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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
4
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gptkbp:bfsParent
|
gptkb:The_F5
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gptkbp:aircraft_operated
|
twin-engine
low-wing
supersonic aircraft
lightweight fighter
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|
gptkbp:allows
|
+8/-3 g
|
|
gptkbp:armament
|
gptkb:Baron
gptkb:rocket
air-to-air missiles
|
|
gptkbp:avionics
|
modernized systems in some variants
|
|
gptkbp:cockpit
|
dual control
|
|
gptkbp:combat_radius
|
1,200 km
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
in some air forces
|
|
gptkbp:design
|
gptkb:Northrop_F-5_family
|
|
gptkbp:engine
|
gptkb:General_Electric_J85
|
|
gptkbp:exported_to
|
many countries
|
|
gptkbp:first_flight
|
gptkb:1972
still in service with some operators
|
|
gptkbp:fuel_capacity
|
2,500 liters
|
|
gptkbp:height
|
4.3 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F-5 F Tiger II
|
|
gptkbp:introduced
|
gptkb:1972
|
|
gptkbp:is_used_by
|
gptkb:aircraft
gptkb:Royal_Canadian_Air_Force
gptkb:Swiss_Air_Force
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
14.3 m
|
|
gptkbp:manufacturer
|
gptkb:Northrop
|
|
gptkbp:material
|
aluminum
|
|
gptkbp:max_speed
|
1,065 km/h
|
|
gptkbp:max_takeoff_weight
|
10,000 kg
|
|
gptkbp:nickname
|
gptkb:Tiger_II
|
|
gptkbp:notable_battle
|
various conflicts
|
|
gptkbp:number_built
|
approximately 1,000
|
|
gptkbp:operational_history
|
used in various air forces worldwide
|
|
gptkbp:range
|
2,300 km
|
|
gptkbp:retired
|
various dates by different operators
|
|
gptkbp:role
|
gptkb:aircraft
multirole fighter
|
|
gptkbp:roll_rate
|
30°/s
|
|
gptkbp:service_ceiling
|
15,240 m
|
|
gptkbp:services
|
gptkb:1972
|
|
gptkbp:stealth_features
|
limited stealth capabilities
|
|
gptkbp:successor
|
gptkb:F-5_E_Tiger_II
|
|
gptkbp:training
|
advanced jet training
|
|
gptkbp:variant
|
gptkb:F-5_Freedom_Fighter
|
|
gptkbp:weight
|
5,500 kg
|
|
gptkbp:wing_area
|
27.9 m²
|
|
gptkbp:wingspan
|
8.2 m
|