Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
4000 kg
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
3
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:family |
gptkb:Mil_Mi-8/17_series
|
| gptkbp:firstFlight |
2017
|
| gptkbp:height |
5.65 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mil Mi-17V-60
|
| gptkbp:length |
18.4 m
|
| gptkbp:mainRotorDiameter |
21.3 m
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:maximumSpeed |
250 km/h
|
| gptkbp:maxTakeoffWeight |
13500 kg
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:range |
800 km
|
| gptkbp:role |
transport helicopter
|
| gptkbp:status |
in production
|
| gptkbp:bfsParent |
gptkb:Iranian_Air_Force
|
| gptkbp:bfsLayer |
5
|