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F-16 Fighting Falcon vs Su-27 Flanker

F-16 Fighting Falcon vs Su-27 Flanker at a glance — top speed 2,178 vs 2,500 km/h, range 4,217 vs 3,530 km, max takeoff weight 19,200 vs 30,000 kg, built 4,604 vs 680 units.

Specifications
F-16 Fighting Falcon Su-27 Flanker
Origin country 🇺🇸 United States 🇷🇺 Ex-USSR
Category Combat Aircraft Combat Aircraft
Manufacturer General Dynamics Sukhoi
First flight 2 February 1974 20 May 1977
Year introduced 1979 1985
Number produced 4604 units 680 units
Average unit price $18.8 million $30 million
Wing area 27.9 m² 62.0 m²
Wingspan 10.0 m 14.7 m
Height 4.9 m 5.9 m
Length 15.1 m 21.9 m
Maximum speed 2178 km/h 2500 km/h
Operational range 4,217 km 3,530 km
Service ceiling 15,240 m 18,500 m
Max. takeoff weight 19,200 kg 30,000 kg
Empty weight 8,570 kg 16,300 kg
Total thrust 1 x 12,701 kgf 2 x 12,502 kgf
Performance Radar Chart

Detailed Comparison

The General Dynamics F-16 and Sukhoi Su-27 were engineered for opposite ends of the air combat spectrum. The United States optimized the F-16 as a lightweight, single-engine multirole platform intended for high-volume production, yielding over 4,600 units at $75 million per airframe. The Soviet Union designed the Su-27 as a heavy, twin-engine, long-range interceptor to counter the American F-15, producing roughly 680 baseline airframes before shifting to heavier multirole derivatives.

Development and Design

The F-16 emerged from the USAF Lightweight Fighter Program as a financially sustainable alternative to heavy air superiority platforms. Its design relied on relaxed static stability managed by an analog—later digital—fly-by-wire system, a side-mounted control stick, and a frameless canopy to maximize pilot visibility under high G-loading. Sukhoi’s T-10 prototype, which evolved into the Su-27, responded to the Soviet requirement to patrol vast, radar-poor borders. This dictated a blended wing-body airframe with large internal fuel volume, eliminating the aerodynamic drag of external drop tanks. Sukhoi integrated large leading-edge root extensions (LERX) to maintain high angle-of-attack handling for an aircraft weighing up to 30,000 kg.

Specifications and Performances

The performance metrics outline a strict division in doctrine. The F-16 is constrained by a 19,200 kg maximum takeoff weight and a single GE F110 engine. This restricts its unrefueled combat radius to roughly 550 km depending on external stores. In contrast, the Su-27 reaches a maximum takeoff weight of 30,000 kg, pushed by two AL-31F turbofans generating 15,340 kgf of dry thrust. This yields a 3,530 km unrefueled range. The Flanker has the kinematic advantage with a Mach 2.35 top speed compared to the F-16's Mach 2.0, but the American jet's smaller radar cross-section and tighter avionics integration historically gave it an edge in situational awareness.

Deployment and usage

In combat, the airframes fulfill entirely different mission profiles based on their technical constraints:

  • The F-16 transitioned from a daytime dogfighter into a primary strike and SEAD platform. Israeli F-16s dismantled Syrian air defenses in the Bekaa Valley in 1982, while USAF units executed thousands of ground-attack sorties during Operation Desert Storm.
  • The baseline Su-27 saw targeted air-to-air use, most pointedly during the 1999–2000 Eritrean-Ethiopian War where Ethiopian Flankers shot down multiple Eritrean MiG-29s. More recently, Ukrainian Su-27s have operated defensively against Russian forces, suffering high attrition against R-37M-equipped Su-35s.

Conclusion

The F-16 holds the definitive edge in multirole strike, SEAD, and network-centric operations. Its open-architecture upgrades, vast munition compatibility, and global supply chain make it the logical choice for air forces requiring high-sortie-rate combat mass near contested borders. The Su-27 holds the advantage in raw kinematic interception and area defense over vast geographies. For an air force operating with robust tanker support, the F-16 provides a higher return on investment. For nations needing to patrol deep airspace or project power without aerial refueling, the heavy Flanker airframe remains the necessary solution.

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Frequently Asked Questions

Which is faster, the F-16 Fighting Falcon or Su-27 Flanker?
The Su-27 Flanker is faster with a maximum speed of 2,500 km/h compared to the F-16 Fighting Falcon's 2,178 km/h, a difference of 322 km/h.
Which has longer range, the F-16 Fighting Falcon or Su-27 Flanker?
The F-16 Fighting Falcon has a longer range at 4,217 km compared to the Su-27 Flanker's 3,530 km.
Which can fly higher, the F-16 Fighting Falcon or Su-27 Flanker?
The Su-27 Flanker has a higher service ceiling at 18,500 meters (60,695 ft) compared to the F-16 Fighting Falcon's 15,240 meters (50,000 ft).
Which is heavier, the F-16 Fighting Falcon or Su-27 Flanker?
The Su-27 Flanker has a higher maximum takeoff weight at 30,000 kg compared to the F-16 Fighting Falcon's 19,200 kg.
Which is larger, the F-16 Fighting Falcon or Su-27 Flanker?
The Su-27 Flanker is longer at 21.9 meters compared to the F-16 Fighting Falcon's 15.1 meters.
Which is more expensive, the F-16 Fighting Falcon or Su-27 Flanker?
The Su-27 Flanker is more expensive at approximately $30 million per unit compared to the F-16 Fighting Falcon at $19 million.
Which entered service first, the F-16 Fighting Falcon or Su-27 Flanker?
The F-16 Fighting Falcon entered service first in 1979, 6 years before the Su-27 Flanker which entered service in 1985.
Which has been built in greater numbers, the F-16 Fighting Falcon or Su-27 Flanker?
The F-16 Fighting Falcon has been produced in greater numbers with 4,604 units compared to 680 units of the Su-27 Flanker.