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Start | Douglas | D-558-II Skyrocket



Douglas D-558-II Skyrocket


General information


ManufacturerDouglas
ModelD-558-II Skyrocket
ModificationD-558-II
CountryUSA
Years1948
TypeExperimental aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan7.62 m
Length13.80 m
Height3.50 m
Wing area16.26 m2
Zero fuel weight-
Empty weight-
Maximum takeoff weight9000 kg
Normal takeoff weight-
Flight duration-
Engine1 ТРД Westinghouse J34-WE-22
Power-
Thrust1 x 13.34 kN
Maximum speed2120 km/h
Cruising speed-
Rate of climb-
Practical range-
Service ceiling25386 m
Hovering ceiling-
Crew-
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