Overview
The Lockheed U-2 Dragon Lady is a high-altitude reconnaissance aircraft developed for intelligence gathering missions. Designed during the Cold War, it is capable of sustained flight at extreme altitudes. The aircraft remains in service after decades of modernization.
Live Fleet Activity (U2)
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Specifications
Units
- Engine
- 1 × General Electric F118-101
- Engine type
- Turbofan
- Thrust
- 17,000 lbf · 76 kN
- Avionics
- Raytheon ASARS 2 , Collins Aerospace SYERS-2C cameras
- Wing tips
- No winglets
- Seats
- 2 economy · 1 business
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 63 ft 0 in · 19.20 m
- Tail height
- 16 ft 8 in · 5.09 m
- Fuselage diameter
- —
- Wing span
- 103 ft 0 in · 31.40 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 40,000 lb · 18,100 kg
- Max landing weight
- —
- Max payload
- 5,000 lb · 2,250 kg
- Fuel capacity
- 2,950 gal · 11,200 L · 8,900 kg (Jet A)
- Max cruise speed
- 413 kt · 475 mph · 765 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 6,090 nm · 7,010 mi · 11,280 km
- Fuel burn
- 1.89 nm/gal · 0.92 km/L
- Ceiling
- 70,000 ft · 21,300 m
- Rate of climb
- 9,000 ft/min · 46 m/s
- Takeoff distance
- —
- Landing distance
- —
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