| Manufacturer | Rutan, Scaled Composites |
| Model | AD-1 |
| Modification | AD-1 |
| Country | USA |
| Years | 1979 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.75 m |
| Length | 11.80 m |
| Height | 2.06 m |
| Wing area | 8.60 m2 |
| Zero fuel weight | - |
| Empty weight | 658 kg |
| Maximum takeoff weight | 973 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 ТРД Microturbo TRS18-046 |
| Power | - |
| Thrust | 2 x 100 kN |
| Maximum speed | 274 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | - |
