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An-124 Condor vs C-130 Hercules

An-124 Condor vs C-130 Hercules at a glance — top speed 865 vs 593 km/h, range 3,700 vs 3,800 km, max takeoff weight 405,000 vs 70,307 kg, built 55 vs 2,500 units.

Antonov An-124 Condor military transport aircraft side profile drawing
🇷🇺 An-124 Condor
Lockheed C-130 Hercules military transport aircraft side profile drawing
Specifications
An-124 Condor C-130 Hercules
Origin country 🇷🇺 Ex-USSR 🇺🇸 United States
Category Military Transport Aircraft Military Transport Aircraft
Manufacturer Antonov Lockheed
First flight 26 December 1982 23 August 1954
Year introduced 1986 1956
Number produced 55 units 2500 units
Average unit price $100 million $68 million
Wing area 628.0 m² 162.0 m²
Wingspan 73.3 m 40.4 m
Height 20.8 m 11.7 m
Length 69.0 m 29.8 m
Maximum speed 865 km/h 593 km/h
Operational range 3,700 km 3,800 km
Service ceiling 9,000 m 10,058 m
Max. takeoff weight 405,000 kg 70,307 kg
Empty weight 175,000 kg 35,800 kg
Total thrust 4 x 23,400 kgf 4 x 3,661 kW
Performance Radar Chart

Detailed Comparison

The Antonov An-124 Condor is a strategic airlifter designed for outsized, super-heavy cargo, while the Lockheed C-130 Hercules is a tactical transport optimized for versatility and austere field operations. The An-124 was developed by the Soviet Union to provide airlift capacity comparable to the American C-5 Galaxy, resulting in a jet-powered aircraft for intercontinental transport of uniquely heavy assets. In contrast, the C-130 was born from a US requirement for a turboprop-powered transport to move troops and supplies to forward operating locations.

Development and Design

The An-124’s design philosophy prioritized maximum payload capacity. Its double-fuselage structure incorporates a "kneeling" landing gear system with 24 wheels, a visor-type upward-hinging nose, and a rear cargo ramp, allowing for simultaneous loading and unloading. This contrasts with the C-130’s simpler, more rugged design, which features a high-wing configuration, four turboprop engines, and a single rear-loading ramp. The C-130's design is not for outsized cargo but for operational flexibility, enabling it to use short, unprepared airstrips inaccessible to a jet airlifter of the An-124's scale. While the An-124 incorporated advanced materials like titanium and composites, the C-130’s success lies in its conventional, robust, and easily maintainable aluminum airframe, which has allowed for continuous production and evolution for over 60 years.

Specifications and Performances

The performance metrics of these aircraft reflect their distinct roles. The An-124 has a maximum takeoff weight of 405,000 kg and can carry a payload of up to 150 tonnes, enabling it to transport multiple main battle tanks or massive industrial components. Its four turbofan engines give it a high cruise speed of 865 km/h and a long ferry range. The C-130 is far smaller, with a maximum takeoff weight of 70,307 kg and a typical payload of around 20 tonnes. Its key performance advantage is its short takeoff and landing (STOL) capability, requiring only 1,093 meters of runway, less than half that of the An-124. This, combined with its turboprop engines, makes the C-130 ideal for tactical airlift directly into contested or underdeveloped areas.

Deployment and usage

The An-124's small production run (55 units) has confined its use to a highly specialized niche. Militarily, it has been used by NATO under the SALIS program for strategic lift to theaters like Afghanistan. Commercially, it is a key asset for moving indivisible cargo such as satellites, turbines, and aerospace components. The C-130, with over 2,500 units built, is a ubiquitous tactical workhorse for dozens of air forces. Beyond transport, its airframe has been adapted into numerous special-mission platforms, including:

  • AC-130 gunships for close air support.
  • MC-130 for special operations infiltration/exfiltration.
  • KC-130 tankers for tactical aerial refueling.
  • EC-130 for electronic warfare.

Conclusion

The An-124 and C-130 are not direct competitors; they represent solutions to fundamentally different logistical problems. The An-124 is a high-value, low-density strategic asset, essential for moving cargo that no other aircraft can. Its limited availability and reliance on long, paved runways define its role. The C-130 is the backbone of tactical airlift, providing unparalleled versatility and access to forward locations. Its value comes not from carrying the largest loads, but from its adaptability, reliability, and sheer numbers, which have made it an indispensable tool for military operations worldwide for decades.

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Frequently Asked Questions

Which is faster, the An-124 Condor or C-130 Hercules?
The An-124 Condor is faster with a maximum speed of 865 km/h compared to the C-130 Hercules's 593 km/h, a difference of 272 km/h.
Which has longer range, the An-124 Condor or C-130 Hercules?
The C-130 Hercules has a longer range at 3,800 km compared to the An-124 Condor's 3,700 km.
Which can fly higher, the An-124 Condor or C-130 Hercules?
The C-130 Hercules has a higher service ceiling at 10,058 meters (32,998 ft) compared to the An-124 Condor's 9,000 meters (29,527 ft).
Which is heavier, the An-124 Condor or C-130 Hercules?
The An-124 Condor has a higher maximum takeoff weight at 405,000 kg compared to the C-130 Hercules's 70,307 kg.
Which is larger, the An-124 Condor or C-130 Hercules?
The An-124 Condor is longer at 69.0 meters compared to the C-130 Hercules's 29.8 meters.
Which is more expensive, the An-124 Condor or C-130 Hercules?
The An-124 Condor is more expensive at approximately $100 million per unit compared to the C-130 Hercules at $68 million.
Which entered service first, the An-124 Condor or C-130 Hercules?
The C-130 Hercules entered service first in 1956, 30 years before the An-124 Condor which entered service in 1986.
Which has been built in greater numbers, the An-124 Condor or C-130 Hercules?
The C-130 Hercules has been produced in greater numbers with 2,500 units compared to 55 units of the An-124 Condor.