Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
military aircraft
|
| gptkbp:aircraft |
high maneuverability
single-engine fly-by-wire system multirole aircraft military trainer jet trainer dual control system ground attack capabilities twin-seat configuration joint_development_with_Pakistan produced_in_China K-8E,_K-8W K-8_family |
| gptkbp:armament |
machine guns
|
| gptkbp:avionics |
modern avionics system
|
| gptkbp:cockpit |
glass cockpit
|
| gptkbp:crew |
2
|
| gptkbp:design |
gptkb:Hongdu
twin-engine |
| gptkbp:design_feature |
low-wing monoplane
|
| gptkbp:engine |
1
|
| gptkbp:engineType |
turbofan engine
|
| gptkbp:exportedTo |
gptkb:Bangladesh
gptkb:Myanmar gptkb:Zimbabwe |
| gptkbp:firstFlight |
1990
|
| gptkbp:fuel_capacity |
1,200 liters
|
| gptkbp:height |
4.8 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
K-8E Karakorum
|
| gptkbp:IATA_code |
developed in the 1980s
in service since 1990s |
| gptkbp:introduced |
1990s
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
12.5 m
|
| gptkbp:manufacturer |
gptkb:Hongdu_Aviation_Industry_Group
|
| gptkbp:maximum_speed |
1,050 km/h
|
| gptkbp:maxTakeoffWeight |
3,600 kg
|
| gptkbp:missions |
training and light attack
training and reconnaissance |
| gptkbp:operational_status |
gptkb:China
1990s |
| gptkbp:primaryUser |
gptkb:Pakistan_Air_Force
gptkb:People's_Liberation_Army_Air_Force |
| gptkbp:range |
1,500 km
|
| gptkbp:role |
trainer aircraft
light attack aircraft |
| gptkbp:service_ceiling |
10,000 m
|
| gptkbp:successor |
K-8W
|
| gptkbp:supportRole |
pilot training
light attack missions |
| gptkbp:tourism |
upgraded avionics
|
| gptkbp:training |
advanced training
|
| gptkbp:variant |
K-8
|
| gptkbp:wingspan |
12.3 m
|