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| Manufacturer | Caproni |
| Model | Caproni-Campini N.1 (CC.2) |
| Modification | Caproni-Campini N.1 |
| Country | Italy |
| Years | 1940 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 15.85 m |
| Length | 13.10 m |
| Height | 4.70 m |
| Wing area | 36.00 m2 |
| Zero fuel weight | - |
| Empty weight | 3640 kg |
| Maximum takeoff weight | 4195 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Isotta Fraschini L.121/RC. 40 |
| Power | - |
| Thrust | 1 x 900 kN |
| Maximum speed | 375 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 100 km |
| Service ceiling | 4000 m |
| Hovering ceiling | - |
| Crew | - |
