Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:armament |
machine guns
missiles rockets |
| gptkbp:capacity |
24 troops
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
3
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:enteredService |
1981 (Mi-17 family)
|
| gptkbp:exportedTo |
gptkb:India
gptkb:Iraq gptkb:Peru |
| gptkbp:family |
gptkb:Mil_Mi-8
|
| gptkbp:firstFlight |
1975 (Mi-17 family)
|
| gptkbp:height |
4.76 m
|
| gptkbp:length |
18.465 m
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:maximumSpeed |
250 km/h
|
| gptkbp:maxTakeoffWeight |
13,000 kg
|
| gptkbp:powerplant |
2 × Klimov VK-2500 turboshaft engines
|
| gptkbp:primaryUser |
gptkb:Russian_Air_Force
gptkb:Indian_Air_Force |
| gptkbp:range |
800 km
|
| gptkbp:role |
gptkb:helicopter
transport helicopter |
| gptkbp:bfsParent |
gptkb:Iranian_Air_Force
|
| gptkbp:bfsLayer |
6
|
| http://www.w3.org/2000/01/rdf-schema#label |
Mil Mi-17V-41
|