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Bernard HV-41

Bernard HV-42


General information


ManufacturerBernard
ModelHV-41
ModificationHV-42
CountryFrance
Years1929
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan9.20 m
Length7.99 m
Height3.20 m
Wing area12.00 m2
Zero fuel weight-
Empty weight-
Maximum takeoff weight-
Normal takeoff weight1650 kg
Flight duration-
Engine1 Hispano-Suiza Special
Power1 x 1000 HP
Thrust-
Maximum speed450 km/h
Cruising speed-
Rate of climb-
Practical range-
Service ceiling-
Hovering ceiling-
Crew1