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Northrop F-5E Tiger II
Specifications
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)
Max takeoff weight: 24,664 lb (11,187 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 US gal (2,563 L)
External fuel: 275 US gal (1,040 L) per tank in up to 3 tanks
Performance
Maximum speed: 917 kn (1,060 mph, 1,700 km/h, Mach 1.6)
Range: 760 nmi (870 mi, 1,405 km)
Ferry range: 2,010 nmi (2,310 mi, 3,700 km)
Service ceiling: 51,800 ft (15,800 m)
Rate of climb: 34,400 ft/min (175 m/s)
Lift-to-drag ratio: 10.0
Armament
Guns: 2× 20 mm (0.787 in) Pontiac M39A2 cannons in the nose, 280 rounds/gun
Hardpoints: 7 total (3× wet): 2× wing-tip AAM launch rails, 4× under-wing & 1× under-fuselage pylon stations holding up to 7,000 pounds (3,200 kg) of payload.
Rockets:
2× LAU-61/LAU-68 rocket pods (each with 19× /7× Hydra 70 mm rockets, respectively); or
2× LAU-5003 rocket pods (each with 19× CRV7 70 mm rockets); or
2× LAU-10 rocket pods (each with 4× Zuni 127 mm rockets); or
2× Matra rocket pods (each with 18× SNEB 68 mm rockets)
Missiles:
Air-to-air missile:
4× AIM-9 Sidewinders or
4× AIM-120 AMRAAMs
Air-to-surface missile:
2× AGM-65 Mavericks
Bombs: A variety of air-to-ground ordnance such as the Mark 80 series of unguided iron bombs (including 3 kg and 14 kg practice bombs), CBU-24/49/52/58 cluster bomb munitions, napalm bomb canisters and M129 Leaflet bomb
Others: up to 3× 150/275 US gallon Sargent Fletcher drop tanks for ferry flight or extended range/loitering time.
Avionics
Emerson Electric AN/APQ-153 radar on early batch of F-5E
Emerson Electric AN/APQ-159 radar on later production F-5E
Data from Quest for Performance
Northrop F-5E Tiger II
Specifications
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)
Max takeoff weight: 24,664 lb (11,187 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 US gal (2,563 L)
External fuel: 275 US gal (1,040 L) per tank in up to 3 tanks
Performance
Maximum speed: 917 kn (1,060 mph, 1,700 km/h, Mach 1.6)
Range: 760 nmi (870 mi, 1,405 km)
Ferry range: 2,010 nmi (2,310 mi, 3,700 km)
Service ceiling: 51,800 ft (15,800 m)
Rate of climb: 34,400 ft/min (175 m/s)
Lift-to-drag ratio: 10.0
Armament
Guns: 2× 20 mm (0.787 in) Pontiac M39A2 cannons in the nose, 280 rounds/gun
Hardpoints: 7 total (3× wet): 2× wing-tip AAM launch rails, 4× under-wing & 1× under-fuselage pylon stations holding up to 7,000 pounds (3,200 kg) of payload.
Rockets:
2× LAU-61/LAU-68 rocket pods (each with 19× /7× Hydra 70 mm rockets, respectively); or
2× LAU-5003 rocket pods (each with 19× CRV7 70 mm rockets); or
2× LAU-10 rocket pods (each with 4× Zuni 127 mm rockets); or
2× Matra rocket pods (each with 18× SNEB 68 mm rockets)
Missiles:
Air-to-air missile:
4× AIM-9 Sidewinders or
4× AIM-120 AMRAAMs
Air-to-surface missile:
2× AGM-65 Mavericks
Bombs: A variety of air-to-ground ordnance such as the Mark 80 series of unguided iron bombs (including 3 kg and 14 kg practice bombs), CBU-24/49/52/58 cluster bomb munitions, napalm bomb canisters and M129 Leaflet bomb
Others: up to 3× 150/275 US gallon Sargent Fletcher drop tanks for ferry flight or extended range/loitering time.
Avionics
Emerson Electric AN/APQ-153 radar on early batch of F-5E
Emerson Electric AN/APQ-159 radar on later production F-5E
Data from Quest for Performance
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