Bell P-39 Aircobra :Fighter 1938 USAAF

How to controll


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

SPECIFICATIONS:
Wingspan: 10.40m
length: 9.20m
height: 3.60m
empty mass: 2,560kg
start mass: 3,722kg
engine: AllisonV-1710-35 liquid-cooled V12-cylinder(1,150hp)
max speed: 596km/h
initial climb: 802m/min
ceiling: 9,790m
range w/max.fuel: 1,288km
armament: 7.7mmMGX4, 12.7mmMGX2, 37mmMGX1
Crew: 1
自動車で言えばミッドシップ(車体中央にエンジンを搭載する)タイプ、その理由は機体中心線上に大口径機関砲を搭載するためでした。プロペラシャフトから37mm機関砲を発射でき、対戦車攻撃などでは非常に有効な武器となります。しかしその性能から空戦では日本のゼロ戦には歯がたたずソ連に供給されソビエト軍で活躍しました。
 
 
The Bell P-39 Airacobra was one of the principal fighter aircraft in service with American forces at the start of World War II. (The P-39 was at first for a short time designated XP-45.) The aircraft's unusual design featured its Allison engine mounted in the middle of the fuselage, just behind the pilot, driving the propeller through a driveshaft passing between the pilot's feet. The purpose of this was to free up space for the heavy main armament, a 37 mm T9 cannon firing through the center of the propeller hub for optimum accuracy and stability when firing. The weight distribution necessitated a tricycle undercarriage, a first among American fighters. Entry to the cockpit was through a side door rather than a moving canopy. The weight distribution of the P-39 supposedly is the reason for its tendency to enter a dangerous flat spin ? a characteristic Soviet tests proved to the then-skeptical manufacturer who had been unable to reproduce them.
 
 

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