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gptkbp:instanceOf
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fighter aircraft
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gptkbp:aircraft
|
gptkb:Chengdu_J-7
twin-engine
second generation
mid-wing
multi-role fighter
J-8 family
J-8V-1, J-8V-2
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|
gptkbp:armament
|
air-to-air missiles
|
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gptkbp:avionics
|
radar system
|
|
gptkbp:built
|
approximately 200
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|
gptkbp:climbRate
|
250 m/s
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:constructionMaterial
|
aluminum alloy
|
|
gptkbp:countermeasures
|
chaff and flare dispensers
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|
gptkbp:crew
|
1
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|
gptkbp:decommissioned
|
2015
|
|
gptkbp:design_feature
|
gptkb:delta_wing
|
|
gptkbp:engine
|
gptkb:WP-13_turbojet
|
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gptkbp:engineType
|
afterburning turbojet
|
|
gptkbp:exportedTo
|
nan
|
|
gptkbp:firstFlight
|
1980
|
|
gptkbp:fuel_capacity
|
3,000 liters
|
|
gptkbp:hasExperienceIn
|
1,200 km
limited
|
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gptkbp:height
|
4.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Chengdu J-8V
|
|
gptkbp:inspiration
|
gptkb:Mikoyan_MiG-21
|
|
gptkbp:introduced
|
1985
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
15.76 m
|
|
gptkbp:manufacturer
|
gptkb:Chengdu_Aircraft_Industry_Group
|
|
gptkbp:maximum_speed
|
Mach_2.5
|
|
gptkbp:maxTakeoffWeight
|
15,000 kg
|
|
gptkbp:missileSystem
|
PL-8,_PL-11
|
|
gptkbp:modifications
|
upgraded avionics
|
|
gptkbp:nickname
|
None known
|
|
gptkbp:operationalHistory
|
served in various conflicts
|
|
gptkbp:operationalRange
|
2,000 km
|
|
gptkbp:origin
|
gptkb:China
|
|
gptkbp:primaryUser
|
gptkb:China
|
|
gptkbp:radar
|
pulse-Doppler radar
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:retirementYear
|
2010s
|
|
gptkbp:role
|
interceptor
fighter-interceptor
|
|
gptkbp:safety_features
|
limited stealth capabilities
|
|
gptkbp:service_ceiling
|
18,000 m
|
|
gptkbp:services
|
gptkb:People's_Liberation_Army_Air_Force
|
|
gptkbp:succeededBy
|
20°/s
|
|
gptkbp:successor
|
gptkb:Chengdu_J-10
|
|
gptkbp:supportRole
|
used for pilot training
|
|
gptkbp:surrounding_area
|
34 m²
|
|
gptkbp:team
|
gptkb:Chengdu_Aircraft_Design_Institute
air superiority
|
|
gptkbp:variant
|
J-8II
|
|
gptkbp:wingspan
|
9.6 m
|