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Engineering-Division VCP-1


General information


ManufacturerEngineering Division
ModelVCP-1
ModificationVCP-1
CountryUSA
Years1919
TypeFighter
Main rotor diameter-
Tail rotor diameter-
Wingspan9.75 m
Length6.81 m
Height2.54 m
Wing area24.99 m2
Zero fuel weight-
Empty weight913 kg
Maximum takeoff weight-
Normal takeoff weight1211 kg
Flight duration-
Engine1 Packard 1A-2025
Power1 x 660 HP
Thrust-
Maximum speed248 km/h
Cruising speed215 km/h
Rate of climb-
Practical range-
Service ceiling-
Hovering ceiling-
Crew1
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