Statements (33)
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
|
https://www.w3.org/2000/01/rdf-schema#label |
Mi-28UB
|
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_helicopter
gptkb:Mi-28攻撃ヘリコプター gptkb:Ми-28 gptkb:Mil_Mi-28 gptkb:Mi-28 |
gptkbp:bfsLayer |
6
|