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Start | CPA | CPA-1


General information


ManufacturerCPA
ModelCPA-1
ModificationCPA-1
CountryFrance
Years1926
TypeBomber
Main rotor diameter-
Tail rotor diameter-
Wingspan22.80 m
Length14.50 m
Height4.32 m
Wing area84.00 m2
Zero fuel weight-
Empty weight3350 kg
Maximum takeoff weight-
Normal takeoff weight4600 kg
Flight duration-
Engine2 Hispano-Suiza 12 Ha
Power1 x 450 HP
Thrust-
Maximum speed195 km/h
Cruising speed158 km/h
Rate of climb-
Practical range-
Service ceiling7000 m
Hovering ceiling-
Crew-
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