Manufacturer | LKL |
Model | LKL-2 |
Modification | LKL-2 |
Country | Poland |
Years | 1930 |
Type | Light aircraft |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 11.50 m |
Length | 7.00 m |
Height | 2.54 m |
Wing area | 18.54 m2 |
Zero fuel weight | - |
Empty weight | 438 kg |
Maximum takeoff weight | 842 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 1 Walter Vega |
Power | 1 x 85 HP |
Thrust | - |
Maximum speed | 150 km/h |
Cruising speed | 130 km/h |
Rate of climb | - |
Practical range | 600 km |
Service ceiling | 4300 m |
Hovering ceiling | - |
Crew | 3 |