C-130 Hercules vs C-2 Greyhound
Overview
The C-130 Hercules and the C-2 Greyhound are both Military Transport Aircraft, manufactured by Lockheed and Northrop Grumman respectively.
Top speed is 593 km/h for the C-130 Hercules vs 635 km/h for the C-2 Greyhound. The C-130 Hercules has an operational range of 3,800 km vs 2,400 km for the C-2 Greyhound. The C-2 Greyhound operates at altitudes up to 10,211 m compared to 10,058 m for the C-130 Hercules. At 70,307 kg MTOW, the C-130 Hercules is 2.6x the C-2 Greyhound's 27,216 kg.
The C-130 Hercules has been produced in 2,500 units vs 56 for the C-2 Greyhound. Unit cost is $68M for the C-130 Hercules vs $39M for the C-2 Greyhound. The C-130 Hercules first flew 10 years before the C-2 Greyhound (1954 vs 1964).
| 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 |
| American carrier onboard delivery aircraft, commonly deployed in the late 20th century for logistics support at sea. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Northrop Grumman |
| First flight | 18 November 1964 |
| Year introduced | 1966 |
| Number produced | 56 units |
| Average unit price | $39 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 | 65.0 mΒ² β |
| Wingspan | 24.6 m β |
| Height | 4.9 m β |
| Length | 17.1 m β |
| Maximum speed | 635 km/h β |
| Operational range | 2,400 km β |
| Service ceiling | 10,211 m β |
| Max. takeoff weight | 27,216 kg β |
| Empty weight | 15,307 kg β |
| Total thrust | 2 x 1,715 kW β |
Performance Radar Chart
Detailed Comparison
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