F-4 Phantom II
USAF F-4E dari 347th Tactical Fighter Wing menjatuhkan bom 500-pon Mark 82.
Tipe	Pesawat tempur pengebom
Produsen	McDonnell Douglas (McDonnell Aircraft)
Perancang	David S. Lewis, Jr.
Pisanan mabur	27 May 1958
Status	1.100 aktif sebagai drone di AS dan aktif di luar AS
Pemakai	Amérika Sarékat Iran Israèl
Diproduksi	1958-1981
Cacah digawé	5.195
Rega satuan	2,4 juta dolar AS ketika baru (F-4E)

F-4 Phantom II ya iku pesawat tempur pengebom buatan Amérika Sarékat. Pesawat iki ukurane gedhé, bermesin ganda lan mligi digunakaké déning Angkatan Udara Amérika Sarékat, Angkatan Laut Amérika Sarékat, sarta Korps Marikir Amérika Sarékat. nalika iki F-4 wis pensiun ing Amérika Sarékat, nanging isih aktif ing pira-pira nagara saliyané Amérika serikat, kaya ing Iran lan Israèl. Nganti taun 2001 isih ana 1000 pesawat jinis iki kaya kang digunakaké ing 11 nagara.^[1]

QF-4 Phantom 74-626 di McGuire Air Force Base, 12 Mèi 2007. A-10 Thunderbolt II dilatar belakang.

F-4 USAF nibakake 107½ MiG Asia Tenggara (50 kanti Sparrow, 31 kanti Sidewinder, 5 kanti Falcon, 15.5 kanti senapan mesin, lan 6 senjata liyané:

Aircraft	Weapons/Tactics	MiG-17	MiG-19	MiG-21	Total
F-4C	AIM-7 Sparrow	4	0	10	14
	AIM-9 Sidewinder	12	0	10	22
	20 mm gun	3	0	1	4
	Maneuvering tactics	2	0	0	2
F-4D	AIM-4 Falcon	4	0	1	5
	AIM-7 Sparrow	4	2	20	26
	AIM-9 Sidewinder	0	2	3	5
	20 mm gun	4.5	0	2	6
	Maneuvering tactics	0	0	2	2
F-4E	AIM-7 Sparrow	0	2	8	10
	AIM-9 Sidewinder	0	0	4	4
	AIM-9+20 mm gun	0	0	1	1
	20 mm gun	0	1	4	5
	Maneuvering tactics	0	1	0	1
Total		33.5	8	66	107.5

Spesifikasi (F-4E)

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Karakteristik umum

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Kru: 2
Dawa: 63 ft 0 in
Amba swisi: 38 ft 4.5 in
Duwur: 16 ft 6 in
Gedhi swiwi: 530.0 ft²
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
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)^[2]

Kinerja

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Laju maksimum: Mach number 2.23 (1,472 mph, 2,370 km/h) at 40,000 ft (12,190 m)
Laju jelajah: 506 knots (585 mph, 940 km/h)
Radius tempur: 367 nm
Jarak jangkau ferri: 1,403 nm with 3 external fuel tanks
Batas keduwuran servis: 60,000 ft
Laju panjat: 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

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1x 20 mm M61 Vulcan gatling cannon, 639 rounds
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 Sidewinders 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

Cathetan sikil

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↑ Pesawat-tempur, (Kaunduh 21/12/12).
↑ Green and Swanborough 2001.

Delang Uga

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Wikimedia Commons duwé médhia ngenani F-4 Phantom II.

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