Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Minotaur IV HAPS Orbital Sciences Corporation × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove | Vostok 8A92M RKK Energiya × remove |
|---|---|---|---|
| Flights | 1 | 105 | 93 |
| Success rate | 100% | 98.1% | 98.9% |
| Thrust | 2,200 kN | 2,366 kN | 3,996 kN |
| Height | 23.9 m | 39.7 m | 30.84 m |
| Diameter | 2.35 m | 3 m | 2.99 m |
| Launch mass | 86 t | 182 t | 282 t |
| LEO capacity | 1,750 kg | 2,820 kg | 3,800 kg |
| GTO capacity | 0 kg | — | — |
| Launch cost | — | $12M | — |
| Reusable | No | No | No |
| Stages | 5 | 3 | 2 |