| Manufacturer | SAI Ambrosini |
| Model | Sagittario |
| Modification | Sagittario II |
| Country | Italy |
| Years | 1953 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 7.50 m |
| Length | 8.50 m |
| Height | 2.02 m |
| Wing area | 14.73 m2 |
| Zero fuel weight | - |
| Empty weight | 1978 kg |
| Maximum takeoff weight | 3293 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 ТРД Rolls-Royce Derwent 9 |
| Power | - |
| Thrust | 1 x 16.00 kN |
| Maximum speed | 1060 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 420 km |
| Service ceiling | 14000 m |
| Hovering ceiling | - |
| Crew | - |
