Overview
The Northrop F-5 Tiger is a lightweight supersonic fighter developed for both U.S. and export markets. Designed to be simple, reliable, and cost-effective, it achieved widespread global adoption. The aircraft served in numerous air forces over several decades.
Live Fleet Activity (F5)
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Specifications
Units
- Engine
- 2 × General Electric J85-GE-21B turbojet
- Engine type
- Jet
- Thrust
- 2 × 5,000 lbf · 22 kN
- Avionics
- Emerson Electric AN/APQ-153/157/159, AN/APG-69
- Wing tips
- No winglets
- Seats
- 1
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 47 ft 5 in · 14.45 m
- Tail height
- 13 ft 4 in · 4.06 m
- Fuselage diameter
- 3 ft 3 in · 1.00 m
- Wing span
- 26 ft 8 in · 8.13 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 24,700 lb · 11,200 kg
- Max landing weight
- —
- Max payload
- 7,050 lb · 3,200 kg
- Fuel capacity
- 700 gal · 2,600 L · 2,100 kg (Jet A)
- Max cruise speed
- 938 kt · 1,079 mph · 1,737 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 124 kt · 143 mph · 230 km/h
- Range
- 2,010 nm · 2,310 mi · 3,720 km
- Fuel burn
- 3.30 nm/gal · 1.61 km/L
- Ceiling
- 51,800 ft · 15,800 m
- Rate of climb
- 34,500 ft/min · 175 m/s
- Takeoff distance
- 2,900 ft · 880 m
- Landing distance
- 2,500 ft · 760 m
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