Mi-25

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instance_of gptkb:helicopter
gptkbp:armament gptkb:Team_Rocket
gptkb:cannon
missiles
gptkbp:combat_experience gptkb:Ethiopian_Civil_War
gptkb:Soviet-Afghan_War
gptkb:Gulf_War
gptkb:Syrian_Civil_War
gptkb:Yugoslav_Wars
gptkb:Iran-Iraq_War
gptkb:Civil_War_in_Angola
gptkbp:crew 2
gptkbp:design_feature advanced avionics
high maneuverability
dual rotor system
twin-engine configuration
low maintenance requirements
high survivability
multi-role capability
high payload capacity
night vision capability
fast deployment
armor protection
versatile weapon systems
capable of aerial refueling
capable of operating in harsh environments
tandem cockpit
anti-tank capability
capable of carrying external fuel tanks
capable of deploying troops
gptkbp:engine TV3-117
gptkbp:first_flight gptkb:1976
gptkbp:height 4.5 m
https://www.w3.org/2000/01/rdf-schema#label Mi-25
gptkbp:length 16.5 m
gptkbp:manufacturer gptkb:Mil_Moscow_Helicopter_Plant
gptkbp:max_speed 300 km/h
gptkbp:max_takeoff_weight 10,500 kg
gptkbp:number_built over 1,000
gptkbp:range 450 km
gptkbp:role close air support
gptkbp:service_entry gptkb:1978
gptkbp:used_by gptkb:Afghanistan
gptkb:Angola
gptkb:Ethiopia
gptkb:India
gptkb:Soviet_Union
gptkb:Syria
gptkb:Iraq
gptkbp:variant gptkb:Mi-24
gptkb:Mi-35
gptkbp:weight 7,500 kg
gptkbp:bfsParent gptkb:Hind-D
gptkbp:bfsLayer 7