C-130 Hercules vs Falcon 50
Overview
The C-130 Hercules and the Falcon 50 are both Military Transport Aircraft, manufactured by Lockheed and Dassault respectively.
Top speed is 593 km/h for the C-130 Hercules vs 888 km/h for the Falcon 50. The C-130 Hercules has an operational range of 3,800 km vs 5,695 km for the Falcon 50. The Falcon 50 operates at altitudes up to 13,716 m compared to 10,058 m for the C-130 Hercules. At 70,307 kg MTOW, the C-130 Hercules is 3.8x the Falcon 50's 18,500 kg.
The C-130 Hercules has been produced in 2,500 units vs 352 for the Falcon 50. Unit cost is $68M for the C-130 Hercules vs $6M for the Falcon 50. The C-130 Hercules first flew 22 years before the Falcon 50 (1954 vs 1976).
| 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 |
| French maritime surveillance jet, noteworthy for transcontinental capacity, extensively deployed for government, business, and emergency medical services. | |
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| Origin country | π«π· France |
| Category | Military Transport Aircraft |
| Manufacturer | Dassault |
| First flight | 1 November 1976 |
| Year introduced | 1979 |
| Number produced | 352 units |
| Average unit price | $6 million |
| Wing area | 162.0 mΒ² β |
| 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 |
| Wing area | 46.8 mΒ² β |
| Wingspan | 18.9 m β |
| Height | 7.0 m β |
| Length | 18.8 m β |
| Maximum speed | 888 km/h β |
| Operational range | 5,695 km β |
| Service ceiling | 13,716 m β |
| Max. takeoff weight | 18,500 kg β |
| Empty weight | 9,150 kg β |
| Total thrust | 3 x 560 kgf β |
Performance Radar Chart
Detailed Comparison
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