McDonnell Douglas F-4 Phantom II :Fighter 1958 U.S.NAVY

How to controll


H:heading C:reset
P:pitching 1:stereo on
R:rolling 2:stereo off

SPECIFICATIONS: E
Wingspan: 11.71m
length: 17.76m
height: 4.96m
empty mass: 12,700kg
start mass: 24,770kg
engine: GE.J79-GE-10 (AB8,120kg)X2
max speed: M2.2
initial climb: 12,375m/min
ceiling: 16.675m
range w/max.fuel: 2,815km
armament: 1x 20 mm M61 Vulcan,
AIM-7Sparrow X 4,
AIM-9Sidewinder X 4, bombs 7,260kg
Crew: 2
アメリカ海軍・空軍で採用されるという名誉を担った20世紀を代表する戦闘機です。 F101の設計思想を発展させ十分な胴体内スペースを確保しでより多くの燃料を搭載でき、また胴体下にミサイルを直接搭載できるようにするなど近代戦闘機のお手本のような機体です。対空戦闘から地上攻撃まで多くのミッションをこなせる万能機でもあります。日本の自衛隊の主力戦闘機としても採用されています。
ミサイル / 爆弾

AIM7スパロー

空対空ミサイル
4発

AIM9
サイドワインダー

空対空ミサイル
4発
 
The McDonnell Douglas F-4 Phantom II[2] was a two-seat supersonic long-range all-weather fighter-bomber produced for the United States military by McDonnell Douglas. Entering service in 1960, the F-4 was designed as the first modern fleet defense fighter for the United States Navy. By 1963, it was adopted by the United States Air Force for the fighter-bomber role. When production ended in 1981, 5,195 Phantom IIs had been built, making it the most numerous American supersonic military aircraft. Until the advent of the F-15 Eagle, the F-4 also held a record for the longest continuous production with a run of 24 years. Innovations in the F-4 included an advanced pulse-doppler radar and extensive use of titanium in the airframe.
Missile and Bomb

AIM-7 Sparrow

antiaircraft missile

X 4

AIM-9 Sidewinders

antiaircraft missile

X 4

 

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