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Start | BAC | BAC.221



BAC BAC.221


General information


ManufacturerBAC
ModelBAC.221
ModificationBAC.221
CountryUnited Kingdom
Years1958
TypeExperimental aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan7.62 m
Length17.56 m
Height3.57 m
Wing area45.52 m2
Zero fuel weight-
Empty weight7458 kg
Maximum takeoff weight9063 kg
Normal takeoff weight8400 kg
Flight duration-
Engine1 ТРД Rolls-Royce Avon RA.28R
Power-
Thrust1 x 49.03 kN
Maximum speed1700 km/h
Cruising speed-
Rate of climb-
Practical range650 km
Service ceiling18000 m
Hovering ceiling-
Crew-
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