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Start | Sud Ouest | SO.9000 Trident


General information


ManufacturerSud-Ouest
ModelSO.9000 Trident
ModificationSO-9000
CountryFrance
Years1953
TypeExperimental aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan7.57 m
Length14.37 m
Height2.84 m
Wing area16.58 m2
Zero fuel weight-
Empty weight2435 kg
Maximum takeoff weight5055 kg
Normal takeoff weight-
Flight duration-
Engine-
Power-
Thrust-
Maximum speed1780 (M=1.63) km/h
Cruising speed890 km/h
Rate of climb-
Practical range-
Service ceiling15000 m
Hovering ceiling-
Crew1
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