NORTHROP F-5 TIGER II

 

Origin:

United States of America

Type:

(F-5E): single-seat fighter;

(F-5F): two-seat advanced trainer

Engine:

Two 5,000 lbst General Electric J85-GE-21 turbojets with afterburning

Specifications:

  • Wingspan: 8.13 m (26 ft 8 in)
  • Length: 14.73 m (48 ft 3¾ in)
  • Height: 4.08 m (13 ft 4½ in)
  • Wing area: 17.3 m² (186 sq ft)
  • Max level speed at high altitude Mach: 1.6
  • Max speed at 11,000 m (36,089 ft): 1,604 km/h (997 mph)
  • Stalling speed flaps and wheels down: 230 km/h (143 mph)
  • Rate of climb at sea level: 2,484 m/min (8,150 ft/min)
  • Time to 9,144 m (30,000 ft): 6.2 mins
  • Service ceiling: 11,735 m (38,500 ft)
  • Tactical radius with 2,857 kg (6,300 lb) ordnance: 305 km (190 miles)
  • Ferry range with drop tanks: 3,720 km (2,314 miles)
  • Take-off run at 7,141 kg (15,745 lb): 610 m (2,000 ft)
  • Landing run: 701 m (2,300 ft)
  • Internal fuel capacity: 2,538 litres (558 Imp gals)
  • Empty weight: 4,349 kg (9,588 lb)
  • Loaded weight: 10,922 kg (24,080 lb)

Photo source: Wikipedia

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