3,188 kN | 2,713 kN | 2,366 kN |
| Height | 36 m | 39.27 m | 39.7 m |
| Diameter | 2.44 m | 3 m | 3 m |
| Launch mass | 191 t | 189 t | 182 t |
| LEO capacity | 1,280 kg | 4,100 kg | 2,820 kg |
| GTO capacity | — | — | — |
| Launch cost | — | $15M | $12M |
| Reusable | No | No | No |
| Stages | 4 | 3 | 3 |