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A-10 Thunderbolt II vs Su-25 Frogfoot

A-10 Thunderbolt II vs Su-25 Frogfoot at a glance — top speed 675 vs 970 km/h, range 4,150 vs 1,000 km, max takeoff weight 22,680 vs 17,600 kg, built 716 vs 1,000 units.

Specifications
A-10 Thunderbolt II Su-25 Frogfoot
Origin country 🇺🇸 United States 🇷🇺 Ex-USSR
Category Combat Aircraft Combat Aircraft
Manufacturer Fairchild Republic Sukhoi
First flight 10 May 1972 22 February 1975
Year introduced 1975 1981
Number produced 716 units 1000 units
Average unit price $20 million $11 million
Wing area 47.0 m² 30.1 m²
Wingspan 17.5 m 14.4 m
Height 4.5 m 4.8 m
Length 16.3 m 15.5 m
Maximum speed 675 km/h 970 km/h
Operational range 4,150 km 1,000 km
Service ceiling 13,716 m 7,000 m
Max. takeoff weight 22,680 kg 17,600 kg
Empty weight 11,321 kg 9,500 kg
Total thrust 2 x 8,224 kgf 2 x 4,505 kgf
Performance Radar Chart

Detailed Comparison

Born from the Cold War need for a dedicated close air support (CAS) aircraft, the American A-10 Thunderbolt II and Soviet Su-25 Frogfoot are defined by their shared mission but diverge in critical design aspects. The A-10 was built around its formidable GAU-8 Avenger 30mm cannon, prioritizing firepower and pilot survivability through features like a titanium "bathtub" cockpit. In contrast, the Su-25 emphasized operational simplicity and ruggedness for deployment from austere forward bases, equipped with a GSh-30-2 30mm cannon.

Development and Design

The A-10's design originated from the U.S. Air Force's A-X program, a direct response to shortcomings in CAS capabilities observed during the Vietnam War. The chief designer prioritized a durable, straightforward airframe capable of sustaining significant damage, incorporating redundant systems and high-bypass turbofan engines for long loiter times. The Su-25 followed a parallel Soviet design philosophy, aiming to provide robust support for ground forces. Its development focused on ruggedness, with a simpler airframe, basic turbojet engines, and a welded steel armored cockpit, all intended to facilitate operations from unprepared airstrips with minimal support. Both aircraft feature a straight-wing design to optimize low-speed, low-altitude maneuverability.

Specifications and Performances

The A-10 is a considerably larger and heavier aircraft, with a maximum takeoff weight of 22,680 kg versus the Su-25's 17,600 kg. This allows the A-10 to carry a much larger external ordnance load of up to 7,257 kg on its 11 hardpoints. While the Su-25 is faster (max speed 970 km/h vs. 706 km/h for the A-10), the A-10's lower speed is a deliberate choice for its role, enhancing target acquisition and engagement time. The A-10’s GAU-8 cannon is its defining weapon, possessing a higher rate of fire (3,900 rpm) and a larger ammunition drum than the Su-25's GSh-30-2. Furthermore, the A-10's much higher service ceiling (13,716 m vs. 7,000 m) provides greater operational flexibility.

Deployment and usage

The A-10 proved its value during Operation Desert Storm in 1991, destroying vast numbers of Iraqi armored vehicles. It has since served extensively in the Balkans, Afghanistan, and Iraq. The introduction of the A-10C variant, with its digital avionics and ability to deploy precision-guided munitions, has ensured its continued effectiveness in modern conflicts. The Su-25's combat debut was in the Soviet-Afghan War, and it has since become a fixture in numerous conflicts, including in Chechnya, Georgia, Syria, and most notably by both sides in the 2022 Russian invasion of Ukraine. Its widespread use highlights its robust design, but has also exposed its vulnerabilities in high-threat environments saturated with modern air defenses.

Conclusion

Both aircraft successfully demonstrated the military value of a purpose-built, heavily armored ground-attack platform. The A-10's design philosophy, centered on pilot survivability and overwhelming cannon-based firepower, has made it an unparalleled CAS asset, particularly when operating under conditions of air superiority. The Su-25's emphasis on ruggedness and operational simplicity led to a prolific and cost-effective aircraft used by numerous air forces, often in high-intensity conflicts. While both platforms face increasing challenges from sophisticated air defense systems, their specialized capabilities ensure they remain operationally relevant.

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Frequently Asked Questions

Which is faster, the A-10 Thunderbolt II or Su-25 Frogfoot?
The Su-25 Frogfoot is faster with a maximum speed of 970 km/h compared to the A-10 Thunderbolt II's 675 km/h, a difference of 295 km/h.
Which has longer range, the A-10 Thunderbolt II or Su-25 Frogfoot?
The A-10 Thunderbolt II has a longer range at 4,150 km compared to the Su-25 Frogfoot's 1,000 km.
Which can fly higher, the A-10 Thunderbolt II or Su-25 Frogfoot?
The A-10 Thunderbolt II has a higher service ceiling at 13,716 meters (45,000 ft) compared to the Su-25 Frogfoot's 7,000 meters (22,965 ft).
Which is heavier, the A-10 Thunderbolt II or Su-25 Frogfoot?
The A-10 Thunderbolt II has a higher maximum takeoff weight at 22,680 kg compared to the Su-25 Frogfoot's 17,600 kg.
Which is larger, the A-10 Thunderbolt II or Su-25 Frogfoot?
The A-10 Thunderbolt II is longer at 16.3 meters compared to the Su-25 Frogfoot's 15.5 meters.
Which is more expensive, the A-10 Thunderbolt II or Su-25 Frogfoot?
The A-10 Thunderbolt II is more expensive at approximately $20 million per unit compared to the Su-25 Frogfoot at $11 million.
Which entered service first, the A-10 Thunderbolt II or Su-25 Frogfoot?
The A-10 Thunderbolt II entered service first in 1975, 6 years before the Su-25 Frogfoot which entered service in 1981.
Which has been built in greater numbers, the A-10 Thunderbolt II or Su-25 Frogfoot?
The Su-25 Frogfoot has been produced in greater numbers with 1,000 units compared to 716 units of the A-10 Thunderbolt II.