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Start | Arup | Arup S-1(4)



Arup Arup S-1(4)


General information


ManufacturerArup
ModelArup S-1(4)
ModificationS-2
CountryUSA
Years1932
TypeExperimental aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan5.80 m
Length4.80 m
Height-
Wing area19.00 m2
Zero fuel weight-
Empty weight-
Maximum takeoff weight350 kg
Normal takeoff weight-
Flight duration-
Engine1 Continental А-40
Power1 x 36 HP
Thrust-
Maximum speed155 km/h
Cruising speed-
Rate of climb-
Practical range-
Service ceiling-
Hovering ceiling-
Crew-
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