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gptkbp:instanceOf
|
fighter aircraft
|
|
gptkbp:aircraft
|
limited
single-engine
|
|
gptkbp:armament
|
gptkb:YJ-83_anti-ship_missile
gptkb:PL-8_air-to-air_missile
GBU-12 Paveway II
PL-12 air-to-air missile
|
|
gptkbp:avionics
|
digital fly-by-wire system
active electronically scanned array radar
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:colors
|
low observable paint
|
|
gptkbp:constructionMaterial
|
composite materials
|
|
gptkbp:countermeasures
|
electronic warfare systems
|
|
gptkbp:crew
|
1
|
|
gptkbp:crew_size
|
Z-10 ejection seat
|
|
gptkbp:debutYear
|
2006
|
|
gptkbp:design
|
gptkb:canard-delta_wing_configuration
|
|
gptkbp:developer
|
Chinese_military_aviation_program
|
|
gptkbp:engine
|
gptkb:WS-10A_Taihang
|
|
gptkbp:exportedTo
|
gptkb:Pakistan
|
|
gptkbp:firstFlight
|
March 23, 1998
|
|
gptkbp:hasExperienceIn
|
1,200 km
used in various military exercises
|
|
gptkbp:height
|
4.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shenyang J-10
|
|
gptkbp:influenced
|
gptkb:Israeli_Lavi
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
14.3 m
|
|
gptkbp:manufacturer
|
gptkb:Shenyang_Aircraft_Corporation
|
|
gptkbp:maximum_speed
|
2,400 km/h
|
|
gptkbp:militaryService
|
gptkb:People's_Liberation_Army
|
|
gptkbp:nickname
|
Vigorous Dragon
|
|
gptkbp:operational_status
|
yes
over 10 years
|
|
gptkbp:operationalRange
|
1,500 km with air-to-air refueling
|
|
gptkbp:productionYears
|
1998-2006
|
|
gptkbp:range
|
3,100 km
|
|
gptkbp:role
|
multirole fighter
|
|
gptkbp:safety_features
|
reduced radar cross-section
|
|
gptkbp:service_ceiling
|
16,000 m
|
|
gptkbp:services
|
gptkb:People's_Liberation_Army_Air_Force
|
|
gptkbp:successor
|
gptkb:Shenyang_FC-31
|
|
gptkbp:team
|
gptkb:Shenyang_Aircraft_Design_Institute
air defense
|
|
gptkbp:trainTypes
|
J-10S
|
|
gptkbp:variant
|
J-10A
J-10B
J-10C
|
|
gptkbp:weight
|
3,000 kg
8,000 kg empty
12,000 kg maximum takeoff
|
|
gptkbp:wingspan
|
9.75 m
|