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 |
|---|---|
| Flights | 1 |
| Success rate | 100% |
| Thrust | 500 kN |
| Height | 22.7 m |
| Diameter | 1.8 m |
| Launch mass | 47 t |
| LEO capacity | — |
| GTO capacity | — |
| Launch cost | — |
| Reusable | No |
| Stages | — |