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Start | IMAM | Ro.37


General information


ManufacturerIMAM
ModelRo.37
ModificationRo.37bis
CountryItaly
Years1934
TypeReconnaissance plane
Main rotor diameter-
Tail rotor diameter-
Wingspan11.08 m
Length8.56 m
Height3.15 m
Wing area31.35 m2
Zero fuel weight-
Empty weight1587 kg
Maximum takeoff weight-
Normal takeoff weight2420 kg
Flight duration-
Engine1 Piaggio P.IX RC 40
Power1 x 560 HP
Thrust-
Maximum speed330 km/h
Cruising speed-
Rate of climb-
Practical range1120 km
Service ceiling7200 m
Hovering ceiling-
Crew-
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