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Breda CC.20

Breda СС.20


General information


ManufacturerBreda
ModelCC.20
ModificationСС.20
CountryItaly
Years1929
TypeBomber
Main rotor diameter-
Tail rotor diameter-
Wingspan42.00 m
Length-
Height-
Wing area-
Zero fuel weight-
Empty weight7700 kg
Maximum takeoff weight-
Normal takeoff weight12000 kg
Flight duration-
Engine3 Isotta-Fraschini Asso 500
Power3 x 500 HP
Thrust-
Maximum speed185 km/h
Cruising speed155 km/h
Rate of climb-
Practical range-
Service ceiling-
Hovering ceiling-
Crew-