Compare rockets
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| Specification | Delta II 7920-8 McDonnell Douglas × remove |
|---|---|
| Flights | 1 |
| Success rate | 100% |
| Thrust | 4,000 kN |
| Height | 39 m |
| Diameter | 2.44 m |
| Launch mass | 220 t |
| LEO capacity | — |
| GTO capacity | — |
| Launch cost | — |
| Reusable | No |
| Stages | 3 |