DHC-2 Beaver vs EC-130 Commando Solo
Overview
The DHC-2 Beaver and the EC-130 Commando Solo are both Military Special Mission Aircraft, manufactured by De Havilland Canada and Lockheed Martin respectively.
The EC-130 Commando Solo reaches 671 km/h β 2.6x the DHC-2 Beaver's 254 km/h. The DHC-2 Beaver has an operational range of 732 km vs 4,300 km for the EC-130 Commando Solo. The EC-130 Commando Solo operates at altitudes up to 8,534 m compared to 5,486 m for the DHC-2 Beaver.
The DHC-2 Beaver has been produced in 1,657 units vs 14 for the EC-130 Commando Solo. Unit cost is $0.4M for the DHC-2 Beaver vs $150M for the EC-130 Commando Solo. The DHC-2 Beaver first flew 10 years before the EC-130 Commando Solo (1947 vs 1957).
| Canadian utility aircraft, renowned for bush flying since the mid-20th century, widely deployed for civilian and military operations. | |
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| Origin country | π¨π¦ Canada |
| Category | Military Special Mission Aircraft |
| Manufacturer | De Havilland Canada |
| First flight | 16 August 1947 |
| Year introduced | 1948 |
| Number produced | 1657 units |
| Average unit price | $400K |
| 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 |
| Wing area | 23.0 mΒ² β |
| Wingspan | 15.0 m β |
| Height | 2.7 m β |
| Length | 9.2 m β |
| Maximum speed | 254 km/h β |
| Operational range | 732 km β |
| Service ceiling | 5,486 m β |
| Max. takeoff weight | -- kg |
| Empty weight | 1,361 kg β |
| Total thrust | 1 x 336 kW β |
| 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 |
| Empty weight | 34,274 kg β |
| Total thrust | 4 x 1,119 kW β |
Performance Radar Chart
Detailed Comparison
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