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[[Gambar:McDONNELL DOUGLAS F-4 PHANTOM II.png|right|300px|Orthographically projected diagram of the F-4B Phantom II.]]
==Karakteristik umum==
{{aircraft specifications
|jet or prop?=jet
|plane or copter?=plane
*Kru: 2
|ref=The Great Book of Fighters,
|length*Dawa: main=63 ft 0 in ▼|span*Amba swisi: main=38 ft 4.5 in ▼|height*Duwur: main=16 ft 6 in ▼*Gedhi swiwi: 530.0 ft²
|airfoil=*Airfoil: NACA airfoil 0006.4-64 root, NACA 0003-64 tip ▼*Bobot kosong: 30,328 lb
*Bobot isi: 41,500 lb
*Bobot maksimum lepas landas: 61,795 lb
*Mesin: 2× General Electric J79-GE-17A axial compressor turbojet, 17,845 lbf masing-masing
* '''[[Zero-lift drag coefficient ]]: ''' 0.0224 ▼* '''[[Zero-lift drag coefficient|Drag area: ]]''' 11.87 ft² (1.10 m²) ▼*Aspect ratio: 2.77
*Fuel capacity: 1,994 US gal (7,549 L) internal, 3,335 US gal (12,627 L) with three external tanks
* '''Maximum landing weight: ''' 36,831 lb (16,706 kg) ▼
===Kinerja===
<!-- please include units. if something doesn't apply, leave it blank. -->
<!-- to add more specificatins, end the alt specs line with a right parenthesis ")" and start a new, fully-formatted line beginning with an asterisk "*" -->
|crew=2
|capacity=
|length alt=19.2 m
|span alt=11.7 m
|height alt=5.0 m
|area main=530.0 ft²
|area alt=49.2 m²
▲|airfoil=NACA airfoil 0006.4-64 root, NACA 0003-64 tip
|empty weight main=30,328 lb
|empty weight alt=13,757 kg
|loaded weight main=41,500 lb
|loaded weight alt=18,825 kg
|useful load main=<!-- lb-->
|useful load alt=<!-- kg-->
|max takeoff weight main=61,795 lb
|max takeoff weight alt=28,030 kg
|more general=
▲* '''[[Zero-lift drag coefficient]]:''' 0.0224
▲* '''[[Zero-lift drag coefficient|Drag area:]]''' 11.87 ft² (1.10 m²)
* '''[[Aspect ratio (wing)|Aspect ratio]]:''' 2.77
* '''Fuel capacity:''' 1,994 US gal (7,549 L) internal, 3,335 US gal (12,627 L) with three external tanks<!--External fuel tanks of 370 US gal (1,420 l) capacity for the outer wing hardpoints and either a 600 or 610 US gal (2,310 or 2,345 l) fuel tank for the centerline station can be fitted to extend the range.--> ▼▲* '''Maximum landing weight:''' 36,831 lb (16,706 kg)
*Laju maksimum: Mach number 2.23 (1,472 mph, 2,370 km/h) at 40,000 ft (12,190 m)
|engine (jet)=General Electric J79-GE-17A
|cruise*Laju speedjelajah: alt=506 knots (585 mph, 940 km/h )▼|type of jet=axial compressor [[turbojet]]
*Radius tempur: 367 nm
|number of jets=2
|ferry*Jarak rangejangkau ferri: 1,403 nm more=with 3 external fuel tanks ▼|thrust main=17,845 lbf
*Batas keduwuran servis: 60,000 ft
|thrust alt=79.6 kN
|climb*Laju ratepanjat: main=41,300 ft/min ▼*Beban swiwi: 78 lb/ft²
*Dorongan/bobot: 0.86
* '''[[Lift-to-drag ratio ]]: ''' 8.58 ▼* '''Takeoff roll: ''' 4,490 ft (1,370 m) at 53,814 lb (24,410 kg) ▼* '''Landing roll: ''' 3,680 ft (1,120 m) at 36,831 lb (16,706 kg) ▼
===Persenjataan===
|max speed main=Mach number 2.23
|max speed alt=1,472 mph, 2,370 km/h
|max speed more=at 40,000 ft (12,190 m)
|cruise speed main=506 knots
▲|cruise speed alt=585 mph, 940 km/h
|combat radius main=367 nm
|combat radius alt=422 mi, 680 km
|ferry range main=1,403 nm
|ferry range alt=1,615 mi, 2,600 km
▲|ferry range more=with 3 external fuel tanks
|ceiling main=60,000 ft
|ceiling alt=18,300 m
▲|climb rate main=41,300 ft/min
|climb rate alt=210 m/s
|loading main=78 lb/ft²
|loading alt=383 kg/m²
|thrust/weight=0.86
|more performance=
▲* '''[[Lift-to-drag ratio]]:''' 8.58
▲* '''Takeoff roll:''' 4,490 ft (1,370 m) at 53,814 lb (24,410 kg)
▲* '''Landing roll:''' 3,680 ft (1,120 m) at 36,831 lb (16,706 kg)
* 1x 20 mm M61 Vulcan gatling cannon, 639 rounds ▼|armament=
▲*Up '''Fuelto capacity:''' 118, 994650 US gallb ( 78, 549480 Lkg) internalof weapons on nine external hardpoints, 3including general purpose bombs, 335 UScluster galbombs, (12TV- and laser-guided bombs, 627 L)rocket withpods, threeair-to-ground externalmissiles, tanks<!anti- runway weapons, anti- ship missiles, targeting pods, recce pods, and nuclear weapons. Baggage pods may also be carried. External fuel tanks of 370 US gal (1,420 l) capacity for the outer wing hardpoints and either a 600 or 610 US gal (2,310 or 2,345 l) fuel tank for the centerline station can be fitted to extend the range. -->
▲* 1x 20 mm M61 Vulcan gatling cannon, 639 rounds
* 4x [[AIM-7 Sparrow ]] in fuselage recesses plus 4x [[AIM-9 Sidewinder]]sSidewinders on wing pylons; upgraded Hellenic F-4E and German F-4F ICE carry AIM-120 AMRAAM, Japanese F-4EJ Kai carry Mitsubishi AAM-3, Hellenic F-4E will carry IRIS-T in future. Iranian F-4s could potentially carry Russian and Red Chinese missiles. UK Phantoms eventually (1978) replaced the AIM-7 Sparrow with [[Skyflash ]] missiles .▼* Up to 18,650 lb (8,480 kg) of weapons on nine external hardpoints, including general purpose bombs, cluster bombs, TV- and laser-guided bombs, rocket pods, air-to-ground missiles, anti-runway weapons, anti-ship missiles, targeting pods, recce pods, and nuclear weapons. Baggage pods may also be carried. External fuel tanks of 370 US gal (1,420 l) capacity for the outer wing hardpoints and either a 600 or 610 US gal (2,310 or 2,345 l) fuel tank for the centerline station can be fitted to extend the range.
▲* 4x [[AIM-7 Sparrow]] in fuselage recesses plus 4x [[AIM-9 Sidewinder]]s on wing pylons; upgraded Hellenic F-4E and German F-4F ICE carry AIM-120 AMRAAM, Japanese F-4EJ Kai carry Mitsubishi AAM-3, Hellenic F-4E will carry IRIS-T in future. Iranian F-4s could potentially carry Russian and Red Chinese missiles. UK Phantoms eventually (1978) replaced the AIM-7 Sparrow with [[Skyflash]] missiles.
}}
== Referensi ==
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