| Manufacturer | Mitsubishi |
| Model | T-2CCV |
| Modification | T-2CCV |
| Country | Japan |
| Years | 1975 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 7.88 m |
| Length | 17.85 m |
| Height | 4.39 m |
| Wing area | 21.17 m2 |
| Zero fuel weight | - |
| Empty weight | 6310 kg |
| Maximum takeoff weight | 12800 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 ТРД Ishikawajima-Harima TF40-1H1801A |
| Power | - |
| Thrust | - |
| Maximum speed | 1204 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 2400 km |
| Service ceiling | 14800 m |
| Hovering ceiling | - |
| Crew | 1 |
