Il-20 Coot-A vs Il-38 May
Il-20 Coot-A vs Il-38 May at a glance — top speed 675 vs 650 km/h, range 6,200 vs 7,500 km, max takeoff weight 64,000 vs 66,000 kg.
Specifications
|
Il-20 Coot-A |
Il-38 May |
| Origin country |
🇷🇺 Ex-USSR |
🇷🇺 Ex-USSR |
| Category |
Military Special Mission Aircraft |
Military Special Mission Aircraft |
| Manufacturer |
Ilyushin |
Ilyushin |
| First flight |
21 March 1968 |
27 September 1961 |
| Year introduced |
-- |
1967 |
| Number produced |
N/A |
58 units |
| Average unit price |
-- |
-- |
| Wing area |
140.6 m² |
140.0 m² |
| Wingspan |
37.4 m |
37.4 m |
| Height |
10.2 m |
10.2 m |
| Length |
35.9 m |
40.1 m |
| Maximum speed |
675 km/h |
650 km/h |
| Operational range |
6,200 km |
7,500 km |
| Service ceiling |
10,000 m |
11,000 m |
| Max. takeoff weight |
64,000 kg |
66,000 kg |
| Empty weight |
33,760 kg |
34,630 kg |
| Total thrust |
4 x 3,169 kW
|
4 x 3,126 kW
|
Detailed Comparison
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Which is faster, the Il-20 Coot-A or Il-38 May?
The Il-20 Coot-A is faster with a maximum speed of 675 km/h compared to the Il-38 May's 650 km/h, a difference of 25 km/h.
Which has longer range, the Il-20 Coot-A or Il-38 May?
The Il-38 May has a longer range at 7,500 km compared to the Il-20 Coot-A's 6,200 km.
Which can fly higher, the Il-20 Coot-A or Il-38 May?
The Il-38 May has a higher service ceiling at 11,000 meters (36,089 ft) compared to the Il-20 Coot-A's 10,000 meters (32,808 ft).
Which is heavier, the Il-20 Coot-A or Il-38 May?
The Il-38 May has a higher maximum takeoff weight at 66,000 kg compared to the Il-20 Coot-A's 64,000 kg.
Which is larger, the Il-20 Coot-A or Il-38 May?
The Il-38 May is longer at 40.1 meters compared to the Il-20 Coot-A's 35.9 meters.
