EA-6B Prowler vs EC-130 Commando Solo
Overview
The EA-6B Prowler and the EC-130 Commando Solo are both Military Special Mission Aircraft, manufactured by Grumman and Lockheed Martin respectively.
Top speed is 1,048 km/h for the EA-6B Prowler vs 671 km/h for the EC-130 Commando Solo. The EA-6B Prowler has an operational range of 3,745 km vs 4,300 km for the EC-130 Commando Solo. The EA-6B Prowler operates at altitudes up to 11,460 m compared to 8,534 m for the EC-130 Commando Solo. At 74,389 kg MTOW, the EC-130 Commando Solo is 2.7x the EA-6B Prowler's 27,896 kg.
The EA-6B Prowler has been produced in 170 units vs 14 for the EC-130 Commando Solo. Unit cost is $52M for the EA-6B Prowler vs $150M for the EC-130 Commando Solo. The EC-130 Commando Solo first flew 11 years before the EA-6B Prowler (1957 vs 1968).
| American electronic warfare aircraft, vital during the Cold War, widely deployed in Iraq and Afghanistan conflicts. | |
|
|
| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Grumman |
| First flight | 25 May 1968 |
| Year introduced | 1971 |
| Number produced | 170 units |
| Average unit price | $52 million |
| American electronic operations aircraft, deployed extensively during conflicts from Vietnam to recent operations in the Middle East. | |
|
|
| 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 | 49.2 mΒ² β |
| Wingspan | 16.0 m β |
| Height | 5.1 m β |
| Length | 18.0 m β |
| Maximum speed | 1048 km/h β |
| Operational range | 3,745 km β |
| Service ceiling | 11,460 m β |
| Max. takeoff weight | 27,896 kg β |
| Empty weight | 14,134 kg β |
| Total thrust | 2 x 2,359 kgf 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 β |
| Empty weight | 34,274 kg β |
| Total thrust | 4 x 1,119 kW β |
Performance Radar Chart
Detailed Comparison
Generating comparison analysis...
Unable to generate comparison at this time.