Statements (60)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Mil_Mi-28
|
| gptkbp:armament |
30 mm cannon
ATG Ms |
| gptkbp:avionics |
digital flight control system
|
| gptkbp:combat_radius |
250 km
|
| gptkbp:countermeasures |
infrared jammers
|
| gptkbp:crew |
2
|
| gptkbp:engine |
T V3-117
|
| gptkbp:exported_to |
gptkb:Kazakhstan
gptkb:Politician gptkb:Venezuela |
| gptkbp:features |
enhanced situational awareness
modular design self-defense systems high maneuverability high agility improved fuel efficiency high thrust-to-weight ratio advanced avionics suite high altitude performance dual rotor system retractable landing gear enhanced firepower high survivability multi-role capability heavy payload capacity night vision capability reduced maintenance requirements fast deployment armored fuselage advanced targeting system low speed handling advanced weapon systems integration digital communications system tandem cockpit |
| gptkbp:first_flight |
gptkb:1982
|
| gptkbp:height |
4.7 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mi-28 A
|
| gptkbp:introduced |
gptkb:1996
|
| gptkbp:length |
17.3 m
|
| gptkbp:manufacturer |
gptkb:Moscow_Mil_Helicopter_Plant
|
| gptkbp:max_speed |
300 km/h
|
| gptkbp:max_takeoff_weight |
10,000 kg
|
| gptkbp:navigation_system |
gptkb:GPS
|
| gptkbp:nickname |
gptkb:Havoc
|
| gptkbp:notable_battle |
gptkb:Syrian_Civil_War
gptkb:Chechen_Wars |
| gptkbp:number_built |
over 100
|
| gptkbp:origin |
gptkb:Russia
|
| gptkbp:range |
450 km
|
| gptkbp:role |
close air support
anti-tank warfare |
| gptkbp:service_ceiling |
5,500 m
|
| gptkbp:services |
gptkb:1996
|
| gptkbp:stealth_features |
low radar cross-section
|
| gptkbp:variant |
gptkb:Mi-28_UB
gptkb:Mi-28_N |
| gptkbp:wingspan |
14.5 m
|