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Start | Soldenhoff | So.A


General information


ManufacturerSoldenhoff
ModelSo.A
ModificationSo.A (D-2156)
CountrySwitzerland
Years1929
TypeExperimental aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan10.00 m
Length5.00 m
Height-
Wing area17.50 m2
Zero fuel weight-
Empty weight260 kg
Maximum takeoff weight-
Normal takeoff weight540 kg
Flight duration-
Engine1 Salmson
Power1 x 40 HP
Thrust-
Maximum speed160 km/h
Cruising speed130 km/h
Rate of climb-
Practical range-
Service ceiling-
Hovering ceiling-
Crew2
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