Compare rockets
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| Specification | Delta 3914 McDonnell Douglas × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove | Vostok 8A92M RKK Energiya × remove |
|---|---|---|---|
| Flights | 12 | 122 | 93 |
| Success rate | 83.3% | 94.3% | 98.9% |
| Thrust | 3,046 kN | 2,713 kN | 3,996 kN |
| Height | 35 m | 39.27 m | 30.84 m |
| Diameter | 2.44 m | 3 m | 2.99 m |
| Launch mass | 185 t | 189 t | 282 t |
| LEO capacity | 951 kg | 4,100 kg | 3,800 kg |
| GTO capacity | 954 kg | — | — |
| Launch cost | — | $15M | — |
| Reusable | No | No | No |
| Stages | 4 | 3 | 2 |