| Manufacturer | McDonnell Douglas |
| Model | T-45 Goshawk |
| Modification | T-45A |
| Country | USA |
| Years | 1988 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.39 m |
| Length | 11.97 m |
| Height | 4.27 m |
| Wing area | 16.68 m2 |
| Zero fuel weight | - |
| Empty weight | 4263 kg |
| Maximum takeoff weight | 5787 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Rolls-Royce/Turbomeca F405-RR-401 |
| Power | - |
| Thrust | 1 x 26.00 kN |
| Maximum speed | 997 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 1854 km |
| Service ceiling | 12875 m |
| Hovering ceiling | - |
| Crew | 2 |
