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F-5E Tiger II vs MiG-21 Fishbed

F-5E Tiger II vs MiG-21 Fishbed at a glance — top speed 1,700 vs 2,125 km/h, range 3,723 vs 660 km, max takeoff weight 11,187 vs 8,625 kg, built 1,399 vs 11,496 units.

Northrop F-5E Tiger II combat aircraft side profile drawing
🇺🇸 F-5E Tiger II
Mikoyan-Gurevich MiG-21 Fishbed combat aircraft side profile drawing
Specifications
F-5E Tiger II MiG-21 Fishbed
Origin country 🇺🇸 United States 🇷🇺 Ex-USSR
Category Combat Aircraft Combat Aircraft
Manufacturer Northrop Mikoyan-Gurevich
First flight 11 August 1972 16 June 1955
Year introduced 1976 1958
Number produced 1399 units 11496 units
Average unit price $2.1 million $2 million
Wing area 17.3 m² 23.0 m²
Wingspan 8.1 m 7.2 m
Height 4.1 m 4.1 m
Length 14.5 m 13.5 m
Maximum speed 1700 km/h 2125 km/h
Operational range 3,723 km 660 km
Service ceiling 15,789 m 19,000 m
Max. takeoff weight 11,187 kg 8,625 kg
Empty weight 4,349 kg 4,871 kg
Total thrust 2 x 3,176 kgf 1 x 4,689 kgf
Performance Radar Chart

Detailed Comparison

The Northrop F-5E Tiger II and the Mikoyan-Gurevich MiG-21 Fishbed stand as the preeminent lightweight export fighters of the Cold War. While both prioritized low acquisition costs and ease of maintenance to equip allied nations, they diverged significantly in aerodynamic philosophy and intended tactical application. The F-5E focused on agility and multi-role versatility for U.S. partners, whereas the MiG-21 was designed as a high-speed interceptor to counter Western strike aircraft.

Development and Design

Northrop developed the F-5E as an evolution of the Freedom Fighter, incorporating more powerful J85-GE-21 engines and improved aerodynamics to create an affordable, modular platform. Its design emphasized modular construction, allowing nations with limited infrastructure to swap components easily. Conversely, the MiG-21 emerged from a requirement to intercept supersonic Western bombers. Its defining feature is the tailed delta wing configuration, optimized for high-speed dashes. While the F-5E utilized a twin-engine layout for survivability and sustained turn performance, the MiG-21 relied on a single, powerful Tumansky turbojet within a minimum-drag fuselage, accepting compromises in range and cockpit visibility to achieve raw speed.

Specifications and Performances

The performance metrics illustrate the doctrinal split: the MiG-21 possesses superior kinematic performance in the vertical plane, while the F-5E excels in horizontal maneuvering. The MiG-21 achieves a maximum speed of 2125 km/h and a service ceiling of 19,000 m, significantly outclassing the F-5E’s 1700 km/h and 15,789 m ceiling. However, the Soviet design suffers from limited endurance, with a range of only 660 km compared to the F-5E's 891 km. The F-5E’s wing design and twin-engine configuration provide better handling at subsonic speeds, whereas the MiG-21’s delta wing bleeds energy rapidly during hard turns, making it difficult to handle during takeoff, landing, and sustained dogfights.

Deployment and usage

Both aircraft saw extensive export success, with the MiG-21 serving over 60 nations and the F-5E over 30. In the Vietnam War, the MiG-21 proved effective using "hit-and-run" interceptor tactics against American strike packages. The F-5E, arriving later, served the South Vietnamese Air Force and later became a staple of the Iran-Iraq War, where it clashed directly with MiG-21s. A testament to the F-5E’s maneuverability is its long-standing use by U.S. Air Force "Aggressor" squadrons to simulate the size and performance of Soviet fighters like the MiG-21 in dissimilar air combat training. The MiG-21 remains in service through heavy modernization programs like the Indian "Bison," while the F-5E continues to serve via upgrades like the Brazilian F-5EM, leveraging its 7,000-pound ordnance capacity for ground attack roles.

Conclusion

The MiG-21 was a superior interceptor, built to scramble, climb fast, and engage bombers. The F-5E was a more balanced, pilot-friendly fighter-bomber. While the MiG-21 holds the advantage in raw speed and production numbers (over 11,000 units), the F-5E offered superior avionics integration, maintainability, and sustained dogfighting capability. In modern asymmetrical warfare, the F-5E's versatile air-to-ground platform often proves more utilitarian than the MiG-21's dedicated interceptor profile, though highly upgraded variants of both airframes continue to defy their age in active service.

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Frequently Asked Questions

Which is faster, the F-5E Tiger II or MiG-21 Fishbed?
The MiG-21 Fishbed is faster with a maximum speed of 2,125 km/h compared to the F-5E Tiger II's 1,700 km/h, a difference of 425 km/h.
Which has longer range, the F-5E Tiger II or MiG-21 Fishbed?
The F-5E Tiger II has a longer range at 3,723 km compared to the MiG-21 Fishbed's 660 km.
Which can fly higher, the F-5E Tiger II or MiG-21 Fishbed?
The MiG-21 Fishbed has a higher service ceiling at 19,000 meters (62,335 ft) compared to the F-5E Tiger II's 15,789 meters (51,801 ft).
Which is heavier, the F-5E Tiger II or MiG-21 Fishbed?
The F-5E Tiger II has a higher maximum takeoff weight at 11,187 kg compared to the MiG-21 Fishbed's 8,625 kg.
Which is larger, the F-5E Tiger II or MiG-21 Fishbed?
The F-5E Tiger II is longer at 14.4 meters compared to the MiG-21 Fishbed's 13.5 meters.
Which is more expensive, the F-5E Tiger II or MiG-21 Fishbed?
The F-5E Tiger II is more expensive at approximately $2.1 million per unit compared to the MiG-21 Fishbed at $2.0 million.
Which entered service first, the F-5E Tiger II or MiG-21 Fishbed?
The MiG-21 Fishbed entered service first in 1958, 18 years before the F-5E Tiger II which entered service in 1976.
Which has been built in greater numbers, the F-5E Tiger II or MiG-21 Fishbed?
The MiG-21 Fishbed has been produced in greater numbers with 11,496 units compared to 1,399 units of the F-5E Tiger II.