Northrop F-5E Tiger II

Explore the Northrop F-5E Tiger II in side view and top view to compare its silhouette and proportions.

Northrop F-5E Tiger II, side profile
Northrop F-5E Tiger II, side profile
14.69 m
Northrop F-5E Tiger II, top view
Northrop F-5E Tiger II, top view
8.13 m

From Wikipedia

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 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 costs 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 US allies. Despite the United States Air Force (USAF) not needing a light fighter at the time, it did procure approximately 1,200 Northrop T-38 Talon trainer aircraft, which were based on Northrop's N-156 fighter design.

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Summary of “Northrop F-5” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.

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Drawing of the Northrop F-5E Tiger II by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/F5/), CC BY 4.0

Specifications

Length
14.69 m
Wingspan
8.13 m
Max take-off weight
11.19 t
Cruise speed
850 km/h
Max speed
1,739 km/h
Range
891 km
Ceiling
15,789 m
Engines
2 × General Electric J85-GE-21 afterburning turbojet engines
Power
3,500 lbf (16 kN) thrust each dry, 5,000 lbf (22 kN) with afterburner
First flight
1972

From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.