E-3 Sentry AWACS vs E-6 Mercury TACAMO
Overview
The E-3 Sentry AWACS and the E-6 Mercury TACAMO are both Military Special Mission Aircraft, manufactured by Boeing and Boeing respectively.
Top speed is 853 km/h for the E-3 Sentry AWACS vs 966 km/h for the E-6 Mercury TACAMO. The E-3 Sentry AWACS has an operational range of 7,400 km vs 12,000 km for the E-6 Mercury TACAMO. The E-6 Mercury TACAMO operates at altitudes up to 12,192 m compared to 10,668 m for the E-3 Sentry AWACS.
The E-3 Sentry AWACS has been produced in 68 units vs 16 for the E-6 Mercury TACAMO. Unit cost is $270M for the E-3 Sentry AWACS vs $141M for the E-6 Mercury TACAMO. The E-3 Sentry AWACS first flew 15 years before the E-6 Mercury TACAMO (1972 vs 1987).
| American airborne early warning and control (AWACS) aircraft, principally used in NATO, UK, France, and Saudi Arabia since the Cold War. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing |
| First flight | 9 February 1972 |
| Year introduced | 1977 |
| Number produced | 68 units |
| Average unit price | $270 million |
| American command-and-control aircraft, operative during the Cold War era, kept primarily for communications with U.S. nuclear forces. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing |
| First flight | 19 February 1987 |
| Year introduced | 1989 |
| Number produced | 16 units |
| Average unit price | $141 million |
| Wing area | 283.0 mΒ² |
| Wingspan | 44.4 m β |
| Height | 12.6 m β |
| Length | 46.6 m β |
| Maximum speed | 853 km/h β |
| Operational range | 7,400 km β |
| Service ceiling | 10,668 m β |
| Max. takeoff weight | 147,417 kg β |
| Empty weight | 83,915 kg β |
| Total thrust | 4 x 2,438 kgf β |
| Wing area | -- mΒ² |
| Wingspan | 45.2 m β |
| Height | 12.9 m β |
| Length | 45.8 m β |
| Maximum speed | 966 km/h β |
| Operational range | 12,000 km β |
| Service ceiling | 12,192 m β |
| Max. takeoff weight | 155,128 kg β |
| Empty weight | 78,378 kg β |
| Total thrust | 4 x 2,803 kgf β |
Performance Radar Chart
Detailed Comparison
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