EC-130 Commando Solo vs EF-111 Raven
Overview
The EC-130 Commando Solo and the EF-111 Raven are both Military Special Mission Aircraft, manufactured by Lockheed Martin and General Dynamics/Grumman respectively.
The EF-111 Raven reaches 2,350 km/h β 3.5x the EC-130 Commando Solo's 671 km/h. The EC-130 Commando Solo has an operational range of 4,300 km vs 3,220 km for the EF-111 Raven. The EF-111 Raven operates at altitudes up to 17,000 m compared to 8,534 m for the EC-130 Commando Solo.
The EC-130 Commando Solo has been produced in 14 units vs 42 for the EF-111 Raven. Unit cost is $150M for the EC-130 Commando Solo vs $65M for the EF-111 Raven. The EC-130 Commando Solo first flew 20 years before the EF-111 Raven (1957 vs 1977).
| 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 electronic warfare aircraft, extensively deployed in Gulf War, notable for radar jamming and deception operations. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | General Dynamics/Grumman |
| First flight | 1 January 1977 |
| Year introduced | 1981 |
| Number produced | 42 units |
| Average unit price | $65 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 | 48.8 mΒ² β |
| Wingspan | 19.2 m β |
| Height | 5.0 m β |
| Length | 23.5 m β |
| Maximum speed | 2350 km/h β |
| Operational range | 3,220 km β |
| Service ceiling | 17,000 m β |
| Max. takeoff weight | 39,680 kg β |
| Empty weight | 24,230 kg β |
| Total thrust | 2 x 4,195 kgf β |
Performance Radar Chart
Detailed Comparison
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