Il-20 Coot-A vs Cirrus SR-20
Il-20 Coot-A vs Cirrus SR-20 at a glance — top speed 675 vs 287 km/h, range 6,200 vs 1,450 km, max takeoff weight 64,000 vs 1,383 kg.
Specifications
|
Il-20 Coot-A |
Cirrus SR-20 |
| Origin country |
🇷🇺 Ex-USSR |
🇺🇸 United States |
| Category |
Military Special Mission Aircraft |
Military Special Mission Aircraft |
| Manufacturer |
Ilyushin |
Cirrus |
| First flight |
21 March 1968 |
21 March 1995 |
| Year introduced |
-- |
1999 |
| Number produced |
N/A |
1459 units |
| Average unit price |
-- |
$630K |
| Wing area |
140.6 m² |
13.5 m² |
| Wingspan |
37.4 m |
11.7 m |
| Height |
10.2 m |
2.5 m |
| Length |
35.9 m |
8.0 m |
| Maximum speed |
675 km/h |
287 km/h |
| Operational range |
6,200 km |
1,450 km |
| Service ceiling |
10,000 m |
5,334 m |
| Max. takeoff weight |
64,000 kg |
1,383 kg |
| Empty weight |
33,760 kg |
943 kg |
| Total thrust |
4 x 3,169 kW
|
1 x 149 kW
|
Detailed Comparison
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Which is faster, the Il-20 Coot-A or Cirrus SR-20?
The Il-20 Coot-A is faster with a maximum speed of 675 km/h compared to the Cirrus SR-20's 287 km/h, a difference of 388 km/h.
Which has longer range, the Il-20 Coot-A or Cirrus SR-20?
The Il-20 Coot-A has a longer range at 6,200 km compared to the Cirrus SR-20's 1,450 km.
Which can fly higher, the Il-20 Coot-A or Cirrus SR-20?
The Il-20 Coot-A has a higher service ceiling at 10,000 meters (32,808 ft) compared to the Cirrus SR-20's 5,334 meters (17,500 ft).
Which is heavier, the Il-20 Coot-A or Cirrus SR-20?
The Il-20 Coot-A has a higher maximum takeoff weight at 64,000 kg compared to the Cirrus SR-20's 1,383 kg.
Which is larger, the Il-20 Coot-A or Cirrus SR-20?
The Il-20 Coot-A is longer at 35.9 meters compared to the Cirrus SR-20's 8.0 meters.
