E-6 Mercury TACAMO vs S-3 Viking
Overview
The E-6 Mercury TACAMO and the S-3 Viking are both Military Special Mission Aircraft, manufactured by Boeing and Lockheed respectively.
Top speed is 966 km/h for the E-6 Mercury TACAMO vs 815 km/h for the S-3 Viking. The E-6 Mercury TACAMO has an operational range of 12,000 km vs 5,121 km for the S-3 Viking. The S-3 Viking operates at altitudes up to 12,466 m compared to 12,192 m for the E-6 Mercury TACAMO. At 155,128 kg MTOW, the E-6 Mercury TACAMO is 6.5x the S-3 Viking's 23,831 kg.
The E-6 Mercury TACAMO has been produced in 16 units vs 188 for the S-3 Viking. Unit cost is $141M for the E-6 Mercury TACAMO vs $27M for the S-3 Viking. The S-3 Viking first flew 15 years before the E-6 Mercury TACAMO (1972 vs 1987).
| 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 |
| American anti-submarine aircraft, operational during the Cold War, recognized for its service in Gulf War naval missions. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Lockheed |
| First flight | 21 January 1972 |
| Year introduced | 1974 |
| Number produced | 188 units |
| Average unit price | $27 million |
| 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 |
| Wing area | 56.0 mΒ² |
| Wingspan | 21.0 m β |
| Height | 7.0 m β |
| Length | 16.3 m β |
| Maximum speed | 815 km/h β |
| Operational range | 5,121 km β |
| Service ceiling | 12,466 m β |
| Max. takeoff weight | 23,831 kg β |
| Empty weight | 12,057 kg β |
| Total thrust | 2 x 2,104 kgf β |
Performance Radar Chart
Detailed Comparison
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