| Manufacturer | de Havilland |
| Model | D.H.112 Venom |
| Modification | DH.112 |
| Country | United Kingdom |
| Years | 1949 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 12.7 m |
| Length | 10.1 m |
| Height | 1.9 m |
| Wing area | 25.9 m2 |
| Zero fuel weight | - |
| Empty weight | - |
| Maximum takeoff weight | - |
| Normal takeoff weight | 7150 kg |
| Flight duration | - |
| Engine | 1 ТРД de Havilland Gnost |
| Power | - |
| Thrust | 23.5 kN |
| Maximum speed | 920 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 1100 km |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
