C-130 Hercules vs Short 360
Overview
The C-130 Hercules and the Short 360 are both Military Transport Aircraft, manufactured by Lockheed and Short Brothers respectively.
Top speed is 593 km/h for the C-130 Hercules vs 404 km/h for the Short 360. The C-130 Hercules has an operational range of 3,800 km vs 1,595 km for the Short 360. The C-130 Hercules operates at altitudes up to 10,058 m compared to 6,100 m for the Short 360. At 70,307 kg MTOW, the C-130 Hercules is 5.7x the Short 360's 12,292 kg.
The C-130 Hercules has been produced in 2,500 units vs 165 for the Short 360. Unit cost is $68M for the C-130 Hercules vs $6.19M for the Short 360. The C-130 Hercules first flew 27 years before the Short 360 (1954 vs 1981).
| 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 |
| British commuter aircraft, recognized for its mid-1980s production, routinely seen for passenger and freight operations globally. | |
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| Origin country | π¬π§ United Kingdom |
| Category | Military Transport Aircraft |
| Manufacturer | Short Brothers |
| First flight | 1 June 1981 |
| Year introduced | 1982 |
| Number produced | 165 units |
| Average unit price | $6.2 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 | 42.1 mΒ² β |
| Wingspan | 22.8 m β |
| Height | 7.2 m β |
| Length | 21.6 m β |
| Maximum speed | 404 km/h β |
| Operational range | 1,595 km β |
| Service ceiling | 6,100 m β |
| Max. takeoff weight | 12,292 kg β |
| Empty weight | 7,870 kg β |
| Total thrust | 2 x 531 kW β |
Performance Radar Chart
Detailed Comparison
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