Manufacturer | Hirth |
Model | Hi.27 Acrostar |
Modification | Acrostar Mk.II |
Country | Germany |
Years | 1970 |
Type | Light aircraft |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 8.28 m |
Length | 6.11 m |
Height | 1.78 m |
Wing area | 10.34 m2 |
Zero fuel weight | - |
Empty weight | 485 kg |
Maximum takeoff weight | 700 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 1 Franklin 6A-350-C1 |
Power | 1 x 220 HP |
Thrust | - |
Maximum speed | - |
Cruising speed | 255 km/h |
Rate of climb | - |
Practical range | - |
Service ceiling | 7500 m |
Hovering ceiling | - |
Crew | 1 |