|
gptkbp:instanceOf
|
fighter aircraft
|
|
gptkbp:aircraft
|
gptkb:delta_wing
second generation
single-engine
multirole fighter
conventional tail
Chengdu_J-7_family
|
|
gptkbp:armament
|
air-to-air missiles
1× 23 mm cannon
|
|
gptkbp:avionics
|
radar system
|
|
gptkbp:built
|
over 1,000
|
|
gptkbp:cockpit
|
tandem_seating
|
|
gptkbp:commissioningDate
|
1960s
|
|
gptkbp:constructionMaterial
|
aluminum alloy
|
|
gptkbp:crew
|
1
|
|
gptkbp:crew_size
|
K-36
|
|
gptkbp:engine
|
gptkb:WP-13_turbojet
|
|
gptkbp:exportedTo
|
gptkb:Bangladesh
gptkb:Myanmar
gptkb:Pakistan
gptkb:Sri_Lanka
|
|
gptkbp:firstFlight
|
1970
|
|
gptkbp:fuel_capacity
|
3,000 liters
|
|
gptkbp:hasExperienceIn
|
1,200 km
limited
|
|
gptkbp:height
|
4.80 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Chengdu J-7E
|
|
gptkbp:introduced
|
1980
|
|
gptkbp:is_used_in
|
gptkb:People's_Liberation_Army_Air_Force
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
14.93 m
|
|
gptkbp:manufacturer
|
gptkb:Chengdu_Aircraft_Industry_Group
|
|
gptkbp:maximum_speed
|
gptkb:Mach_2.0
|
|
gptkbp:maxTakeoffWeight
|
12,000 kg
14,000 kg
|
|
gptkbp:nickname
|
Fangyun
|
|
gptkbp:operational_status
|
limited
1970s to 2010s
|
|
gptkbp:operationalHistory
|
served in various conflicts.
|
|
gptkbp:operationalRange
|
2,000 km
|
|
gptkbp:produces
|
gptkb:Mikoyan-Gurevich_MiG-21
|
|
gptkbp:propulsion
|
50 kN
|
|
gptkbp:retired
|
2010s
|
|
gptkbp:role
|
ground attack
air superiority fighter
|
|
gptkbp:safety_features
|
limited
|
|
gptkbp:service_ceiling
|
17,000 m
|
|
gptkbp:successor
|
gptkb:Chengdu_J-10
|
|
gptkbp:supportRole
|
advanced training
|
|
gptkbp:surrounding_area
|
34.5 m²
|
|
gptkbp:takeoffDistance
|
250 km/h
300 km/h
|
|
gptkbp:team
|
gptkb:Chengdu_Aircraft_Design_Institute
|
|
gptkbp:variant
|
gptkb:Chengdu_J-7
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:wingspan
|
8.13 m
|