Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
20000 kg
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
5
|
| gptkbp:developedBy |
gptkb:Mil_Mi-26
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1996
|
| gptkbp:improves |
gptkb:Mi-26
|
| gptkbp:length |
40 m
|
| gptkbp:mainRotorDiameter |
32 m
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:maxTakeoffWeight |
56000 kg
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:role |
heavy-lift cargo helicopter
|
| gptkbp:status |
gptkb:prototype
|
| gptkbp:bfsParent |
gptkb:Mil_Mi-26
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mi-26M
|