| |
|
| Country:
USA |
|
Type: Fighter |
| Manufacturer:
Northrop |
| Service:
1962 - 2008 |
| First
Flight: 30 July 1959 |
| Production:
2236 |
|
|
|
|
|
|
|
|
The F-5A/B Freedom Fighter and F-5E/F Tiger II are part of a family of widely used light supersonic fighter aircraft, designed and built by Northrop in the United States, beginning in 1960s. Hundreds remain in service in air forces around the world in the early 21st Century, and the type has also been the basis for a number of other aircraft.
The F-5 started life as a privately-funded light fighter program by Northrop in the 1950s. The first generation F-5A Freedom Fighter entered service in the 1960s. Over 800 were produced through 1972 for U.S. allies during the Cold War. The USAF had no need for a light fighter, but it did need a trainer and procured about 1,200 of a derivative airframe for this purpose, the T-38 Talon.
The improved second-generation F-5E Tiger II was also primarily used by American Cold War allies and, in limited quantities, served in US military aviation as a training and aggressor aircraft; Tiger II production amounted to 1,400 of all versions, with production ending in 1987. Many F-5s continuing in service into the 1990s and 2000s have undergone a wide variety of upgrade programs to keep pace with the changing combat environment. The F-5 was also developed into a dedicated reconnaissance version, the RF-5 Tigereye.
The F-5N/F variants remain in service with the United States Navy as an adversary trainer.
|
| TECHNICAL
SPECIFICATIONS ( F-5E Tiger II) |
|
General characteristics
- Crew: 1
- Length: 47 ft 4.75 in (14.45 m)
- Wingspan: 26 ft 8 in (8.13 m)
- Height: 13 ft 4.5 in (4.08 m)
- Wing area: 186 ft (17.28 m)
- 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 x 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 ft (0.32 m)
- 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, 3,720 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 x 20 mm Pontiac M39A2 cannon in the nose, 280 rounds/gun
- Missiles: AIM-7 Sparrow, AIM-9 Sidewinder, AGM-65 Maverick, AIM-120 AMRAAM
- Bombs: M129 Leaflet bomb, 500 lb (225 kg) Mk82, 2,000 lb (900 kg) Mk84,CBU-24/49/52/58 cluster munitions
- Total of up to 7,000 lb (3,200 kg) of ordnance.
|