E-6 Mercury TACAMO vs Hawker 800
Overview
The E-6 Mercury TACAMO and the Hawker 800 are both Military Special Mission Aircraft, manufactured by Boeing and Hawker Beechcraft respectively.
Top speed is 966 km/h for the E-6 Mercury TACAMO vs 830 km/h for the Hawker 800. The E-6 Mercury TACAMO has an operational range of 12,000 km vs 5,232 km for the Hawker 800. The Hawker 800 operates at altitudes up to 12,497 m compared to 12,192 m for the E-6 Mercury TACAMO. At 155,128 kg MTOW, the E-6 Mercury TACAMO is 12:1 the Hawker 800's 12,701 kg.
The E-6 Mercury TACAMO has been produced in 16 units vs 650 for the Hawker 800. Unit cost is $141M for the E-6 Mercury TACAMO vs $13.78M for the Hawker 800. The Hawker 800 first flew 4 years before the E-6 Mercury TACAMO (1983 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 |
| British mid-size twinjet corporate aircraft, known for its international charters and private operations since the mid-1980s. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Hawker Beechcraft |
| First flight | 26 June 1983 |
| Year introduced | 1983 |
| Number produced | 650 units |
| Average unit price | $13.8 million |
| 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 |
| Wingspan | 16.6 m β |
| Height | 5.5 m β |
| Length | 15.6 m β |
| Maximum speed | 830 km/h β |
| Operational range | 5,232 km β |
| Service ceiling | 12,497 m β |
| Max. takeoff weight | 12,701 kg β |
| Empty weight | 7,108 kg β |
| Total thrust | 2 x 1,057 kgf β |
Performance Radar Chart
Detailed Comparison
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