Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:avionics |
glass cockpit
|
| gptkbp:basedOn |
gptkb:Mi-26
|
| gptkbp:capacity |
20,000 kg
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
2
|
| gptkbp:engine |
D-136-2
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
2011
|
| gptkbp:height |
8.145 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mi-26T2
|
| gptkbp:length |
40.025 m
|
| gptkbp:mainRotorDiameter |
32 m
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:maximumSpeed |
295 km/h
|
| gptkbp:maxTakeoffWeight |
56,000 kg
|
| gptkbp:notableFeature |
reduced crew workload
modern avionics suite night and all-weather capability |
| gptkbp:numberOfEngines |
2
|
| gptkbp:primaryUser |
gptkb:Russian_Air_Force
gptkb:Algerian_Air_Force |
| gptkbp:range |
800 km
|
| gptkbp:role |
heavy-lift cargo helicopter
|
| gptkbp:status |
in service
|
| gptkbp:bfsParent |
gptkb:Mil_Mi-26
|
| gptkbp:bfsLayer |
6
|