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Westland Limousine I


General information


ManufacturerWestland
ModelLimousine
ModificationLimousine I
CountryUnited Kingdom
Years1919
TypeTransport aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan11.51 m
Length8.46 m
Height3.30 m
Wing area40.88 m2
Zero fuel weight-
Empty weight990 kg
Maximum takeoff weight1535 kg
Normal takeoff weight-
Flight duration-
Engine1 Rolls-Royce Falcon III
Power1 x 275 HP
Thrust-
Maximum speed145 km/h
Cruising speed121 km/h
Rate of climb-
Practical range467 km
Service ceiling5182 m
Hovering ceiling-
Crew-