An-124 Condor vs C-141 Starlifter
Overview
The An-124 Condor and the C-141 Starlifter are both Military Transport Aircraft, manufactured by Antonov and Lockheed respectively.
Top speed is 865 km/h for the An-124 Condor vs 805 km/h for the C-141 Starlifter. The An-124 Condor has an operational range of 3,700 km vs 4,723 km for the C-141 Starlifter. The C-141 Starlifter operates at altitudes up to 12,497 m compared to 9,000 m for the An-124 Condor. At 405,000 kg MTOW, the An-124 Condor is 2.8x the C-141 Starlifter's 146,556 kg.
The An-124 Condor has been produced in 55 units vs 285 for the C-141 Starlifter. Unit cost is $100M for the An-124 Condor vs $40M for the C-141 Starlifter. The C-141 Starlifter first flew 19 years before the An-124 Condor (1963 vs 1982).
| Soviet heavy transport aircraft, employed globally in strategic airlift operations during the Cold War era. | |
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| Origin country | π¨π³ Ex-USSR |
| Category | Military Transport Aircraft |
| Manufacturer | Antonov |
| First flight | 26 December 1982 |
| Year introduced | 1986 |
| Number produced | 55 units |
| Average unit price | $100 million |
| American military transport aircraft, pivotal during the Vietnam War, chiefly used for strategic airlift missions. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Lockheed |
| First flight | 17 December 1963 |
| Year introduced | 1965 |
| Number produced | 285 units |
| Average unit price | $40 million |
| Wing area | 628.0 mΒ² β |
| Wingspan | 73.3 m β |
| Height | 20.8 m β |
| Length | 69.0 m β |
| Maximum speed | 865 km/h β |
| Operational range | 3,700 km β |
| Service ceiling | 9,000 m β |
| Max. takeoff weight | 405,000 kg β |
| Empty weight | 175,000 kg β |
| Total thrust | 4 x 5,850 kgf β |
| Wing area | 300.0 mΒ² β |
| Wingspan | 49.0 m β |
| Height | 12.0 m β |
| Length | 51.3 m β |
| Maximum speed | 805 km/h β |
| Operational range | 4,723 km β |
| Service ceiling | 12,497 m β |
| Max. takeoff weight | 146,556 kg β |
| Empty weight | 65,540 kg β |
| Total thrust | 4 x 2,296 kgf β |
Performance Radar Chart
Detailed Comparison
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