| Manufacturer | Leduc |
| Model | Leduc 0.10 |
| Modification | Leduc 0.10 |
| Country | France |
| Years | 1949 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.25 m |
| Length | 10.52 m |
| Height | 3.40 m |
| Wing area | 16.00 m2 |
| Zero fuel weight | - |
| Empty weight | 1800 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 3000 kg |
| Flight duration | - |
| Engine | 1 ПВРД Leduc |
| Power | - |
| Thrust | 1 x 2000 kN |
| Maximum speed | 902 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
