EC-130 Commando Solo vs KC-130 Hercules
Overview
The EC-130 Commando Solo and the KC-130 Hercules are both Military Special Mission Aircraft, manufactured by Lockheed Martin and Lockheed Martin respectively.
Top speed is 671 km/h for the EC-130 Commando Solo vs 670 km/h for the KC-130 Hercules. The EC-130 Commando Solo has an operational range of 4,300 km vs 5,250 km for the KC-130 Hercules. The EC-130 Commando Solo operates at altitudes up to 8,534 m compared to 8,534 m for the KC-130 Hercules.
The EC-130 Commando Solo has been produced in 14 units vs 124 for the KC-130 Hercules. Unit cost is $150M for the EC-130 Commando Solo vs $22M for the KC-130 Hercules. The EC-130 Commando Solo first flew 3 years before the KC-130 Hercules (1957 vs 1960).
| American electronic operations aircraft, deployed extensively during conflicts from Vietnam to recent operations in the Middle East. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Lockheed Martin |
| First flight | 1 January 1957 |
| Year introduced | 1975 |
| Number produced | 14 units |
| Average unit price | $150 million |
| American military transport aircraft, noted for tactical refueling and cargo application, extensively operational during Cold War era and beyond. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Lockheed Martin |
| First flight | 1 January 1960 |
| Year introduced | 1962 |
| Number produced | 124 units |
| Average unit price | $22 million |
| Wing area | 162.0 mΒ² β |
| Wingspan | 40.3 m β |
| Height | 11.8 m β |
| Length | 29.7 m β |
| Maximum speed | 671 km/h β |
| Operational range | 4,300 km β |
| Service ceiling | 8,534 m β |
| Max. takeoff weight | 74,389 kg β |
| Empty weight | 34,274 kg β |
| Total thrust | 4 x 1,119 kW β |
| Wing area | 162.0 mΒ² β |
| Wingspan | 40.4 m β |
| Height | 11.6 m β |
| Length | 29.8 m β |
| Maximum speed | 670 km/h β |
| Operational range | 5,250 km β |
| Service ceiling | 8,534 m β |
| Max. takeoff weight | 79,379 kg β |
| Empty weight | 34,274 kg β |
| Total thrust | 4 x 1,119 kW β |
Performance Radar Chart
Detailed Comparison
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