| Manufacturer | IMAM |
| Model | Ro.1 |
| Modification | Ro.1 |
| Country | Italy |
| Years | 1927 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 15.30 m |
| Length | 9.36 m |
| Height | 3.38 m |
| Wing area | 39.99 m2 |
| Zero fuel weight | - |
| Empty weight | 1275 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 2175 kg |
| Flight duration | - |
| Engine | 1 Bristol Jupiter IV |
| Power | 1 x 420 HP |
| Thrust | - |
| Maximum speed | 255 km/h |
| Cruising speed | 206 km/h |
| Rate of climb | - |
| Practical range | 1200 km |
| Service ceiling | 6000 m |
| Hovering ceiling | - |
| Crew | 2 |
