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Start | Handley Page | HP.39 Gugnunc



Handley-Page HP.39 Gugnunc


General information


ManufacturerHandley Page
ModelHP.39 Gugnunc
ModificationHP.39
CountryUnited Kingdom
Years1912
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan12.20 m
Length7.85 m
Height-
Wing area27.22 m2
Zero fuel weight-
Empty weight619 kg
Maximum takeoff weight989 kg
Normal takeoff weight-
Flight duration-
Engine1 Armstrong Siddeley Mongoose I
Power1 x 150 HP
Thrust-
Maximum speed180 km/h
Cruising speed156 km/h
Rate of climb-
Practical range-
Service ceiling-
Hovering ceiling-
Crew2
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