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Start | IMAM | Ro.30


General information


ManufacturerIMAM
ModelRo.30
ModificationRo.30
CountryItaly
Years1932
TypeOther
Main rotor diameter-
Tail rotor diameter-
Wingspan15.75 m
Length10.24 m
Height3.50 m
Wing area33.36 m2
Zero fuel weight-
Empty weight1580 kg
Maximum takeoff weight-
Normal takeoff weight2630 kg
Flight duration-
Engine1 Piaggio P.VIII
Power1 x 500 HP
Thrust-
Maximum speed235 km/h
Cruising speed210 km/h
Rate of climb-
Practical range1600 km
Service ceiling7500 m
Hovering ceiling-
Crew3
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