GlobalMilitary.net Open-source military intelligence Updated daily

F-5E Tiger II vs J-7 Fishcan

F-5E Tiger II vs J-7 Fishcan at a glance — top speed 1,700 vs 2,200 km/h, range 3,723 vs 2,200 km, max takeoff weight 11,187 vs 9,100 kg, built 1,399 vs 2,400 units.

Northrop F-5E Tiger II combat aircraft side profile drawing
🇺🇸 F-5E Tiger II
Chengdu J-7 Fishcan combat aircraft side profile drawing
🇨🇳 J-7 Fishcan
Specifications
F-5E Tiger II J-7 Fishcan
Origin country 🇺🇸 United States 🇨🇳 China
Category Combat Aircraft Combat Aircraft
Manufacturer Northrop Chengdu
First flight 11 August 1972 17 January 1966
Year introduced 1976 1966
Number produced 1399 units 2400 units
Average unit price $2.1 million $2 million
Wing area 17.3 m² 24.9 m²
Wingspan 8.1 m 8.3 m
Height 4.1 m 4.1 m
Length 14.5 m 14.0 m
Maximum speed 1700 km/h 2200 km/h
Operational range 3,723 km 2,200 km
Service ceiling 15,789 m 17,500 m
Max. takeoff weight 11,187 kg 9,100 kg
Empty weight 4,349 kg 5,292 kg
Total thrust 2 x 3,176 kgf 1 x 6,598 kgf
Performance Radar Chart

Detailed Comparison

The Northrop F-5E Tiger II and the Chengdu J-7 Fishcan emerged as two of the most widely exported light fighters of the Cold War, catering to nations requiring cost-effective air defense. While the F-5E was designed specifically as a highly agile, multi-role platform for U.S. allies, the J-7 is a Chinese license-produced derivative of the Soviet MiG-21, emphasizing speed and interception over versatility. Both achieved massive production numbers—approximately 1,400 for the Tiger II and 2,400 for the Fishcan—competing directly in the global arms market for budget-conscious air forces.

Development and Design

The F-5E Tiger II, evolved from the Freedom Fighter, prioritized operational simplicity and modular maintenance. Its twin-engine configuration using General Electric J85s provided reliability and redundancy, while the aerodynamic design focused on subsonic and transonic agility. Uniquely, its modular construction allowed for component swapping, drastically reducing logistical footprints. Conversely, the J-7 adheres strictly to the Soviet interception doctrine. It utilizes a single-engine, tailed delta-wing configuration with a nose air intake, optimized for high-altitude, high-speed dashes. While the F-5E integrated functional radar capabilities for its class early on, early J-7 variants suffered from cramped cockpits and primitive avionics, necessitating extensive upgrades—such as the double-delta wing J-7E—to remain relevant in modern environments.

Specifications and Performances

The aerodynamic differences dictate distinct performance profiles. The J-7 possesses superior kinematic performance in the vertical regime, with a service ceiling of 17,500 m and a climb rate of 195 m/s, compared to the F-5E’s 15,789 m and 175 m/s. The J-7 also achieves a significantly higher maximum speed of 2,200 km/h (Mach 2+), eclipsing the F-5E's 1,700 km/h.

However, the F-5E offers superior utility as a weapons platform. With a Maximum Takeoff Weight of 11,187 kg, it supports a heavier payload (up to 7,000 lbs) compared to the J-7's 9,100 kg limit. The F-5E's twin 20mm M39A2 cannons and compatibility with precision munitions like the AGM-65 Maverick contrast sharply with the J-7's reliance on a single 30mm cannon and unguided rockets. Furthermore, the F-5E's wingtip rails for AIM-9 Sidewinders allow for rapid engagement, whereas the J-7's hardpoints are more limited.

Deployment and Usage

Northrop designed the F-5E to fit into diverse logistical ecosystems, leading to its adoption by over 30 nations. It saw combat in the Iran-Iraq War and Vietnam, but notably found a niche as an "Aggressor" aircraft for the USAF due to its visual and performance similarity to the MiG-21. The J-7 served primarily as the PLAAF’s backbone for decades, tasked with territorial defense. While widely exported to nations like Pakistan (as the F-7), its combat record is less distinguished than the Soviet MiG-21 it was based on. The J-7 remains a point-defense interceptor, whereas the F-5E functions effectively in ground attack and multi-role sorties.

Conclusion

Ultimately, the F-5E Tiger II represents a more balanced, pilot-friendly platform capable of sustained multi-role operations, justified by its higher unit cost of $3.0 million. The J-7 Fishcan, at $2.0 million, offers raw speed and high-altitude capability but is operationally limited by its short range, small payload, and older avionics architecture. While the J-7 relies on raw kinematic power for interception, the F-5E relies on versatility and sustainment, making it the superior tactical asset for air forces requiring more than simple airspace denial.

Change comparison vs

Frequently Asked Questions

Which is faster, the F-5E Tiger II or J-7 Fishcan?
The J-7 Fishcan is faster with a maximum speed of 2,200 km/h compared to the F-5E Tiger II's 1,700 km/h, a difference of 500 km/h.
Which has longer range, the F-5E Tiger II or J-7 Fishcan?
The F-5E Tiger II has a longer range at 3,723 km compared to the J-7 Fishcan's 2,200 km.
Which can fly higher, the F-5E Tiger II or J-7 Fishcan?
The J-7 Fishcan has a higher service ceiling at 17,500 meters (57,414 ft) compared to the F-5E Tiger II's 15,789 meters (51,801 ft).
Which is heavier, the F-5E Tiger II or J-7 Fishcan?
The F-5E Tiger II has a higher maximum takeoff weight at 11,187 kg compared to the J-7 Fishcan's 9,100 kg.
Which is larger, the F-5E Tiger II or J-7 Fishcan?
The F-5E Tiger II is longer at 14.4 meters compared to the J-7 Fishcan's 13.9 meters.
Which is more expensive, the F-5E Tiger II or J-7 Fishcan?
The F-5E Tiger II is more expensive at approximately $2.1 million per unit compared to the J-7 Fishcan at $2.0 million.
Which entered service first, the F-5E Tiger II or J-7 Fishcan?
The J-7 Fishcan entered service first in 1966, 10 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 J-7 Fishcan?
The J-7 Fishcan has been produced in greater numbers with 2,400 units compared to 1,399 units of the F-5E Tiger II.