MiG-17 "Fresco" @·AIRCRAFTUBE

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Mikoyan-Gurevich MiG-17 ''Fresco''

The Mikoyan-Gurevich MiG-17 (NATO reporting name : Fresco) (China :Shenyang J-5) (Poland : PZL-Mielec Lim-6) is a high-subsonic fighter aircraft produced in the USSR from 1952 and operated by numerous air forces in many variants. It is an advanced development of the very similar appearing MiG-15 of the Korean War.

The MiG-17 first saw combat in 1958 over the Straits of Taiwan and was used as an effective threat against supersonic fighters of the United States in the Vietnam War. It was also briefly known as the "Type 38", by U.S. Air Force designation prior to the development of NATO codes.

Development

While the MiG-15bis would be destined to introduce swept wings to air combat over Korea, by 1949, the Mikoyan-Gurevich design bureau had already begun work on its replacement, originally the MiG-15bis45, which would fix any problems found with the MiG-15 in combat. The result was one of the most successful transonic fighters introduced before the advent of true supersonic types such as the Mikoyan-Gurevich MiG-19 and North American F-100 Super Sabre. The design would ultimately still prove effective into the 1960s when pressed into dogfights over Vietnam against supersonic types which were generally flown at subsonic speeds, and not optimized for subsonic maneuvering short-range engagements.

While the MiG-15 used a Mach sensor to deploy airbrakes because it could not safely exceed Mach 0.92, the MiG-17 was designed to be controllable at higher Mach numbers. Early versions which retained the original Soviet copy of the Rolls-Royce Nene VK-1 engine were heavier with equal thrust. Later MiG-17s would be the first Soviet fighter application of an afterburner which offered increased thrust on demand by dumping fuel in the exhaust of the basic engine.

Though the MiG-17 still strongly resembles its forebear, it had an entirely new thinner and more highly swept wing and tailplane for speeds approaching Mach 1. While the F-86 introduced the "all-flying" tailplane which helped controllability near the speed of sound, this would not be adopted on MiGs until the fully supersonic MiG-19. The wing had a "sickle sweep" compound shape with a 45° angle like the U.S. F-100 Super Sabre near the fuselage (and tailplane), and a 42° angle for the outboard part of the wings. The stiffer wing resisted the tendency to bend its wingtips and lose aerodynamic symmetry unexpectedly at high speeds and wing loads.

Other easily visible differences to its predecessor were the three wing-fences on each wing, instead of the MiG-15's two, the addition of a ventral fin and a longer and less tapered rear fuselage that added about 3 feet in length. The MiG-17 shared the same Klimov VK-1 engine and much of the rest of its construction such as the forward fuselage, landing gear and gun installation was carried over. The first prototype, designated I-330 "SI" by the construction bureau, was flown on the 14 January 1950, piloted by Ivan Ivashchenko.

In the midst of testing, pilot Ivashchenko was killed when his aircraft developed flutter which tore off his horizontal tail, causing a spin and crash on 17 March 1950. Lack of wing stiffness also resulted in aileron reversal which was discovered and fixed. Construction and tests of additional prototypes "SI-2" and experimental series aircraft "SI-02" and "SI-01" in 1951, were generally successful. On 1 September 1951, the aircraft was accepted for production, and formally given its own MiG-17 designation after so many changes from the original MiG-15. It was estimated that with the same engine as the MiG-15's, the MiG-17's maximum speed is higher by 40–50 km/h, and the fighter has greater manoeuvrability at high altitude.

Serial production started in August 1951, but large quantity production was delayed in favor of producing more MiG-15s so it was never introduced in the Korean War. It did not enter service until October 1952, when the MiG-19 was almost ready to be flight tested. During production, the aircraft was improved and modified several times. The basic MiG-17 was a general-purpose day fighter, armed with three cannons, one Nudelman N-37 37mm cannon and two 23mm with 80 rounds per gun, 160 rounds total. It could also act as a fighter-bomber, but its bombload was considered light relative to other aircraft of the time, and it usually carried additional fuel tanks instead of bombs.

Although a canopy which provided clear vision to the rear necessary for dogfighting like the F-86 was designed, production MiG-17Fs got a cheaper rear-view periscope which would still appear on Soviet fighters as late as the MiG-23. By 1953, pilots got safer ejection seats with protective face curtain and leg restraints like the Martin-Baker seats in the west. The MiG-15 had suffered for its lack of a radar gunsight, but in 1951, Soviet engineers obtained a captured F-86 Sabre from Korea and they copied the optical gunsight and SRD-3 gun ranging radar to produce the ASP-4N gunsight and SRC-3 radar. The combination would prove deadly over the skies of Vietnam against aircraft such as the F-4 Phantom whose pilots lamented that guns and radar gunsights had been omitted as obsolescent.

The second prototype variant, "SP-2" (dubbed "Fresco A" by NATO), was an interceptor equipped with a radar. Soon a number of MiG-17P ("Fresco B") all-weather fighters were produced with the Izumrud radar and front air intake modifications.

In early 1953 the MiG-17F day fighter entered production. The "F" indicated it was fitted with the VK-1F engine with an afterburner by modifying the rear fuselage with a new convergent-divergent nozzle and fuel system. The afterburner doubled the rate of climb and greatly improved vertical maneuvers. But while the plane was not designed to be supersonic, skilled pilots could just dash to supersonic speed in a shallow dive, although the aircraft would often pitch up just short of Mach 1. This became the most popular variant of the MiG-17. The next mass-produced variant, MiG-17PF ("Fresco D") incorporated a more powerful Izumrud RP-2 radar, though they were still dependent on Ground Control Interception to find and be directed to targets. In 1956 a small series (47 aircraft) was converted to the MiG-17PM standard (also known as PFU) with four first-generation Kaliningrad K-5 (NATO reporting name AA-1 'Alkali') air-to-air missiles. A small series of MiG-17R reconnaissance aircraft were built with VK-1F engine (after first being tested with the VK-5F engine).

Over 6,000 MiG-17s were built in the USSR by 1958. Another 2,000 were built under licence in Poland and China.

License production

In 1955, Poland received a license for MiG-17 production. The MiG-17F was produced by the WSK-Mielec factory under the designation Lim-5. The first Lim-5 was built on 28 November 1956 and 477 were built by 1960. An unknown number were built as the Lim-5R reconnaissance variant, fitted with the AFA-39 camera. In 1959–1960, 129 MiG-17PF interceptors were produced as the Lim-5P . PZL-WSK also developed several Polish strike variants based on the MiG-17 : the Lim-5M, produced from 1960; Lim-6bis, produced from 1963; and Lim-6M (converted in the 1970s); as well as two reconnaissance variants : the Lim-6R (Lim-6 "bis" R) and MR.

In China, an initial MiG-17F was assembled from parts in 1956, with license production following in 1957 at Shenyang. The Chinese-built version is known as the Shenyang J-5 (for local use) or F-5 (for export).

Operational history

MiG-17s were designed to intercept straight and level flying enemy bombers, not for air to air combat (Dog-fighting) with other fighters. This subsonic (.93 Mach) fighter was effective against slower (.6-.8 Mach), heavily loaded U.S. fighter-bombers, as well as the mainstay American strategic bombers during the MiG-17's development cycle (such as the Boeing B-50 Superfortress or Convair B-36 Peacemaker, which were both still powered by piston engines). Even if the target had sufficient warning and time to shed weight and drag by dropping external ordnance and accelerate to supersonic escape speeds, doing so would have inherently forced the enemy aircraft to abort its bombing mission. However, the USAF's introduction of strategic bombers capable of supersonic dash speeds such as the Convair B-58 Hustler and General Dynamics FB-111 rendered the MiG-17 obsolete in front-line PVO service and they were supplanted by supersonic interceptors such as the MiG-21 and MiG-23.

MiG-17s were not available for the Korean War, but saw combat for the first time over the Straits of Taiwan when PRC (Communist China) MiG-17s clashed with ROC (Nationalist China) F-86 Sabres in 1958.

In 1958, MiG-17s downed a US reconnaissance Lockheed C-130 Hercules over Armenia, with 17 casualties.

Vietnam War

In 1960, the first group of approximately 50 North Vietnamese airmen were transferred to the People's Republic of China (PRC) to begin transitional training onto the MiG-17. By this time the first detachment of Chinese trained MiG-15 pilots had returned to North Vietnam, and a group of 31 airmen were deployed to the People's Liberation Army Air Force base at Son Dong for conversion to the MiG-17. By 1962 the first North Vietnamese pilots had finished their MiG-17 courses in the Soviet Union and China, and returned to their units; to mark the occasion, the Soviets sent as a "gift" 36 MiG-17 fighters and MiG-15UTI trainers to Hanoi in February 1964. These airmen would create North Vietnam's first jet fighter regiment, the 921st. By 1965, another group of MiG pilots had returned from training in Krasnodar, in the USSR, as well as from the PRC. This group would form North Vietnam's second fighter unit, the 923rd Fighter Regiment. While the newly created 923rd FR operated strictly MiG-17s, and initially these were the only types available to oppose modern American supersonic jets, more modern supersonic Soviet fighters would be later introduced as the 921st FR would operate both MiG-17s and MiG-21s (in 1969 the 925th FR MiG-19 unit would be formed).

Although U.S. fighter-bombers had been engaged in combat since 1961, and some of the most experienced Americans such as James Robinson Risner were Korean War aces, the North Vietnamese Air Force MiGs and their untried pilots lacked combat experience. The baptism of fire of the MiG-17 in this conflict occurred on 3 April 1965. That day two groups of MiGs took off from Noi Bai airbase. The first group comprised two jets and acted like a bait; the second was made-up of four MiG-17s and was the strike group. Their target were U.S. Navy aircraft supporting an USAF 80-aircraft strike package trying the knock out Ham Rung bridge near Thanh Hoa. The MiG-17 leader, Lt. Pham Ngoc Lan, spotted a group of Vought F-8 Crusaders of the VF-211, USS Hancock, and shot-up the F-8E flown by Lt. Cdr. Spence Thomas, which would perform an emergency landing ashore at Da Nang. His wingman Phan Van Tuc claimed a second F-8, but this is not corroborated by USN loss listings.

On 4 April 1965, the USAF conducted a "re-strike" on the Hàm Rồng/Thanh Hoa bridge with 48 Republic F-105 Thunderchiefs of the 355th Tactical Fighter Wing (TFW) loaded with 384 x 750 lb (340 kg) bombs. The Thunderchiefs were escorted by a MiG CAP flight of North American F-100 Super Sabres from the 416th Tactical Fighter Squadron (TFS). Coming from above, four MiG-17s from the 921st Fighter Regiment (FR) tore through the escorts and dove onto the Thunderchiefs, shooting two of them down; the leader Tran Hanh downed F-105D 59-1754 of Major F. E. Benett, and his element leader Le Minh Huan downed F-105D 59-1764 of Captain J. A. Magnusson. The Super Sabres engaged with one firing a "AIM-9 Sidewinder" air-to-air missile which apparently missed (or malfunctioned), and another F-100D flown by Captain Donald Kilgus fired 20mm cannons, which also apparently missed, but shot down and killed Tran Hanh's wingman Pham Giay. No other U.S. airmen reported any confirmed aerial kills during the air battle. However, Tran Hanh stated that three of his accompanying MiG-17s had been shot down by the opposing USAF fighters.

During the 4 April 1965 engagement, four MiG-17s from the 921st FR had tangled with over 50 U.S. jet fighter-bombers, consisting of F-105s and F-100s. Three F-100s from the MiGCAP, piloted by LTC Emmett L. Hays, CPT Keith B. Connolly, and CPT Donald W. Kilgus, all from the 416th TFS, engaged the MiG-17s. One Super Sabre fired an air-to-air missile and Connolly and Kilgus engaged with 20 mm cannon, with only Kilgus claiming a probable kill. The four attacking MiGs from the 921st FR were flown by Flight Leader Tran Hanh, Wingman Pham Giay, Le Minh Huan and Tran Nguyen Nam. Flight Leader Tran Hanh was the only survivor from the air battle and reportedly stated that his three MiG-17s were "... shot down by the F-105s." Based upon the report, the USAF F-100s very well could have been mistaken for F-105s, and the reported loss of three MiG-17s to those mistaken jet fighters would indicate that the USAF F-100 Super Sabres had obtained the first U.S. aerial combat victories during the Vietnam War.

The MiG-17 was the primary interceptor of the fledgling Vietnam People's Air Force in 1965, scoring its first aerial victories and seeing extensive combat during the Vietnam War, the aircraft frequently worked in conjunction with MiG-21s and MiG-19s. Many historians believe that some North Vietnamese pilots, in fact, preferred the MiG-17 over the MiG-21 because it was more agile, though not as fast; however, of the 16 NVAF Aces of the war, 13 of them attained that status while flying the MiG-21. Only three North Vietnamese Airmen gained Ace status while flying the MiG-17. Those were : Nguyen Van Bay (7 victories), Luu Huy Chao and Le Hai (both with six).

The MiG-17 was not originally designed to function as a fighter-bomber, but in 1971 Hanoi directed that United States Navy warships were to be attacked by elements of the North Vietnamese Air Force. This would require the MiG-17 to be fitted with bomb mountings and release mechanisms. Chief Engineer of the NVAF ground crews, Truong Khanh Chau, was tasked with the mission of modifying two MiG-17s for the ground attack role; after three months of work, the two jets were ready. On 19 April 1972, two pilots from the 923rd FR took their bomb laden MiG-17s and attacked the U.S. Navy destroyer USS Higbee (DD-806) and light cruiser USS Oklahoma City (CLG-5). Each MiG was armed with two 250 kg (550 lb) bombs. Pilot Le Xuan Di managed to hit the destroyer's aft 5" gun mount, destroying it, but inflicting no fatalities, as the crewmen had vacated the turret earlier due to a malfunction with the gun system.

From 1965 to 1972, MiG-17s from the NVAF 921st and 923rd FRs would claim 71 aerial victories against U.S. aircraft : 11 Crusaders, 16 F-105 Thunderchiefs, 32 McDonnell Douglas F-4 Phantom IIs, two Douglas A-4 Skyhawks, seven Douglas A-1 Skyraiders (propeller driven strike aircraft), one C-47 cargo/transport aircraft, one Sikorsky CH-3C helicopter and one Ryan Firebee UAV.

The American fighter community was shocked in 1965 when elderly, subsonic MiG-17s downed sophisticated Mach-2-class F-105 Thunderchief fighter-bombers over North Vietnam.

Other MiG-17 users

Twenty countries flew MiG-17s. The MiG-17 became a standard fighter in all Warsaw Pact countries in the late 1950s and early 1960s. They were also bought by many other countries, mainly in Africa and Asia, that were neutrally aligned or allied with the USSR. The MiG-17 still flies today in the air forces of Burkina Faso, China (JJ-5 Trainer) Mali, Mozambique, North Korea, Republic of the Congo, Sudan, Tanzania and Zimbabwe. Africa

At least 24 of them served with the Nigerian Air Force and were flown by a mixed group of local Nigerian and mercenary pilots from East Germany, Soviet Union, South Africa, the United Kingdom, and Australia during the 1967-70 Nigerian Civil War.

Asia

  • Four were hurriedly supplied by the USSR to Sri Lanka during the 1971 insurgency and were used for bombing and ground attack in the brief insurgency. Four North Korean MiG-17 aircraft were involved in the EC-121 shootdown incident in 1969.

    Soviet Union

    Similarly in 1958, a U.S. Air Force Lockheed C-130 was shot down by four MiG-17 fighters when it flew into Soviet airspace near Yerevan, Armenia while on a Sun Valley SIGINT mission, with all 17 crew killed.

    United States

    A number of U.S. federal agencies undertook a program at Groom Lake to evaluate the MiG-17 to help fight the Vietnam War, as North Vietnamese MiG-17s and MiG-21s had a kill rate against them of 9 :1. The program was code-named HAVE DRILL, involving trials of two ex-Syrian MiG-17F Frescos over the skies of Groom Lake. These aircraft were given USAF designations and fake serial numbers so that they may be identified in DOD standard flight logs.

    In addition to tracking the dog fights staged between the various MiG models against virtually every fighter in U.S. service, and against SAC's B-52 Stratofortress and B-58 Hustlers to test the ability of the bombers’ countermeasures systems. They also performed radar cross-section and propulsion tests that contributed greatly to improvements in U.S. aerial performance in Vietnam.

    According to the FAA there are 27 privately owned MiG-17s in the U.S.

    Variants

    • I-330 : Prototype.
    • MiG-17 ("Fresco A") : Basic fighter version powered by VK-1 engine ("aircraft SI").
    • MiG-17A : Fighter version powered by VK-1A engine with longer lifespan.
    • MiG-17AS : Multirole conversion, fitted to carry unguided rockets and the K-13 air to air missile.
    • MiG-17P ("Fresco B") : All-weather fighter version equipped with Izumrud radar ("aircraft SP").
    • MiG-17F ("Fresco C") : Basic fighter version powered by VK-1F engine with afterburner ("aircraft SF").
    • MiG-17PF ("Fresco D") : All-weather fighter version equipped with Izumrud radar and VK-1F engine ("aircraft SP-7F").
    • MiG-17PM/PFU ("Fresco E") : Fighter version equipped with radar and K-5 (NATO : AA-1 "Alkali") air-to-air missiles ("aircraft SP-9").
    • MiG-17R : Reconnaissance aircraft with VK-1F engine and camera ("aircraft SR-2s")
    • MiG-17SN : Experimental variant with twin side intakes, no central intake, and nose redesigned to allow 23 mm cannons to pivot to engage ground targets. Not produced.
    • Shenyang J-5 : Originally designated Dongfeng-101 - (East Wind-101), and also Type 56 before being designated J-5 in 1964

    Some withdrawn aircraft were converted to remotely controlled targets.

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    This text is available under the Creative Commons Attribution-ShareAlike License
    Source : Article Mikoyan-Gurevich MiG-17 of Wikipedia ( authors )

    Specifications (J-5)

    • Crew : 1.
    • Length : (JJ-5 - 11.5 m/37 ft 9 in)(J-5A - 11.36 m/37 ft 4 in) 11.09 m (36 ft 5 in)
    • Height : 3.8 m (12 ft 5 in).
    • Wingspan : 9.628 m (31 ft 7 in).
    • Wing area : 22.6 m² (790 ft²).
    • Empty weight : (JJ-5 - 4,080 kg / 8,994 lb) (J-5A - 4,151kg / 9,151 lb) n.a. kg (n.a. lb).
    • Gross weight : (JJ-5 - 6,215 kg / 13,700 lb) 6,000 kg (13,230 lb).
    • Maximum speed : @ 5,000 m (JJ-5 - 1,048 km/h / 651 mph)(J-5A - 1,145 km/h/711 mph) 1,130 km/h (702 mph).
    • Range : with drop tanks @ 10,000 m (JJ-5 - 1,230 km/764 mi) (J-5A - 1,730 km/1,075 mi) 1,424 km (1,037 miles).
    • Service ceiLIng : (JJ-5 - 14,300 m/46,900 ft) (J-5A - 16,600 m/54,450 ft) 16,500 m (54,000 ft).
    • Rate of cLImb @ 5,000 m : (JJ-5 - 27 m/s/5,315 ft/min) (J-5A - 65 m/s/12,800 ft/min) 65 m/s (12,795 ft/min).
    • Powerplant : One Wopen WP-5, (JJ-5(WP-5D) - 22.27 kN/5,000 lbf) 25.5 kN (5,730 lbf) thrust dry, 33.8 kN (7,452 lbf) with afterburner.
    • Armament : One Type 37 37 mm aircraft cannon. Two Type 23-1 23 mm aircraft cannon. (JJ-5 - One Type 23-1 23 mm aircraft cannon) (J-5A - Three Type 23-1 23 mm aircraft cannon).

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    This text is available under the Creative Commons Attribution-ShareAlike License
    Source : Article Mikoyan-Gurevich MiG-17 of Wikipedia ( authors )
    Mikoyan-Gourevitch Mig-17 "Fresco" : Your comments on this subject
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    The site is not optimized, or even designed to run on older browsers or those deliberately deviating from standards. You will most probably encounter display issues with Internet Explorer. In this case, it is strongly recommended installing a modern (and free!) browser that's respecting the standards, like Firefox, Opera, Chrome or Safari.

    Cookies and Javascript

    This site uses cookies and JavaScript to function properly. Please ensure that your browser is configured accordingly. Neither of these technologies, or other means shall in no case be used on the Site for the retention or disclosure of personal information about its Visitors. See the "Legal" page for more on this subject.

    Website layout

    Left menus

    Because of the lack of space on smartphones and small tablets, these menus are hidden. Everything is nevertheless accessible via the main menu option, located between the video and photo sections. This menu is placed there for compatibility reasons with some browsers, which play the videos over the menus.

    "Search" and "Latest" :
    The link "In Titles" restricts the search to the titles of different forms. Use this option if you are looking for a plane, a constructor, a pilot or a particular event that could have been treated as a subject.

    The link "In Stories" will bring you to a search in all texts (the "Story" tab) and will take more time. The search term will appear highlighted in green when opening the corresponding story.

    Would you believe, "Timeline" will show all subjects in chronological order.

    "Random" will reload the entire page with a new random topic.

    The bottom section keeps you abreast of the latest five entries. New topics are added regularly. Don't hesitate to come visit us often : add bookmark.

    Blogs and Comments central section

    Under the photos section comes the comments tabs window :

    You can enter general comments in your own language via one of the two buttons on the left (BLOG EN and BLOG FR). Note that these buttons are accessible regardless of the language to allow some participation in the other language.

    All comments are subject to moderation and will be published only if they comply with the basic rules of decorum, while remaining relevant to the purpose of this site.

    The third tab allows you to enter comments on the shown topic and is bilingual. Personal anecdotes, supplements and other information questions will take place here.

    The "Story" tab shows the explanatory texts. They are most often taken from Wikipedia, a site where we participate regularly.

    The "Data" tab is reserved for list of features and specifications.

    Right menus

    On a smartphone, the lack of space is growing and this menu is moved to the bottom of the page to give priority to videos and pictures.

    The top right icons are links to videos posted by third parties (on their own responsabilities) or by ourselves. The link below these icons will take you to the channel of the one who posted the video. Feel free to suggest other videos if you think they are of some interest (Use the BLOG button or the "Contact" link).