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Start | IMAM | Ro.58


General information


ManufacturerIMAM
ModelRo.58
ModificationRo.58
CountryItaly
Years1942
TypeFighter
Main rotor diameter-
Tail rotor diameter-
Wingspan13.40 m
Length9.89 m
Height3.39 m
Wing area26.20 m2
Zero fuel weight-
Empty weight4350 kg
Maximum takeoff weight-
Normal takeoff weight6100 kg
Flight duration-
Engine2 Daimler-Benz DB 601A-1
Power2 x 1175 HP
Thrust-
Maximum speed605 km/h
Cruising speed560 km/h
Rate of climb-
Practical range1500 km
Service ceiling9800 m
Hovering ceiling-
Crew-
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