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gptkbp:instanceOf
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gptkb:fighter_aircraft_airframe
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gptkbp:countryOfOrigin
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gptkb:United_States
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gptkbp:designedFor
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supersonic flight
twin-engine configuration
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gptkbp:emptyWeight
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13,757 kg
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gptkbp:feature
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folding wingtips
reinforced landing gear
large fuel capacity
tailhook for carrier operations (not used in USAF F-4E)
airbrakes
canopy with good visibility
enlarged nose for radar and cannon
internal M61 Vulcan cannon housing
leading edge slats (late models)
multiple external stores pylons
provisions for electronic warfare pods
provisions for reconnaissance pods
two-seat tandem cockpit
ventral fin for stability
wing hardpoints
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gptkbp:firstFlight
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1967
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gptkbp:height
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5.0 meters
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gptkbp:length
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19.2 meters
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gptkbp:manufacturer
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gptkb:McDonnell_Douglas
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gptkbp:material
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gptkb:steel
gptkb:aluminum_alloy
titanium
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gptkbp:maxTakeoffWeight
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28,030 kg
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gptkbp:predecessor
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gptkb:F-4C_Phantom_II
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gptkbp:role
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gptkb:interceptor
gptkb:aircraft
multirole fighter
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gptkbp:successor
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F-15 Eagle
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gptkbp:usedBy
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gptkb:Iranian_Air_Force
gptkb:United_States_Air_Force
gptkb:Turkish_Air_Force
gptkb:Israeli_Air_Force
gptkb:South_Korean_Air_Force
gptkb:Hellenic_Air_Force
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gptkbp:usedIn
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gptkb:McDonnell_Douglas_F-4E_Phantom_II
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gptkbp:wingspan
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11.7 meters
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gptkbp:bfsParent
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gptkb:RF-4E_Phantom_II
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gptkbp:bfsLayer
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7
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https://www.w3.org/2000/01/rdf-schema#label
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F-4E Phantom II airframe
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