| Manufacturer | Vought |
| Model | F8U-1 (F-8A-B) Crusader |
| Modification | F-8A |
| Country | USA |
| Years | 1955 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.87 m |
| Length | 16.53 m |
| Height | 4.80 m |
| Wing area | 34.84 m2 |
| Zero fuel weight | - |
| Empty weight | 7037 kg |
| Maximum takeoff weight | 12459 kg |
| Normal takeoff weight | 10732 kg |
| Flight duration | - |
| Engine | 1 ТРДФ Pratt Whitney J75-P-4A/12 |
| Power | - |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 917 km/h |
| Rate of climb | - |
| Practical range | 2372 km |
| Service ceiling | 12983 m |
| Hovering ceiling | - |
| Crew | 1 |
