An-32 Cline vs C-130 Hercules
Overview
The An-32 Cline and the C-130 Hercules are both Military Transport Aircraft, manufactured by Antonov and Lockheed respectively.
Top speed is 530 km/h for the An-32 Cline vs 593 km/h for the C-130 Hercules. The An-32 Cline has an operational range of 1,400 km vs 3,800 km for the C-130 Hercules. The C-130 Hercules operates at altitudes up to 10,058 m compared to 9,000 m for the An-32 Cline. At 70,307 kg MTOW, the C-130 Hercules is 2.5x the An-32 Cline's 28,500 kg.
The An-32 Cline has been produced in 373 units vs 2,500 for the C-130 Hercules. Unit cost is $15M for the An-32 Cline vs $68M for the C-130 Hercules. The C-130 Hercules first flew 22 years before the An-32 Cline (1954 vs 1976).
| Soviet transport plane, widely deployed in domestic and overseas services, notably utilized in various military and humanitarian missions. | |
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| Origin country | πΊπ¦ Ukraine |
| Category | Military Transport Aircraft |
| Manufacturer | Antonov |
| First flight | 9 July 1976 |
| Year introduced | 1982 |
| Number produced | 373 units |
| Average unit price | $15 million |
| American military transport aircraft, known for significant roles in Vietnam War and Desert Storm, extensively used for various cargo missions. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Lockheed |
| First flight | 23 August 1954 |
| Year introduced | 1956 |
| Number produced | 2500 units |
| Average unit price | $68 million |
| Wing area | -- mΒ² |
| Wingspan | 29.2 m β |
| Height | 8.8 m β |
| Length | 24.5 m β |
| Maximum speed | 530 km/h β |
| Operational range | 1,400 km β |
| Service ceiling | 9,000 m β |
| Max. takeoff weight | 28,500 kg β |
| Empty weight | 16,800 kg β |
| Total thrust | 2 x 1,864 kW β |
| Wing area | 162.0 mΒ² |
| Wingspan | 40.4 m β |
| Height | 11.7 m β |
| Length | 29.8 m β |
| Maximum speed | 593 km/h β |
| Operational range | 3,800 km β |
| Service ceiling | 10,058 m β |
| Max. takeoff weight | 70,307 kg β |
| Empty weight | 35,800 kg β |
| Total thrust | 4 x 915 kW β |
Performance Radar Chart
Detailed Comparison
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