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Start | Central Aircraft | Centaur 2A



Central-Aircraft Centaur 2A


General information


ManufacturerCentral Aircraft
ModelCentaur 2A
ModificationCentaur 2A
CountryUnited Kingdom
Years1919
TypeTransport aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan19.41 m
Length11.96 m
Height3.81 m
Wing area83.15 m2
Zero fuel weight-
Empty weight2271 kg
Maximum takeoff weight-
Normal takeoff weight3289 kg
Flight duration-
Engine2 Beardmore
Power2 x 160 HP
Thrust-
Maximum speed145 km/h
Cruising speed105 km/h
Rate of climb-
Practical range724 km
Service ceiling-
Hovering ceiling-
Crew-
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