F5e Tiger Ii Fighter Jet Specifications And History

The F5E Tiger II is a single-seat, twin-engine supersonic fighter jet that was designed and built by Northrop Corporation in the 1970s. The aircraft is an upgraded version of the F-5A Freedom Fighter, which was originally designed in the 1950s. The F5E Tiger II was developed to meet the needs of the United States Air Force (USAF) and other allied countries for a low-cost, high-performance fighter jet.

Design and Development

The F5E Tiger II was designed to be a more advanced version of the F-5A Freedom Fighter, with improved performance and capabilities. The aircraft features a new wing design, which provides better maneuverability and control at high speeds. The F5E also has a more powerful engine, the General Electric J85-GE-21, which produces 5,000 pounds of thrust.

The F5E Tiger II has a length of 47 feet 3 inches (14.4 meters) and a wingspan of 26 feet 8 inches (8.1 meters). The aircraft has an empty weight of 9,158 pounds (4,153 kilograms) and a maximum takeoff weight of 20,480 pounds (9,292 kilograms). The F5E has a top speed of Mach 1.6 (over 1,000 mph) and a range of over 500 miles (800 kilometers).

Key Features

Single-seat, twin-engine supersonic fighter jet
New wing design for improved maneuverability and control
More powerful engine, General Electric J85-GE-21, producing 5,000 pounds of thrust
Length: 47 feet 3 inches (14.4 meters)
Wingspan: 26 feet 8 inches (8.1 meters)
Empty weight: 9,158 pounds (4,153 kilograms)
Maximum takeoff weight: 20,480 pounds (9,292 kilograms)
Top speed: Mach 1.6 (over 1,000 mph)
Range: over 500 miles (800 kilometers)

Operational History

The F5E Tiger II was first introduced in 1972 and was used by the United States Air Force (USAF) as a training aircraft. The aircraft was also exported to several other countries, including Brazil, Chile, Indonesia, and the Philippines.

The F5E Tiger II saw combat in several conflicts, including the Vietnam War and the Iran-Iraq War. The aircraft was also used by the USAF as a aggressor aircraft, simulating the tactics and techniques of enemy fighter jets.

Users

United States Air Force (USAF)
Brazil
Chile
Indonesia
Philippines
Other countries

Specifications

Crew: 1
Length: 47 feet 3 inches (14.4 meters)
Wingspan: 26 feet 8 inches (8.1 meters)
Height: 13 feet 4 inches (4.1 meters)
Empty weight: 9,158 pounds (4,153 kilograms)
Maximum takeoff weight: 20,480 pounds (9,292 kilograms)
Powerplant: 2 x General Electric J85-GE-21 turbojet engines
Thrust: 5,000 pounds (2,268 kilograms) each
Maximum speed: Mach 1.6 (over 1,000 mph)
Range: over 500 miles (800 kilometers)
Service ceiling: 40,000 feet (12,192 meters)

Ammunition and Armament

2 x M39 20mm cannon
4 x AIM-9 Sidewinder missiles
2 x AIM-7 Sparrow missiles
4 x Mk 82 500-pound bombs
2 x Mk 84 2,000-pound bombs

Conclusion

The F5E Tiger II is a highly advanced and capable fighter jet that was designed and built by Northrop Corporation in the 1970s. The aircraft features a new wing design, more powerful engine, and improved performance and capabilities. The F5E Tiger II saw combat in several conflicts and was used by the United States Air Force (USAF) and other countries as a training and aggressor aircraft.