E-4 NOAC vs King Air 90
Overview
The E-4 NOAC and the King Air 90 are both Military Special Mission Aircraft, manufactured by Boeing and Beechcraft respectively.
Top speed is 969 km/h for the E-4 NOAC vs 494 km/h for the King Air 90. The E-4 NOAC has an operational range of 12,600 km vs 2,446 km for the King Air 90. The E-4 NOAC operates at altitudes up to 13,716 m compared to 7,574 m for the King Air 90. At 374,850 kg MTOW, the E-4 NOAC is 70:1 the King Air 90's 5,352 kg.
The E-4 NOAC has been produced in 4 units vs 3,100 for the King Air 90. The King Air 90 first flew 16 years before the E-4 NOAC (1964 vs 1980).
| 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 twin-turboprop aircraft, prominently deployed for utility, corporate, and military purposes from the 1960s onward. | |
|
|
| Origin country | 🇺🇸 United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Beechcraft |
| First flight | 1 January 1964 |
| Year introduced | 1964 |
| Number produced | 3100 units |
| Average unit price | -- |
| Wing area | 510.0 m² ◉ |
| Wingspan | 59.7 m ◉ |
| Height | 19.3 m ◉ |
| Length | 70.5 m ◉ |
| Maximum speed | 969 km/h ◉ |
| Operational range | 12,600 km ◉ |
| Service ceiling | 13,716 m ◉ |
| Max. takeoff weight | 374,850 kg ◉ |
| Empty weight | 190,000 kg ◉ |
| Total thrust | 4 x 5,954 kgf ◉ |
| Wing area | 26.0 m² ◉ |
| Wingspan | 13.8 m ◉ |
| Height | 4.7 m ◉ |
| Length | 11.9 m ◉ |
| Maximum speed | 494 km/h ◉ |
| Operational range | 2,446 km ◉ |
| Service ceiling | 7,574 m ◉ |
| Max. takeoff weight | 5,352 kg ◉ |
| Empty weight | 3,217 kg ◉ |
| Total thrust | 2 x 313 kW ◉ |
Performance Radar Chart
Detailed Comparison
Loading analysis...
Generating comparison analysis...
Unable to generate comparison at this time.
Frequently Asked Questions
Which is faster, the E-4 NOAC or King Air 90?
The E-4 NOAC is faster with a maximum speed of 969 km/h compared to the King Air 90's 494 km/h, a difference of 475 km/h.
Which has longer range, the E-4 NOAC or King Air 90?
The E-4 NOAC has a longer range at 12,600 km compared to the King Air 90's 2,446 km.
Which can fly higher, the E-4 NOAC or King Air 90?
The E-4 NOAC has a higher service ceiling at 13,716 meters (45,000 ft) compared to the King Air 90's 7,574 meters (24,849 ft).
Which is heavier, the E-4 NOAC or King Air 90?
The E-4 NOAC has a higher maximum takeoff weight at 374,850 kg compared to the King Air 90's 5,352 kg.
Which is larger, the E-4 NOAC or King Air 90?
The E-4 NOAC is longer at 70.5 meters compared to the King Air 90's 11.9 meters.
Which entered service first, the E-4 NOAC or King Air 90?
The King Air 90 entered service first in 1964, 10 years before the E-4 NOAC which entered service in 1974.
Which has been built in greater numbers, the E-4 NOAC or King Air 90?
The King Air 90 has been produced in greater numbers with 3,100 units compared to 4 units of the E-4 NOAC.