Manufacturer | Heliopolis |
Model | Gomhouria |
Modification | Gomhouria Mk.8 |
Country | Egypt |
Years | 1952 |
Type | Other |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 10.60 m |
Length | 7.85 m |
Height | 2.05 m |
Wing area | 13.50 m2 |
Zero fuel weight | - |
Empty weight | 520 kg |
Maximum takeoff weight | 800 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 1 Teledyne Continental O-300-A |
Power | 1 x 145 HP |
Thrust | - |
Maximum speed | 225 km/h |
Cruising speed | 205 km/h |
Rate of climb | - |
Practical range | 780 km |
Service ceiling | 6000 m |
Hovering ceiling | - |
Crew | 2 |