Compare rockets
Pick up to 4 vehicles to compare specs and flight records side by side. Browse all →
| Specification | Thor Delta A McDonnell Douglas × remove |
|---|---|
| Flights | 2 |
| Success rate | 100% |
| Thrust | 667 kN |
| Height | 31 m |
| Diameter | 2.44 m |
| Launch mass | 50 t |
| LEO capacity | 250 kg |
| GTO capacity | 68 kg |
| Launch cost | $9.59M |
| Reusable | No |
| Stages | 3 |