Compare rockets
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| Specification | Start Moscow Institute of Thermal Technology × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove | Voskhod Soviet Space Program × remove | Long March 2D China Aerospace Science and Technology Corporation × remove |
|---|---|---|---|---|
| Flights | 1 | 122 | 299 | 100 |
| Success rate | 0% | 94.3% | 95.7% | 99% |
| Thrust | 887 kN | 2,713 kN | — | 2,962 kN |
| Height | 28.9 m | 39.27 m | — | 38.3 m |
| Diameter | 1.61 m | 3 m | — | 3.35 m |
| Launch mass | 60 t | 189 t | — | 232 t |
| LEO capacity | 645 kg | 4,100 kg | — | 3,500 kg |
| GTO capacity | — | — | — | 0 kg |
| Launch cost | $10.5M | $15M | — | $30M |
| Reusable | No | No | No | No |
| Stages | 5 | 3 | — | 2 |