gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:armament
|
gptkb:30_mm_Shipunov_2A42_autocannon
air-to-air missiles
rocket pods
anti-tank guided missiles
|
gptkbp:avionics
|
gptkb:radar
night vision system
thermal imaging system
|
gptkbp:countryOfOrigin
|
gptkb:Russia
|
gptkbp:crew
|
2
|
gptkbp:engine
|
gptkb:Klimov_TV3-117VMA
|
gptkbp:engineType
|
turboshaft
|
gptkbp:exportedTo
|
gptkb:Algeria
gptkb:Iraq
gptkb:Uganda
|
gptkbp:firstFlight
|
1982
|
gptkbp:hasEjectionSeats
|
no
|
gptkbp:height
|
3.82 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mil Mi-28
|
gptkbp:introduced
|
2009
|
gptkbp:landingGear
|
retractable tricycle
|
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:NATOReportingName
|
gptkb:Havoc
|
gptkbp:nickname
|
gptkb:Havoc
|
gptkbp:numberOfEngines
|
2
|
gptkbp:primaryUser
|
gptkb:Russian_Air_Force
|
gptkbp:range
|
435 km
|
gptkbp:role
|
close air support
anti-armor
armed reconnaissance
|
gptkbp:tailRotorType
|
X-type
|
gptkbp:usedInConflict
|
gptkb:Syrian_Civil_War
gptkb:Russo-Ukrainian_War
|
gptkbp:variant
|
gptkb:Mi-28NM
gptkb:Mi-28N
gptkb:Mi-28NE
gptkb:Mi-28UB
|
gptkbp:bfsParent
|
gptkb:Russian_Aerospace_Forces
|
gptkbp:bfsLayer
|
5
|