Compare rockets
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| Specification | Delta 5920-8 McDonnell Douglas × remove |
|---|---|
| Flights | 1 |
| Success rate | 100% |
| Thrust | 3,468 kN |
| Height | 34 m |
| Diameter | 2.44 m |
| Launch mass | 201 t |
| LEO capacity | 3,848 kg |
| GTO capacity | 1,405 kg |
| Launch cost | $34.22M |
| Reusable | No |
| Stages | 3 |