Tupolev Tu-128 :Interceptor 1961 USSR

How to controll


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

SPECIFICATIONS:
Wingspan: 18.10m
length: 27.20m
height: 7.00m
empty mass: 25,960kg
start mass: 40,000kg
engine: Lyulka AL-21F-3 turbojet, 10,790kgX2
max speed: 1,740 km/h
initial climb: 1125 m/s
ceiling: 18,000m
range w/max.fuel: 3,200km
armament: AAMX4 missiles
Crew: 2
世界最大の戦闘機といってもいいでしょう。中型爆撃機なみの大きさです。高空から進入する爆撃機を撃墜する目的で設計され、全天候能力を持ち武装も対空ミサイルのみです。運動性はその機体の大きさから軽快ではなく、ミサイルキャリアーとしての使用を前提とされていました。通常は赤外線誘導とレーダー誘導の対空ミサイルを各2発づつ装備します。
ミサイル / 爆弾
ビスノバR−4R
空対空ミサイル
2発
and
ビスノバR−4T
空対空ミサイル
2〜4発
 
The Tupolev Tu-28 (NATO reporting name 'Fiddler') was developed by the Soviet Union in the 1960s as a long-range interceptor aircraft. Also known as the Tu-128, it remains the world's largest fighter aircraft.In 1955 the PVO issued a specification for a long-range interceptor aircraft to defend the vast territory of the Soviet Union, which was so extensive that even with a far richer economy it would have been impossible to provide comprehensive air defense. To provide the necessary range and ability to carry a powerful radar and air-to-air missiles, Tupolev developed an aircraft similar to the Tu-105 (Tu-22) bomber. The Tu-102 development aircraft first flew in 1959, with the initial operational version, the Tu-28P ('Fiddler-A'), entering production in 1963. This was replaced in production by the definitive Tu-128 ('Fiddler-B'). Based, like the Tu-22 bomber, on the unsuccessful Tu-98 supersonic bomber, it had a broad, low/mid-mounted swept wing carrying the main landing gear in wing-mounted pods, and slab tailplanes. Two Lyulka AL-21F-3 turbojet engines were mounted in the fuselage. Unlike the Tu-22, there is no internal weapon bay. Weapons were carried on wing pylons, with the fuselage used for enormous fuel tanks. The Tu-28P seated two crew in tandem, with separate canopies.
Missile and Bomb

Bisnovat R-4R

antiaircraft missile

X 2
and
antiaircraft missile
X 2
 

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