Il-20 Coot-A vs King Air 90
Overview
The Il-20 Coot-A and the King Air 90 are both Military Special Mission Aircraft, manufactured by Ilyushin and Beechcraft respectively.
Top speed is 675 km/h for the Il-20 Coot-A vs 494 km/h for the King Air 90. The Il-20 Coot-A has an operational range of 6,200 km vs 2,446 km for the King Air 90. The Il-20 Coot-A operates at altitudes up to 10,000 m compared to 7,574 m for the King Air 90. At 64,000 kg MTOW, the Il-20 Coot-A is 12:1 the King Air 90's 5,352 kg.
The King Air 90 first flew 4 years before the Il-20 Coot-A (1964 vs 1968).
| Soviet COMINT/ELINT surveillance-reconnaissance aircraft, developed in the late 1960s, used for electronic intelligence gathering and radar mapping. | |
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| Origin country | π¨π³ Ex-USSR |
| Category | Military Special Mission Aircraft |
| Manufacturer | Ilyushin |
| First flight | 21 March 1968 |
| Year introduced | -- |
| Number produced | N/A |
| Average unit price | -- |
| American twin-turboprop aircraft, prominently deployed for utility, corporate, and military purposes from the 1960s onward. | |
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| Origin country | πΊπΈ 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 | 140.6 mΒ² β |
| Wingspan | 37.4 m β |
| Height | 10.2 m β |
| Length | 35.9 m β |
| Maximum speed | 675 km/h β |
| Operational range | 6,200 km β |
| Service ceiling | 10,000 m β |
| Max. takeoff weight | 64,000 kg β |
| Empty weight | 33,760 kg β |
| Total thrust | 4 x 792 kW β |
| Wing area | 26.0 mΒ² β |
| Wingspan | 13.8 m β |
| Height | 4.7 m β |
| Length | 11.9 m β |
| Maximum speed | 494 km/h β |
| Operational range | 2,446 km β |
| Service ceiling | 7,574 m β |
| Max. takeoff weight | 5,352 kg β |
| Empty weight | 3,217 kg β |
| Total thrust | 2 x 313 kW β |
Performance Radar Chart
Detailed Comparison
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Frequently Asked Questions
Which is faster, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A is faster with a maximum speed of 675 km/h compared to the King Air 90's 494 km/h, a difference of 181 km/h.
Which has longer range, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A has a longer range at 6,200 km compared to the King Air 90's 2,446 km.
Which can fly higher, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A has a higher service ceiling at 10,000 meters (32,808 ft) compared to the King Air 90's 7,574 meters (24,849 ft).
Which is heavier, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A has a higher maximum takeoff weight at 64,000 kg compared to the King Air 90's 5,352 kg.
Which is larger, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A is longer at 35.9 meters compared to the King Air 90's 11.9 meters.