| Manufacturer | Rockwell |
| Model | XFV-12 |
| Modification | XFV-12A |
| Country | USA |
| Years | - |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.69 m |
| Length | 13.39 m |
| Height | 3.15 m |
| Wing area | 27.20 m2 |
| Zero fuel weight | 6259 kg |
| Empty weight | - |
| Maximum takeoff weight | 11000 kg |
| Normal takeoff weight | 8845 kg |
| Flight duration | - |
| Engine | 1 ТРДФ Pratt Whitney F401-PW-40 |
| Power | - |
| Thrust | - |
| Maximum speed | 2200 (M=2) km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
