Compare rockets
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| Specification | Antares 120 Orbital Sciences Corporation × remove | Voskhod Soviet Space Program × remove | Vostok 8A92M RKK Energiya × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|---|
| Flights | 2 | 299 | 93 | 105 |
| Success rate | 100% | 95.7% | 98.9% | 98.1% |
| Thrust | 3,265 kN | — | 3,996 kN | 2,366 kN |
| Height | 40.5 m | — | 30.84 m | 39.7 m |
| Diameter | 3.9 m | — | 2.99 m | 3 m |
| Launch mass | 276 t | — | 282 t | 182 t |
| LEO capacity | 4,600 kg | — | 3,800 kg | 2,820 kg |
| GTO capacity | — | — | — | — |
| Launch cost | $80M | — | — | $12M |
| Reusable | No | No | No | No |
| Stages | 2 | — | 2 | 3 |