Compare rockets
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| Specification | Delta II 6925 McDonnell Douglas × remove | Long March 2D China Aerospace Science and Technology Corporation × remove | Voskhod Soviet Space Program × remove |
|---|---|---|---|
| Flights | 13 | 100 | 299 |
| Success rate | 100% | 99% | 95.7% |
| Thrust | 3,981 kN | 2,962 kN | — |
| Height | 38.1 m | 38.3 m | — |
| Diameter | 2.44 m | 3.35 m | — |
| Launch mass | 218 t | 232 t | — |
| LEO capacity | 3,981 kg | 3,500 kg | — |
| GTO capacity | 1,446 kg | 0 kg | — |
| Launch cost | — | $30M | — |
| Reusable | No | No | No |
| Stages | 4 | 2 | — |