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Start | Shenyang | CK-1


General information


ManufacturerShenyang
ModelCK-1
ModificationCK-1C
CountryChina
Years1977
TypeUnmanned aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan7.50 m
Length8.44 m
Height2.96 m
Wing area8.55 m2
Zero fuel weight-
Empty weight2000 kg
Maximum takeoff weight3340 kg
Normal takeoff weight-
Flight duration60-70 h
Engine1 ТРД WP6
Power-
Thrust1 x 2600 kN
Maximum speed900 km/h
Cruising speed-
Rate of climb-
Practical range-
Service ceiling18000 m
Hovering ceiling-
Crew-
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