The Lavochkin La-7 (Russian: Лавочкин Ла-7; NATO reporting name: Fin)[2] is a piston-engined single-seat Soviet fighter aircraft developed during World War II by the Lavochkin Design Bureau. It was a development and refinement of the Lavochkin La-5, and the last in a family of aircraft that had begun with the LaGG-1 in 1938. Its first flight was in early 1944 and it entered service with the Soviet Air Forces later in the year. A small batch of La-7s was given to the Czechoslovak Air Force the following year, but it was otherwise not exported. Armed with two or three 20 mm (0.8 in) cannon, it had a top speed of 661 kilometers per hour (411 mph). The La-7 was felt by its pilots to be at least the equal of any German piston-engined fighter. It was phased out in 1947 by the Soviet Air Force, but served until 1950 with the Czechoslovak Air Force.
Specifications
General Characteristics
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- Wingspan 32.7ft (10.0m)
- Length 27.9ft (8.5m)
- Height 10.9ft (3.3m)
- Empty Weight N/A
- Loaded Weight 6,289lbs (2,852kg)
Performance
- Horse Power/Weight Ratio 0.311
- Wing Loading 18.5lbs/ft2 (90.4kg/m2)
- Wing Area 339.7ft2 (31.6m2)
- Drag Points 2720
Parts
- Number of Parts 106
- Control Surfaces 9
- Performance Cost 583
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