Information AboutMig-17 |
| CATEGORIES ABOUT MIKOYAN-GUREVICH MIG-17 | |
| single engine aircraft | |
| jet aircraft | |
| soviet fighter aircraft 1950-1959 | |
| vietnam war aircraft | |
| SHOPPER'S DELIGHT | |
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markings.]] The Mikoyan-Gurevich MiG-17 (МиГ-17 in Cyrillic script) ( NATO Reporting Name '''Fresco''') is a Soviet jet Fighter Aircraft , in service from 1952 . DEVELOPMENT The MiG-17 design was generally based on a previous successful , 1950 . Second prototype variant SP-2 was an Interceptor , with a Radar . Despite the SI prototype crash on March 17, 1950, tests of other prototype '''SI-2''' and experimental series aircraft '''SI-02''' and '''SI-01''', in 1951, were generally successful, and on September 1, 1951 the aircraft was accepted for a production. It was estimated that with the same engine as MiG-15's, the MiG-17's maximum speed is higher by 40-50 km/h, and the fighter has greater maneuverability at high altitude. The serial production started in August 1951 . During production, the aircraft was improved and modified several times. The basic MiG-17 was a general purpose day-fighter, armed with 3 Cannon s, considered to be most effective in action against enemy aircraft. It could also act as a Fighter-bomber , but its Bomb load was considered light relative to other aircraft of the time, and it usually carried additional fuel tanks instead of bombs. Soon a number of MiG-17P all-weather fighters were produced with the Izumrud radar and front air intake modifications. In the spring of 1953 the '''MiG-17F''' day-fighter entered production. Fitted with the VK-1F engine with an Afterburner , which improved its performance, it became the most popular variant of the MiG-17. The next mass-produced variant with afterburner and radar was the '''MiG-17PF'''. In 1956 a small series (47 aircraft) was converted to '''MiG-17PM''' (also known as '''PFU''') with 4 first-generation air-to-air missiles K-5 (NATO: AA-1). A small series of '''MiG-17R''' reconnaissance aircraft were built with VK-1F engine (it was tested with VK-5F engine). Several thousand MiG-17s were built in the USSR by 1958 . LICENCE PRODUCTION In produced from 1960, Lim-6bis ''' produced from 1963 and ''' Lim-6M ''' (converted in the 1970s ) and reconnaissance variants: '''Lim-6R''' (Lim-6bisR) and '''MR'''. In China , first MiG-17F was assembled from parts in 1956, then in 1957 started licence production in Shenyang . The Chinese-built version is known as the Shenyang J-5 (for local use) or '''F-5''' (for export - not to be confused with the F-5 Freedom Fighter ). According to some sources, earlier MiG-17s, delivered from the USSR, were designated J-4. From 1964 , the Chinese produced variant with a radar, similar to the MiG-17PF, known as the '''J-5A''' (F-5A). The Chinese developed also two-seater Trainer variant '''JJ-5''' ('''FT-5''' for export), merging J-5 with cabin of the JJ-2 (licence-built MiG-15UTI). It was produced in 1966-1986, being the last produced MiG-17 variant and its only twin-seater variant. The Soviets did not produce a two-seat MiG-17, as they felt that the training variant of the older MiG-15 was sufficient. SERVICE The MiG-17 became a standard fighter in all Warsaw Pact countries in the late 1950s and early 1960s . They were also bought by numerous countries being under political influence of the USSR , and other, mainly Africa n and Asia n ones. MiG-17s were not available for the Korean War but saw considerable service as the main aircraft of the North Vietnamese Air Force during the Vietnam War , when it frequently worked in conjunction with MiG-21s ordinarily flown by Soviet or Chinese pilots. In fact, the pilots preferred the MiG-17 to the MiG-21 in that conflict as the MiG-17 was more agile, though not as fast as the MiG-21. They also flew against Israel in the various Arab-Israeli Conflict s. Twenty countries flew MiG-17's. APPLICATION The strategic purpose of this, and most other Soviet fighters, was to shoot down U.S. bombers, not engage in dogfights. This subsonic (.93 Mach) fighter was effective against slower (.6-.8 Mach), heavily loaded U.S. fighter-bombers. Even if the target had sufficient warning and time to shed external weight/drag and accelerate to supersonic escape speed, doing so would have inherently forced it to abort its bombing mission. VARIANTS
Among experimental variants there was an attack 'aircraft SN' of 1953, with central air intake replaced with two side intakes, and two 23 mm cannons mounted in a new nose, that could be swung down to shoot at ground targets. It was not produced. Some withdrawn aircraft were converted to remote controlled targets. DESCRIPTION Armament: Day-fighter variants (MiG-17, MiG-17F) were armed with two NR-23 23 mm cannons (80 rounds each) and one N-37 37 mm cannon (40 rounds), on a common bed under the central air intake. The gun bed could be easily wound down for maintenance. Variants with radar (MiG-17P, PF) were armed with three NR-23 23 mm cannons (100 rounds), due to radar weight. All variants could carry 100 kg bombs on two underwing pylons (some could cary 250 kg bombs), but usually they were used for 400 l fuel tanks. MiG-17R was armed with two 23 mm cannons. The only variant with air-to-air missiles was MiG-17PM (PFU), carrying 4 rockets K-5 (NATO: AA-1). It had no cannons. In different countries, MiG-17s were sometimes modified to carry unguided rockets or bombs on additional pylons. MiG-17P was equipped with Izumrud-1 (RP-1) radar, MiG-17PF with RP-1 or later with Izumrud-5 (RP-5) radar. MiG-17PM was also equipped with a radar, used to aim missiles. Other variants had no radar. __NOTOC__ SPECIFICATIONS (MIG-17F)
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