| Technical data | |
|---|---|
| Type | Il-80 |
| Function | Airborne command |
| Year | ? |
| Crew | ? |
| Engines | 4*13,000kg NK-86? |
| Length | 59.94m |
| Height | 15.8m |
| Wingspan | 40.06m |
| Wing area | 320m2 |
| Empty weight | ?kg |
| Loaded weight | ?kg |
| Wing Load (kg/m2) | ? |
| Thrust to Weight |
? |
| Speed | ?km/h |
| Landing Speed | ?km/h |
| Landing Roll | ?m |
| Takeoff Roll | ?m |
| Turn time | ?sec |
| Range | ?km |
| Flight Endurance | ?hmin |
| Ceiling | ?m |
| Climb | |
| 1000m | ?min |
| Payload | |
| Fuel | ?kg |
| Armament | |
| Guns | ? |
| Rockets | ? |
Il-80 by Ilyushin OKB
Airborne command center, based on Il-86 widebody airliner. Designation also was used for cancelled SLAR aircraft of Il-76 family.
Three Il-86 airframes were equipped as Il-80, intended for use in case of nuclear conflict.
| Created July 13, 1999 |  |
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