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Start | CAMS | CAMS 52


General information


ManufacturerCAMS
ModelCAMS 52
ModificationCAMS 52
CountryFrance
Years1930
TypeBomber
Main rotor diameter-
Tail rotor diameter-
Wingspan30.36 m
Length16.00 m
Height4.90 m
Wing area120.00 m2
Zero fuel weight-
Empty weight4400 kg
Maximum takeoff weight7618 kg
Normal takeoff weight-
Flight duration-
Engine2 Gnome & Rhone 9Akx
Power2 x 480 HP
Thrust-
Maximum speed200 km/h
Cruising speed170 km/h
Rate of climb-
Practical range1400 km
Service ceiling5000 m
Hovering ceiling-
Crew5
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