Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:armament |
machine guns
missiles rockets |
| gptkbp:capacity |
4,000 kg
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:crew |
3
|
| gptkbp:developedBy |
gptkb:Mil_Mi-8
|
| gptkbp:engineType |
twin-turbine
|
| gptkbp:enteredService |
1981
|
| gptkbp:firstFlight |
1975
|
| gptkbp:height |
4.76 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mil Mi-17V-21
|
| gptkbp:length |
18.17 m
|
| gptkbp:mainRotorDiameter |
21.3 m
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:maximumSpeed |
250 km/h
|
| gptkbp:maxTakeoffWeight |
13,000 kg
|
| gptkbp:NATOReportingName |
Hip-H
|
| gptkbp:operator |
gptkb:China
gptkb:India gptkb:Iraq gptkb:Mexico gptkb:Russia |
| gptkbp:range |
800 km
|
| gptkbp:role |
gptkb:helicopter
transport helicopter |
| gptkbp:seatingCapacity |
24
|
| gptkbp:serviceCeiling |
6,000 m
|
| gptkbp:bfsParent |
gptkb:Iranian_Air_Force
|
| gptkbp:bfsLayer |
5
|