Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Saturn I Chrysler × remove | Vostok 8A92M RKK Energiya × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|
| Flights | 10 | 93 | 105 |
| Success rate | 100% | 98.9% | 98.1% |
| Thrust | 6,700 kN | 3,996 kN | 2,366 kN |
| Height | 55 m | 30.84 m | 39.7 m |
| Diameter | 6.6 m | 2.99 m | 3 m |
| Launch mass | 510 t | 282 t | 182 t |
| LEO capacity | 9,100 kg | 3,800 kg | 2,820 kg |
| GTO capacity | — | — | — |
| Launch cost | — | — | $12M |
| Reusable | No | No | No |
| Stages | 3 | 2 | 3 |