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Start | Hillson | Bi-Mono


General information


ManufacturerHillson
ModelBi-Mono
ModificationBi-Mono
CountryUnited Kingdom
Years1941
TypeExperimental aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan6.10 m
Length4.40 m
Height-
Wing area12.26 m2
Zero fuel weight-
Empty weight-
Maximum takeoff weight-
Normal takeoff weight-
Flight duration-
Engine1 de Havilland Gipsy Six
Power1 x 200 HP
Thrust-
Maximum speed185 km/h
Cruising speed-
Rate of climb-
Practical range-
Service ceiling-
Hovering ceiling-
Crew-
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