Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:armament |
gptkb:30_mm_Shipunov_2A42_autocannon
air-to-air missiles rocket pods anti-tank guided missiles |
| gptkbp:basedOn |
gptkb:Mi-28N
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
2
|
| gptkbp:engine |
gptkb:Klimov_TV3-117VMA
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:enteredService |
2017
|
| gptkbp:feature |
advanced avionics
improved crew survivability dual controls |
| gptkbp:firstFlight |
2013
|
| gptkbp:length |
17.01 m
|
| gptkbp:mainRotorDiameter |
17.2 m
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:maximumSpeed |
300 km/h
|
| gptkbp:maxTakeoffWeight |
11,500 kg
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:primaryUser |
gptkb:Russian_Air_Force
|
| gptkbp:range |
435 km
|
| gptkbp:role |
training helicopter
combat helicopter |
| gptkbp:serviceCeiling |
5,600 m
|
| gptkbp:bfsParent |
gptkb:Mi-28
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mi-28UB
|