| Manufacturer | Vought |
| Model | XF8U-3 Crusader III |
| Modification | XF8U-3 |
| Country | USA |
| Years | 1958 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.86 m |
| Length | 17.88 m |
| Height | 4.98 m |
| Wing area | 41.81 m2 |
| Zero fuel weight | - |
| Empty weight | 9916 kg |
| Maximum takeoff weight | 17171 kg |
| Normal takeoff weight | 14659 kg |
| Flight duration | - |
| Engine | 1ТРДФ Pratt Whitney J75-P-5A/6 |
| Power | - |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 925 km/h |
| Rate of climb | - |
| Practical range | 3289 km |
| Service ceiling | 18288 m |
| Hovering ceiling | - |
| Crew | 1 |
