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Start | Central Aircraft | Centaur IV



Central-Aircraft Centaur IV


General information


ManufacturerCentral Aircraft
ModelCentaur IV
ModificationCentaur IVA
CountryUnited Kingdom
Years1919
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan10.43 m
Length7.54 m
Height-
Wing area-
Zero fuel weight-
Empty weight408 kg
Maximum takeoff weight635 kg
Normal takeoff weight-
Flight duration-
Engine1 Anzani
Power1 x 100 HP
Thrust-
Maximum speed121 km/h
Cruising speed105 km/h
Rate of climb-
Practical range-
Service ceiling-
Hovering ceiling-
Crew3
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