Mikojan/Gurevich MiG-15 :Fighter 1947 USSR

How to controll


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

SPECIFICATIONS:
Wingspan: 10.08m
length: 10.11m
height: 3.70m
empty mass: 3,580kg
start mass: 4,960kg
engine: Klimov VK-1 turbojet,(2,270kg)
max speed: 1,043km/h
initial climb: 50m/s
ceiling: 15,200m
range w/max.fuel: 1,420km
armament: 37mmMG X 1, 23mmMG X 2, 2x 100 kg (220 kg) bombs
Crew: 1
あまりにも有名な、旧共産圏を代表する戦闘機です。そしてこの機体からMiGの歴史は始まったと言えます。約15,000機あまり生産されたと見られており、朝鮮戦争やベトナム戦争に参戦しています。小型・軽量にデザインされており一撃離脱の戦法で西側諸国のパイロットを悩ませました。事実上昇力と速度はアメリカのFー86Fを上回っていました。
 
 
The Mikoyan-Gurevich MiG-15 (Russian: Микоян и Гуревич МиГ-15) (NATO reporting name "Fagot") was a jet fighter developed for the USSR. In March of 1946, Soviet leadership sought out a new swept-wing jet fighter from the leading aircraft design houses. The Mikoyan OKB's response was a design with the bureau designation I-310; a project that was influenced by plans for the Focke-Wulf Ta 183, which Soviet forces had captured when they overran Berlin in 1945. The I-310 first flew on the 30th December 1947. Previous Soviet designs like the MiG-9 had been hampered by the poor quality of available engines, but acquisition of the British Rolls-Royce Nene turbojet led to the development of an unauthorized local copy, the Klimov VK-1, which powered the I-310. MiG-15 undersideThe I-310 was a clean, swept-wing fighter with wings and tail swept at a 35° angle. Although it possessed a number of dangerous handling eccentricities (some of which were never really resolved), including pitch-up at transsonic speeds, it had exceptional performance, with a top speed of over 650 mph (1,040 km/h). The I-310's primary competitor was the similar Lavochkin La-168. After evaluations, the MiG design was chosen for production. Designated MiG-15, the first production example flew on 31 December 1948. It received the NATO reporting name "Fagot", entering Soviet air force service in 1949. An improved variant, the MiG-15bis ("bis" being Latin for "twice"), entered service in early 1950, with a number of changes intended to mitigate the aircraft's handling flaws.
 
 

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