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https://en.wikipedia.org/wiki/Lavochkin_La-7
The Lavochkin La-7 (Russian: ???????? ??-7) was a piston-engined Soviet fighter developed during World War II by the Lavochkin Design Bureau (OKB). 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 (0.79 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. By 1943, the La-5 had become a mainstay of the Soviet Air Forces, yet both its head designer, Semyon Lavochkin, as well as the engineers at the Central Aerohydrodynamics Institute (Russian: TsAGI), felt that it could be improved upon. TsAGI refined earlier studies of aerodynamic improvements to the La-5 airframe in mid-1943 and modified La-5FN c/n 39210206 to evaluate the changes. These included complete sealing of the engine cowling, rearrangement of the wing center section to accommodate the oil cooler and the relocation of the engine air intake from the top of the cowling to the bottom to improve the pilot's view. Combat trials began in mid-September 1944 and were generally very positive. However four aircraft were lost to engine failures and the engines suffered from numerous lesser problems, despite its satisfactory service in the La-5FN. One cause was the lower position of the engine air intakes in the wing roots of the La-7 which caused the engine to ingest sand and dust. One batch of flawed wings was built and caused six accidents, four of them fatal, in October which caused the fighter to be grounded until the cause was determined to be a defect in the wing spar. Production of the first aircraft fitted with three B-20 cannon began in January 1945 when 74 were delivered. These aircraft were 65 kilograms (143 lb) heavier than those aircraft with the two ShVAK guns, but the level speed was slightly improved over the original aircraft. However, the time to climb to 5000 meters increased by two-tenths of a second over the older model. More than 2000 aircraft were delivered before the war's end, most by Zavod Nr. 21. A total of 5753 aircraft had been built by Zavod Nr. 21, Nr. 381, and Nr. 99 in Ulan-Ude, when production ended in early 1946. Role Fighter Manufacturer Lavochkin OKB First flight February 1944 Introduction 1944 Retired 1950 Primary users Soviet Air Forces Czechoslovak Air Force Number built 5,753 Developed from Lavochkin La-5 The 63rd Guard Fighter Aviation Corps began combat trials of the La-7 in mid-September 1944 in support of the 1st Baltic Front. Thirty aircraft were provided for the trials, which lasted one month. During this time the new fighters made 462 individual sorties and claimed 55 aerial victories while losing four aircraft in combat. Four other La-7s were lost to non-combat causes, mostly related to engine problems. A total of three pilots were killed during the trials to all causes. The British test pilot, Eric "Winkle" Brown was given the chance to fly an La-7 at the former Erprobungsstelle Tarnewitz Luftwaffe aircraft test station on the Baltic coast, shortly after the German surrender in May 1945. He described the handling and performance as "quite superb", but the armament and sights were "below par", the "wooden construction would have withstood little combat punishment" and the instrumentation was "appallingly basic". Production of the La-7 amounted to 5,753 aircraft, plus 584 La-7UTI trainers. Those aircraft still in service after the end of the war were given the NATO reporting name Fin. The follow-up model, the La-9, despite its outward similarity, was a completely new design. Tactical significance The La-7 ended the superiority in vertical maneuverability that the Messerschmitt Bf 109G had previously enjoyed over other Soviet fighters. Furthermore, it was fast enough at low altitudes to catch, albeit with some difficulties, Focke Wulf Fw 190 fighter-bombers that attacked Soviet units on the frontlines and immediately returned to German-controlled airspace at full speed. The Yakovlev Yak-3 and the Yakovlev Yak-9U with the Klimov VK-107 engine lacked a large enough margin of speed to overtake the German raiders. 115 La-7s were lost in air combat, only half the number of Yak-3s. Specifications (1945 production model) General characteristics Crew: 1 Length: 8.6 m (28 ft 3 in) Wingspan: 9.8 m (32 ft 2 in) Height: 2.54 m (8 ft 4 in) Wing area: 17.59 m2 (189.3 sq ft) Empty weight: 2,638 kg (5,816 lb) Gross weight: 3,315 kg (7,308 lb) Powerplant: 1 × Shvetsov ASh-82FN 14-cylinder, two-row, air-cooled radial, 1,380 kW (1,850 hp) Propellers: 3-bladed VISh-105V-4 Performance Maximum speed: 661 km/h (411 mph; 357 kn) at 6,000 meters (19,685 ft) Range: 665 km (413 mi; 359 nmi) (1944 model) Service ceiling: 10,450 m (34,280 ft) Rate of climb: 15.72 m/s (3,095 ft/min) Time to altitude: 5.3 minutes to 5,000 meters (16,404 ft) Armament Guns: 2 × cowl-mounted 20 mm ShVAK cannons with 200 rounds per gun or 3 × cowl-mounted 20 mm Berezin B-20 cannons with 100 rounds per gun Bombs: 200 kg (440 lb) of bombs * |
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