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Start | Caudron | C.23



Caudron C.23


General information


ManufacturerCaudron
ModelC.23
ModificationC.23
CountryFrance
Years1918
TypeBomber
Main rotor diameter-
Tail rotor diameter-
Wingspan24.50 m
Length13.00 m
Height3.40 m
Wing area105.00 m2
Zero fuel weight-
Empty weight2341 kg
Maximum takeoff weight-
Normal takeoff weight4170 kg
Flight duration-
Engine2 Salmson CU 9Z
Power2 x 260 HP
Thrust-
Maximum speed144 km/h
Cruising speed122 km/h
Rate of climb-
Practical range-
Service ceiling4500 m
Hovering ceiling-
Crew2
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