Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Lockheed XFV-1 Vertical Take-Off and Landing (VTOL) Navy Fighter Aircraft Prototype.
1 x Allison XT40-A-14 turboprop engine developing 7,000 horsepower while driving 2 x three-bladed propeller units in the nose in contra-rotating fashion.
Propulsion
581 mph
935 kph | 505 kts
Max Speed
42,979 ft
13,100 m | 8 miles
Service Ceiling
419 miles
675 km | 364 nm
Operational Range
10,820 ft/min
3,298 m/min
Rate-of-Climb