Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:avionics |
modernized digital avionics suite
|
| gptkbp:basedOn |
gptkb:Mi-26
|
| gptkbp:capacity |
20,000 kg
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
5
|
| gptkbp:developedBy |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:engine |
D-136
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:features |
gptkb:glass_cockpit
improved survivability enhanced navigation system night operation capability |
| gptkbp:firstFlight |
2018
|
| gptkbp:height |
8.15 m
|
| gptkbp:introduced |
2022
|
| gptkbp:length |
40 m
|
| gptkbp:mainRotorDiameter |
32 m
|
| gptkbp:manufacturer |
gptkb:Rostvertol
|
| gptkbp:maximumSpeed |
295 km/h
|
| gptkbp:maxTakeoffWeight |
56,000 kg
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:primaryUser |
gptkb:Russian_Aerospace_Forces
|
| gptkbp:range |
800 km
|
| gptkbp:role |
heavy-lift cargo helicopter
|
| gptkbp:selfProtectionSystem |
gptkb:Vitebsk
|
| gptkbp:bfsParent |
gptkb:Mil_Mi-26
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mi-26T2V
|