Manufacturer | Aero |
Model | A-101 Oca |
Modification | A.101 |
Country | Czechoslovakia |
Years | 1934 |
Type | Bomber |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 16.99 m |
Length | 12.09 m |
Height | 3.73 m |
Wing area | 58.72 m2 |
Zero fuel weight | - |
Empty weight | 2578 kg |
Maximum takeoff weight | - |
Normal takeoff weight | 4345 kg |
Flight duration | - |
Engine | 1 Praga (Isotta-Fraschini) |
Power | 1 x 990 HP |
Thrust | - |
Maximum speed | 265 km/h |
Cruising speed | 212 km/h |
Rate of climb | - |
Practical range | 845 km |
Service ceiling | 5500 m |
Hovering ceiling | - |
Crew | - |