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F-5E Tiger II American Supersonic Light Fighter Aircraft

F-5E

Supersonic Light Fighter Aircraft
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Basic Information
Name
F-5E Tiger II American Supersonic Light Fighter Aircraft
Designation
F-5E
Alternate Designation
Equipment Type
Supersonic Light Fighter Aircraft
Manufacturer
Northrop Grumman
Date of Introduction
1972
Description

F-5E Tiger II Single-seat fighter version with AN/APQ-159 replacing earlier AN/APQ-153 in F-5A. The Northrop F-5 is a family of supersonic light fighter aircraft initially designed as a privately funded project in the late 1950s by Northrop Corporation. There are two main models, the original F-5A and F-5B Freedom Fighter variants and the extensively updated F-5E and F-5F Tiger II variants. The design team wrapped a small, highly aerodynamic fighter around two compact and high-thrust General Electric J85 engines, focusing on performance and a low cost of maintenance. Smaller and simpler than contemporaries such as the McDonnell Douglas F-4 Phantom II, the F-5 cost less to procure and operate, making it a popular export aircraft. Though primarily designed for a day air superiority role, the aircraft is also a capable ground-attack platform. The F-5A entered service in the early 1960s. During the Cold War, over 800 were produced through 1972 for U.S. allies. Though at the time the United States Air Force (USAF) did not have a need for a light fighter, it did procure approximately 1,200 Northrop T-38 Talon trainer aircraft, which were based on Northrop's N-156 fighter design. After winning the International Fighter Aircraft Competition, a program aimed at providing effective low-cost fighters to American allies, 1970 Northrop introduced the second-generation F-5E Tiger II 1972. This upgrade included more powerful engines, larger fuel capacity, greater wing area, improved leading edge extensions for better turn rates, optional air-to-air refueling, and improved avionics including air-to-air radar. Primarily used by American allies, it remains in US service to support training exercises. It has served in a wide array of roles, being able to perform both air and ground attack duties; the type was used extensively in the Vietnam War. A total of 1,400 Tiger IIs were built before production ended in 1987. More than 3,800 F-5s and the closely related T-38 advanced trainer aircraft were produced in Hawthorne, California. The F-5N/F variants are in service with the United States Navy and United States Marine Corps as adversary trainers. Approximately 500 aircraft were in service as of 2014. The F-5 was also developed into a dedicated reconnaissance version, the RF-5 Tigereye. The F-5 also served as a starting point for a series of design studies which resulted in the Northrop YF-17 and the F/A-18 naval fighter aircraft. The Northrop F-20 Tigershark was an advanced variant to succeed the F-5E which was ultimately canceled when export customers did not emerge.

Air & Air Defense Specifications
Crew 1
Engine Turbojet
Max Speed 1733.0 km/h
Cruise Speed 904.0 km/h
Variants
AE.9 Spanish designation of the Northrop F-5B.
F-5-21 Temporary designation for the YF-5B.
YF-5B One F-5B was fitted with a 5,000 lbf (2,268 kgf) General Electric J85-GE-21 engine, and used as a prototype for the F-5E Tiger II.
F-5B Two-seat trainer version.
F-5B(G) Two-seat trainer version of the F-5B for the Royal Norwegian Air Force.
F-5BM Two-seat trainer version in use by the Spanish Air Force for air combat training.
F-5D Unbuilt trainer version.
F-5F Tiger II Two-seat trainer version of F-5E Tiger II, AN/APQ-167 radar tested, intended to replace AN/APQ-157, but not carried out.
F-5F Tiger III Upgraded trainer version of the F-5F in use by the Chilean Air Force.
F-5T Upgraded F-5F in use by the Republic of Singapore Air Force.
F-5THF Twin-seat version of F-5TH in active services with the Royal Thai Air Force as of May 2020.
F-5FM Upgraded trainer version of the F-5F for the Brazilian Air Force.
System
Alternate Designation(s) F-5E Tiger II
Type Supersonic Light Fighter Aircraft
Manufacturer Northrop Corporation
Crew 1 ea
Number of Engines 2 ea
Number of Hard Points 7 total (only pylon stations 3, 4 and 5 are wet-plumbed): 2× wing-tip AAM launch rails, 4× under-wing & 1× under-fuselage pylon stations with a capacity of 3,200 kg.
Dimensions
Length 14.45 m
Width (Wing Span) 8.13 m
Wing Area 17.30 m sq
Height 4.06 m
Empty Weight 4,410 kg
Maximum Weapons Load 3,175 kg
Maximum Takeoff Weight 11,214 kg
Automotive
Engine Name 2 x General Electric J85-GE-21B
Engine Type Turbojet
Engine Power, Dry INA
Engine Power, Afterburner 2,268 kg static thrust each
Fuel Capacity 2,555 liters
Maximum Speed 1,733 km/h
Cruise Speed 904 km/h
Stall Speed 230 km/h
Climb Rate 10,516 m/min
Ceiling 15,789 m
Ferry Range 2,861 km
Radius at Altitude 1,056 km at 4,575 m, max fuel, 2 AAM, combat reserves
Main Gun System
System
Name 1 x M39 Autocannon
Type Single-Barrel Autocannon
Caliber 20 mm
Length 1.83 m
Weight 80.9 kg
Barrels Single barrel (progressive RH parabolic twist, 9 grooves)
Action Five-chamber revolver
Rate of Fire 1,500 rpm
Muzzle Velocity 1,030 m/s
Ammunition
Type Rifle
Caliber 20 mm
Cartridge 20×102 mm
Basic Load 280 Rounds
Main Missile Systems
Option 1 2× AIM-9 Sidewinder air-to-air missile on wingtips (initial F-5E Tiger II loadout)
Option 2 4× AIM-9 Sidewinder or 4× AIM-120 AMRAAM air-to-air missile (F-5S and modernized F-5E)
Option 3 4× AGM-65 Maverick air-to-surface missiles (on upgraded F-5 after 1995)
Option 4 AA-8 Aphid, AA-10 Alamo, AA-11 Archer and other Russian/Chinese AAMs (Iranian ver.)
Rocket Weapon Systems
Option 1 2× LAU-61/LAU-68 rocket pods (each with 19× /7× Hydra 70 mm rockets, respectively)
Option 2 2× LAU-5003 rocket pods (each with 19× CRV7 70 mm rockets)
Option 3 2× LAU-10 rocket pods (each with 4× Zuni 127 mm rockets)
Option 4 2× Matra rocket pods (each with 18× SNEB 68 mm rockets)
Bomb Weapon Systems
Note 9 x 227-kg bombs.
Fire Control / Avionics
Fire Control Radar AN/APQ-159 Radar
Navigation Radar INA
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor INA
NBC Protection INA
EW Counter Measures INA
Chaffs/Flares INA
Details
Country of Origin United States
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
F
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
14.45 m
Width
8.13 m
Height
4.06 m
Weight
11214 kg
Operators (17)
South Korea
Turkey
Iran
Brazil
Spain
Bahrain
Chile
Honduras
Indonesia
Kenya
Malaysia
Mexico
Morocco
Switzerland
Thailand
Tunisia
Yemen
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