Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Start-1.2 Moscow Institute of Thermal Technology × remove | Long March 2D China Aerospace Science and Technology Corporation × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove |
|---|---|---|---|
| Flights | 1 | 100 | 105 |
| Success rate | 100% | 99% | 98.1% |
| Thrust | 500 kN | 2,962 kN | 2,366 kN |
| Height | 22.7 m | 38.3 m | 39.7 m |
| Diameter | 1.8 m | 3.35 m | 3 m |
| Launch mass | 47 t | 232 t | 182 t |
| LEO capacity | — | 3,500 kg | 2,820 kg |
| GTO capacity | — | 0 kg | — |
| Launch cost | — | $30M | $12M |
| Reusable | No | No | No |
| Stages | — | 2 | 3 |