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gptkbp:instanceOf
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gptkb:aircraft
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|
gptkbp:armament
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gptkb:AIM-7_Sparrow
gptkb:AIM-9_Sidewinder
gptkb:M39_cannon
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|
gptkbp:avionics
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gptkb:General_Electric_AN/APG-67_radar
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|
gptkbp:crew
|
1
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gptkbp:developedBy
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gptkb:Northrop_F-5E_Tiger_II
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gptkbp:emptyWeight
|
6,577 kg
|
|
gptkbp:engineType
|
gptkb:General_Electric_F404_turbofan
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|
gptkbp:firstFlight
|
1982
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|
gptkbp:height
|
4.20 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Northrop F-20 Tigershark
|
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gptkbp:length
|
14.45 m
|
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gptkbp:manufacturer
|
gptkb:Northrop_Corporation
|
|
gptkbp:maximumSpeed
|
Mach 2.1
|
|
gptkbp:maxTakeoffWeight
|
11,340 kg
|
|
gptkbp:nickname
|
gptkb:Tigershark
|
|
gptkbp:notableFeature
|
single-engine design
advanced avionics for its time
|
|
gptkbp:numberBuilt
|
3
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:primaryUser
|
none (not adopted for service)
|
|
gptkbp:projectCancelled
|
1986
|
|
gptkbp:range
|
2,530 km
|
|
gptkbp:role
|
air superiority fighter
light fighter
|
|
gptkbp:serviceCeiling
|
16,800 m
|
|
gptkbp:status
|
gptkb:prototype
|
|
gptkbp:successor
|
gptkb:Northrop_F-5E_Tiger_II
|
|
gptkbp:targetMarket
|
export market
|
|
gptkbp:wingspan
|
8.13 m
|
|
gptkbp:bfsParent
|
gptkb:Northrop_Corporation
|
|
gptkbp:bfsLayer
|
6
|