Il-20 Coot-A vs Tu-214
Il-20 Coot-A vs Tu-214 at a glance — top speed 675 vs 900 km/h, range 6,200 vs 6,500 km, max takeoff weight 64,000 vs 110,750 kg.
Specifications
|
Il-20 Coot-A |
Tu-214 |
| Origin country |
🇷🇺 Ex-USSR |
🇷🇺 Russia |
| Category |
Military Special Mission Aircraft |
Military Transport Aircraft |
| Manufacturer |
Ilyushin |
Tupolev |
| First flight |
21 March 1968 |
21 March 1996 |
| Year introduced |
-- |
1996 |
| Number produced |
N/A |
89 units |
| Average unit price |
-- |
$65 million |
| Wing area |
140.6 m² |
184.2 m² |
| Wingspan |
37.4 m |
41.8 m |
| Height |
10.2 m |
13.9 m |
| Length |
35.9 m |
46.1 m |
| Maximum speed |
675 km/h |
900 km/h |
| Operational range |
6,200 km |
6,500 km |
| Service ceiling |
10,000 m |
12,100 m |
| Max. takeoff weight |
64,000 kg |
110,750 kg |
| Empty weight |
33,760 kg |
59,000 kg |
| Total thrust |
4 x 3,169 kW
|
2 x 16,000 kgf
|
Detailed Comparison
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Which is faster, the Il-20 Coot-A or Tu-214?
The Tu-214 is faster with a maximum speed of 900 km/h compared to the Il-20 Coot-A's 675 km/h, a difference of 225 km/h.
Which has longer range, the Il-20 Coot-A or Tu-214?
The Tu-214 has a longer range at 6,500 km compared to the Il-20 Coot-A's 6,200 km.
Which can fly higher, the Il-20 Coot-A or Tu-214?
The Tu-214 has a higher service ceiling at 12,100 meters (39,698 ft) compared to the Il-20 Coot-A's 10,000 meters (32,808 ft).
Which is heavier, the Il-20 Coot-A or Tu-214?
The Tu-214 has a higher maximum takeoff weight at 110,750 kg compared to the Il-20 Coot-A's 64,000 kg.
Which is larger, the Il-20 Coot-A or Tu-214?
The Tu-214 is longer at 46.1 meters compared to the Il-20 Coot-A's 35.9 meters.
