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Engineering-Division PW-1


General information


ManufacturerEngineering Division
ModelPW-1
ModificationPW-1
CountryUSA
Years1921
TypeFighter
Main rotor diameter-
Tail rotor diameter-
Wingspan9.75 m
Length6.86 m
Height2.54 m
Wing area24.99 m2
Zero fuel weight-
Empty weight938 kg
Maximum takeoff weight-
Normal takeoff weight1363 kg
Flight duration2.5 h
Engine1 Packard 1A-1237
Power1 x 350 HP
Thrust-
Maximum speed235 km/h
Cruising speed211 km/h
Rate of climb-
Practical range-
Service ceiling-
Hovering ceiling-
Crew-
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