Start | Letov | S-239

Letov S-239


General information


ManufacturerLetov
ModelS-239
ModificationS-239
CountryCzechoslovakia
Years1933
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan10.00 m
Length6.14 m
Height-
Wing area14.00 m2
Zero fuel weight-
Empty weight375 kg
Maximum takeoff weight580 kg
Normal takeoff weight-
Flight duration-
Engine1 Walter Minor 4
Power1 x 85 HP
Thrust-
Maximum speed174 km/h
Cruising speed140 km/h
Rate of climb-
Practical range420 km
Service ceiling4700 m
Hovering ceiling-
Crew2