Compare rockets
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| Specification | Start Moscow Institute of Thermal Technology × remove | Long March 2D China Aerospace Science and Technology Corporation × remove | Tsiklon-2 Yuzhnoye Design Bureau × remove | Electron Rocket Lab × remove |
|---|---|---|---|---|
| Flights | 1 | 100 | 105 | 91 |
| Success rate | 0% | 99% | 98.1% | 95.6% |
| Thrust | 887 kN | 2,962 kN | 2,366 kN | 162 kN |
| Height | 28.9 m | 38.3 m | 39.7 m | 18 m |
| Diameter | 1.61 m | 3.35 m | 3 m | 1.2 m |
| Launch mass | 60 t | 232 t | 182 t | 13 t |
| LEO capacity | 645 kg | 3,500 kg | 2,820 kg | 300 kg |
| GTO capacity | — | 0 kg | — | — |
| Launch cost | $10.5M | $30M | $12M | $6M |
| Reusable | No | No | No | No |
| Stages | 5 | 2 | 3 | 3 |