Statements (44)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
fighter aircraft airframe
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:designedFor |
supersonic flight
twin-engine configuration |
| gptkbp:emptyWeight |
13,757 kg
|
| gptkbp:feature |
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 |
| gptkbp:firstFlight |
1967
|
| gptkbp:height |
5.0 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
F-4E Phantom II airframe
|
| gptkbp:length |
19.2 meters
|
| gptkbp:manufacturer |
gptkb:McDonnell_Douglas
|
| gptkbp:material |
gptkb:steel
titanium aluminum alloy |
| gptkbp:maxTakeoffWeight |
28,030 kg
|
| gptkbp:predecessor |
gptkb:F-4C_Phantom_II
|
| gptkbp:role |
gptkb:aircraft
interceptor multirole fighter |
| gptkbp:successor |
F-15 Eagle
|
| gptkbp:usedBy |
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 |
| gptkbp:usedIn |
gptkb:McDonnell_Douglas_F-4E_Phantom_II
|
| gptkbp:wingspan |
11.7 meters
|
| gptkbp:bfsParent |
gptkb:RF-4E_Phantom_II
|
| gptkbp:bfsLayer |
7
|