E-4 NOAC vs E-6 Mercury TACAMO
| American advanced airborne command post, launched during the Cold War, extensively employed for national emergency operations. | |
|
|
| Origin country | 🇺🇸 United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing |
| First flight | 1 January 1980 |
| Year introduced | 1974 |
| Number produced | 4 units |
| Average unit price | $223 million |
| American command-and-control aircraft, operative during the Cold War era, kept primarily for communications with U.S. nuclear forces. | |
|
|
| Origin country | 🇺🇸 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 | 510.0 m² |
| Wingspan | 59.7 m â—‰ |
| Height | 19.3 m â—‰ |
| Length | 70.5 m â—‰ |
| Maximum speed | 969 km/h â—‰ |
| Operational range | 12,600 km â—‰ |
| Service ceiling | 13,716 m â—‰ |
| Max. takeoff weight | 374,850 kg â—‰ |
| Empty weight | 190,000 kg |
| Total thrust | 4 x 23,814 kgf â—‰ |
|
|
| Wing area | -- m² |
| Wingspan | 45.2 m â—‰ |
| Height | 12.9 m â—‰ |
| Length | 45.8 m â—‰ |
| Maximum speed | 966 km/h â—‰ |
| Operational range | 12,000 km â—‰ |
| Service ceiling | 12,192 m â—‰ |
| Max. takeoff weight | 155,128 kg â—‰ |
| Empty weight | -- kg |
| Total thrust | 4 x 11,213 kgf â—‰ |
|
|
Performance Radar Chart
Frequently Asked Questions
Which is faster, the E-4 NOAC or E-6 Mercury TACAMO?
The E-4 NOAC is faster with a maximum speed of 969 km/h compared to the E-6 Mercury TACAMO's 966 km/h, a difference of 3 km/h.
Which has longer range, the E-4 NOAC or E-6 Mercury TACAMO?
The E-4 NOAC has a longer range at 12,600 km compared to the E-6 Mercury TACAMO's 12,000 km.
Which can fly higher, the E-4 NOAC or E-6 Mercury TACAMO?
The E-4 NOAC has a higher service ceiling at 13,716 meters (45,000 ft) compared to the E-6 Mercury TACAMO's 12,192 meters (40,000 ft).
Which is heavier, the E-4 NOAC or E-6 Mercury TACAMO?
The E-4 NOAC has a higher maximum takeoff weight at 374,850 kg compared to the E-6 Mercury TACAMO's 155,128 kg.
Which is larger, the E-4 NOAC or E-6 Mercury TACAMO?
The E-4 NOAC is longer at 70.5 meters compared to the E-6 Mercury TACAMO's 45.8 meters.
Which is more expensive, the E-4 NOAC or E-6 Mercury TACAMO?
The E-4 NOAC is more expensive at approximately $223 million per unit compared to the E-6 Mercury TACAMO at $141 million.
Which entered service first, the E-4 NOAC or E-6 Mercury TACAMO?
The E-4 NOAC entered service first in 1974, 15 years before the E-6 Mercury TACAMO which entered service in 1989.
Which has been built in greater numbers, the E-4 NOAC or E-6 Mercury TACAMO?
The E-6 Mercury TACAMO has been produced in greater numbers with 16 units compared to 4 units of the E-4 NOAC.