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Dobkevicius Dobi I

Dobkevicius Dobi-I


General information


ManufacturerDobkevicius
ModelDobi I
ModificationDobi-I
CountryLithuania
Years1922
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan7.90 m
Length4.50 m
Height1.55 m
Wing area7.50 m2
Zero fuel weight-
Empty weight167 kg
Maximum takeoff weight-
Normal takeoff weight300 kg
Flight duration-
Engine1 Haacke HFM-2
Power1 x 30 HP
Thrust-
Maximum speed175 km/h
Cruising speed130 km/h
Rate of climb167 m/min
Practical range-
Service ceiling3800 m
Hovering ceiling-
Crew-