Thursday, September 18, 2014

Northrop F-5E Tiger II

Wiki:http://en.wikipedia.org/wiki/Northrop_F-5




M39A2 cannon in the nose of a Brazilian F-5
Data from Quest for Performance[142]
General characteristics
Crew: 1
Length: 47 ft 4¾ in (14.45 m)
Wingspan: 26 ft 8 in (8.13 m)
Height: 13 ft 4½ in (4.08 m)
Wing area: 186 ft² (17.28 m²)
Airfoil: NACA 65A004.8 root, NACA 64A004.8 tip
Empty weight: 9,558 lb (4,349 kg)
Loaded weight: 15,745 lb (7,157 kg)
Max. takeoff weight: 24,722 lb (11,214 kg)
Powerplant: 2 × General Electric J85-GE-21B turbojet
Dry thrust: 3,500 lbf (15.5 kN) each
Thrust with afterburner: 5,000 lbf (22.2 kN) each
Zero-lift drag coefficient: 0.0200
Drag area: 3.4 ft² (0.32 m²)
Aspect ratio: 3.86
Internal fuel: 677 U.S. gal (2,563 L)
External fuel: 275 U.S. gal (1,040 L) per tank in up to 3 tanks
Performance
  1. Maximum speed: 917 kn (Mach 1.6, 1,060 mph, 1,700 km/h) ; at altitude
  2. Range: 760 nmi (870 mi, 1,405 km)
  3. Ferry range: 2,010 nmi (2,310 mi, 3,700 km[143])
  4. Service ceiling: 51,800 ft (15,800 m)
  5. Rate of climb: 34,400 ft/min (175 m/s)
  6. Lift-to-drag ratio: 10.0
Armament
Avionics





























End

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