Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Piasecki PV-2 Helicopter Technology Demonstrator.
1 x Franklin 4AC-199 4-cylinder piston engine developing 90 horsepower and driving a three-bladed main rotor unit over fuselage and a two-blade rigid tail rotor unit at the rear.
160 kph | 86 kts
240 km | 130 nm