| Manufacturer | Renard |
| Model | R-38 |
| Modification | R-38 |
| Country | Belgium |
| Years | 1939 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.64 m |
| Length | 8.80 m |
| Height | 2.90 m |
| Wing area | 20.00 m2 |
| Zero fuel weight | - |
| Empty weight | 1950 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 2600 kg |
| Flight duration | - |
| Engine | 1 Rolls-Royce Merlin II |
| Power | 1 x 1020 HP |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 486 km/h |
| Rate of climb | 980 m/min |
| Practical range | 1350 km |
| Service ceiling | 12900 m |
| Hovering ceiling | - |
| Crew | - |
