Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Start Moscow Institute of Thermal Technology × remove | Long March 3B/E China Aerospace Science and Technology Corporation × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|
| Flights | 1 | 77 | 105 |
| Success rate | 0% | 97.4% | 98.1% |
| Thrust | 887 kN | 5,924 kN | 2,366 kN |
| Height | 28.9 m | 56.3 m | 39.7 m |
| Diameter | 1.61 m | 3.35 m | 3 m |
| Launch mass | 60 t | 456 t | 182 t |
| LEO capacity | 645 kg | 12,000 kg | 2,820 kg |
| GTO capacity | — | 5,500 kg | — |
| Launch cost | $10.5M | $70M | $12M |
| Reusable | No | No | No |
| Stages | 5 | 3 | 3 |