Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
4000 kg
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
3
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:exportedTo |
multiple countries
|
| gptkbp:family |
gptkb:Mil_Mi-8
|
| gptkbp:firstFlight |
1975
|
| gptkbp:height |
4.76 m
|
| gptkbp:length |
18.17 m
|
| gptkbp:mainRotorDiameter |
21.29 m
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:maximumSpeed |
250 km/h
|
| gptkbp:maxTakeoffWeight |
13000 kg
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:range |
800 km
|
| gptkbp:role |
gptkb:helicopter
transport helicopter |
| gptkbp:serviceCeiling |
6000 m
|
| gptkbp:usedBy |
gptkb:Afghan_Air_Force
gptkb:Russian_Air_Force gptkb:Indian_Air_Force gptkb:Mexican_Air_Force gptkb:Iraqi_Air_Force |
| gptkbp:variant |
gptkb:Mil_Mi-17
|
| gptkbp:weapon |
yes
|
| gptkbp:bfsParent |
gptkb:Iranian_Air_Force
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mil Mi-17V-16
|