HASEGAWA 1/72-SCALE MIKOYAN MIG-25 FOXBAT SOVIET AF COLD WAR INTERCEPTOR KIT

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HASEGAWA 1/72-SCALE MIKOYAN MIG-25 FOXBAT SOVIET AF COLD WAR INTERCEPTOR KIT BELENKO

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Additional Information from Internet Encyclopedia

The Mikoyan-Gurevich MiG-25 (Russian: Микоян и Гуревич МиГ-25) (NATO reporting name: Foxbat) is a supersonic interceptor and reconnaissance aircraft that was among the fastest military aircraft to enter service. It was designed by the Soviet Union's Mikoyan-Gurevich bureau. The first prototype flew in 1964 and the aircraft entered service in 1970. It has a top speed of Mach 2.83 (Mach 3.2 is possible but at risk of significant damage to the engines), and features a powerful radar and four air-to-air missiles.

When first seen in reconnaissance photography, the large wing planform suggested an enormous and highly maneuverable fighter, at a time when U.S. design theories were also evolving towards higher maneuverability due to combat performance in the Vietnam War. The appearance of the MiG-25 sparked serious concern in the West and prompted dramatic increases in performance for the McDonnell Douglas F-15 Eagle then under development in late 1960s. The capabilities of the MiG-25 were better understood in 1976 when Soviet pilot Viktor Belenko defected in a MiG-25 to the United States via Japan. It turned out that the aircraft's weight necessitated its large wings.

Production of the MiG-25 series ended in 1984 after completion of 1,190 aircraft. A symbol of the Cold War, the MiG-25 flew with Soviet allies and former Soviet republics, remaining in limited service in Russia and several other nations. It is one of the highest-flying military aircraft, and the second fastest after the SR-71 reconnaissance aircraft

Work on the new Soviet interceptor that became the MiG-25 started in mid-1959, a year before Soviet intelligence learned of the American Mach 3 A-12 reconnaissance aircraft. It is not clear if the design was influenced by the American A-5 Vigilante.

The design bureau studied several possible layouts for the new aircraft. One had the engines located side-by-side, as on the MiG-19. The second had a stepped arrangement with one engine amidships, with exhaust under the fuselage, and another in the aft fuselage. The third project had an engine arrangement similar to that of the English Electric Lightning, with two engines stacked vertically. Option two and three were both rejected because the size of the engines meant any of them would result in a very tall aircraft which would complicate maintenance.

The idea of placing the engines in underwing nacelles was also rejected because of the dangers of any thrust asymmetry during flight. Having decided on engine configuration, there was thought of giving the machine variable-sweep wings and a second crew member, a navigator. Variable geometry would improve maneuverability at subsonic speed, but at the cost of decreased fuel tank capacity. Because the reconnaissance aircraft would operate at high speed and high altitude the idea was soon dropped. Another interesting but impractical idea was to improve the field performance using two RD36-35 lift-jets. Vertical takeoff and landing would allow for use of damaged runways during wartime and was studied on both sides of the Iron Curtain. The perennial problem with engines dedicated to vertical lift is they become mere deadweight in horizontal flight, and also occupy space in the airframe needed for fuel. The MiG interceptor would need all the fuel it could get, so the idea was abandoned.

The first prototype was a reconnaissance variant, designated "Ye-155-R1", that made its first flight on 6 March 1964. It had some characteristics that were unique to that prototype, and some of these were visually very evident: the wings had fixed wingtip tanks (600 litre capacity) to which small winglets were attached for stability purposes, but when it was found that fuel sloshing around in the tanks caused vibrations they were eliminated. The aircraft also had attachments for movable foreplanes, canards, to help with pitch control at high speed (provisions for canards had previously been installed, but not used, on the Ye-152P.)

The first flight of the interceptor prototype, "Ye-155-P1", took place on 9 September 1964. Development of the MiG-25, which represented a major step forward in Soviet aerodynamics, engineering and metallurgy, took several more years to complete.

On 9 July 1967, the new aircraft was first shown to the public at the Domodedovo air show, with four prototypes (three fighters and a reconnaissance aircraft) making a flypast.

Because of the thermal stresses incurred in flight above Mach 2, the Mikoyan-Gurevich OKB had difficulties choosing what materials to use for the aircraft. They had to use E-2 heat-resistant Plexiglas for the canopy, and high-strength stainless steel for the wings and fuselage. Using titanium rather than steel would have been ideal, but it was expensive and difficult to work with. The problem of cracks in welded titanium structures with thin walls could not be solved, so the heavier nickel steel was used instead. It cost far less than titanium and allowed for welding, along with heat resistant seals. The MiG-25 was constructed from 80% nickel steel alloy, 11% aluminium, and 9% titanium. The steel components were formed by a combination of spot-welding, automatic machine welding and hand arc welding methods.

Initially, the interceptor version was equipped with the TL-25 Smerch-A (also referred to as Product 720) radar, a development of the system carried by the earlier Tu-128. While powerful, and thus long-ranged and resistant to jamming, the system – due to the age of its design and its intended purpose (tracking and targeting high- and fast-flying US bombers and reconnaissance aircraft), lacked Look-down/shoot-down capability, which limited its effectiveness against low-flying targets (this is one of the reasons why it was replaced with the Mikoyan-Gurevich MiG-31, whose Zaslon radar has that capability). By the time the MiG-25 entered service in 1969, this was a serious shortcoming, as strategic bombing doctrine was shifting towards low-level penetration of enemy territory. After Belenko's defection to Japan exposed this flaw to the West, a government decree issued on November 4, 1976 called for urgent development of a more advanced radar. This resulted in the pulse-Doppler radar Sapphire-25 system fitted to the MiG-25PD variant.

Automatic control system SAU 155П1 (interceptor) or SAU 155Р1 (scout): navigation system «Peleng-D (ETC, DM)»; heat radar 26Ш-1; radio guidance system «Lazur» (for interceptor); direction finder ARC-10; altimeter great heights RV-18 (RV-19); SPO Sirena-3M» or LO 06 «Birch»; control system air intake СРВМу-2A; system range radionavigation RSBN-6C «coral»; marker radio MCI-56П; intercom SPU-7; the Respondent CO-63B; system of air signals SVS-MO-5; voice informer RI-65; voice recorder MS-61 and others On late production was installed SEC «rainbow».

All interceptors installed «Polet-1I,» consisting of the electronic systems of navigation and landing, курсовертикали, air signals and systems of the automatic flight control. The spies were established: photographic equipment And 70 or A-72 station Electronic intelligence Cube-3M», «Sabre» Side looking airborne radar, the station of signals intelligence «Virazh» or «Pitch».

Armament interceptor includes four supersonic (M>5) UR great range R-40T (R-40TD) air-to-air missiles with thermal homing head and P-40P (R-40RD) with semi-active radar guidance system (maximum launch range, on altitudinal goal on a collision course – 35–60 km). Under the fuselage can suspended fuel tank. The aircraft could carry unguided gravity bombs in a rudimentary strike capability. As the bombs would weigh no more and incur no more drag than its regular load of R-40 missiles, its performance was not impaired, leading to some impressive bombing feats; when released at an altitude of 20,000m (66,000 ft) and a speed above Mach 2, a 500 kg bomb would have a glide range of several tens of kilometres.

The MiG-25 was theoretically capable of a maximum speed of Mach 3+ and a ceiling of 90,000 ft (27,000 m). Its high speed was problematic: although sufficient thrust was available to reach Mach 3.2, a limit of Mach 2.83 had to be imposed as the turbines tended to overspeed and overheat at higher speeds, possibly damaging them beyond repair.

The unarmed 'B' version had greater impact than the interceptor when the USSR sent two MiG-25R, and two MiG-25RB to Egypt in March 1971 and stayed until July 1972. They were operated by the Soviet 63rd Independent Air Detachment (Det 63) set up specially for this mission. Det 63 flew over Israeli held territory in Sinai on reconnaissance missions roughly 20 times. The flights were in pairs at maximum speed and high altitude (between 17,000–23,000 m).

On 6 November 1971, an Egyptian MiG-25 flying at Mach 2.5 was met by Israeli F-4Es and fired upon unsuccessfully. A MiG-25 was tracked flying over Sinai at Mach 3.2 during this period. The MiG-25 engines went into overspeed, which led to them being scrapped. Unit Det 63 was sent back home in 1972, though reconnaissance Foxbats were sent back to Egypt in 19–20 October 1973 during the Yom Kippur War. Unit Det 154 remained there until late 1974.

On 13 February 1981, the Israeli Air Force sent two RF-4Es over Lebanon as decoys for Syrian MiG-25 interceptors. As the MiGs scrambled, the RF-4Es turned back delivering chaff and using ECM pods. Two IDF/AF F-15As were waiting for the MiGs and shot one of them down with AIM-7F missiles. The other MiG was able to escape. In a similar engagement, on 29 July 1981, a Syrian MiG-25 was again downed by an Israeli F-15A, after which a second MiG-25 launched its R-40 missiles at the F-15 and its wingman, but they missed. However, other sources say the missiles hit and downed one of the F-15s. On 31 August 1982, a third Syrian MiG-25 was damaged by an Israeli Hawk SAM and then destroyed by an F-15.

During the 1970s, the Soviet air force conducted reconnaissance overflights across Iran using its MiG-25RBSh aircraft in response to joint US-Iran recon operations.

The Swedish Air Force observed via radar a Soviet Air Defense MiG-25 at 63,000 ft trailed 2.9 km behind the Lockheed SR-71 Blackbird at 72,000 ft over the Baltic Sea in the 1980s.

The MiG-25 was in service with the Iraqi Air Force during the Iran–Iraq War. On 19 March 1982 an Iranian F-4E was badly damaged by missile fired by an Iraqi MiG-25. Iraqi MiG-25s made another kill against Iran in February 1983, when an Iraqi MiG-25PD shot down an Iranian C-130. On April 1984, an Iraqi MiG-25PD shot down an Iranian F-5E. On 21 March 1984, an Iraqi MiG-25PD shot down an Iranian F-4E and on 5 June 1985 an Iraqi MiG-25PD shot down a second Iranian F-4E. On 23 February 1986, an Iraqi MiG-25PD shot down an Iranian EC-130E and on 10 June an RF-4E, later in October 1986, an Iraqi MiG-25PDS shot down a second RF-4E.

The most successful Iraqi MiG-25 pilot of the war was Colonel Mohammed Rayyan, who was credited with 10 kills. Eight of these were while flying the MiG-25P from 1981 to 1986. In 1986, after attaining the rank of Colonel, Rayyan was shot down and killed by Iranian F-14s. For the majority of the air combat Iraqi pilots used R-40 missiles.

On 3 May 1981, an Iraqi MiG-25PD shot down an Algerian Gulfstream III. On 2 October 1986, an Iraqi MiG-25PD shot down a Syrian MiG-21RF.

According to research by journalist Tom Cooper, at least 10 MiG-25s (9 reconnaissance and 1 fighter) may have been shot down by Iranian F-14s (one of them shared with an F-5) during the Iran-Iraq war. Only three MiG-25 losses (to ground fire and air combat) were confirmed by Iraq.

During the Persian Gulf War, a US Navy F/A-18, piloted by Lt Cdr Scott Speicher, was shot down on the first night of the war by a missile fired by a MiG-25. The kill was reportedly made with a Bisnovat R-40TD missile fired from a MiG-25PDS flown by Lt. Zuhair Dawood of the 84th squadron of the IQAF.

Two IQAF MiG-25s were shot down by U.S. Air Force F-15s on January 19. The MiGs attempted to hide from the F-15s by using chaff and electronic jammers in order to engage the F-15s undetected. However the F-15 pilots were able to reacquire the two Iraqi MiG-25s and shot both down with AIM-7 Sparrow missiles. In another incident, an Iraqi MiG-25PD, after eluding eight USAF F-15s at long range, fired three missiles at General Dynamics EF-111A Raven electronic warfare aircraft, forcing them to abort their mission and leave attacking aircraft without electronic jamming support.

In a different incident, two MiG-25s approached a pair of F-15s, fired missiles at long range which were evaded by the F-15s, and then outran the American fighters. Two more F-15s joined the pursuit, and a total of 10 air-to-air missiles were fired at the MiG-25s, though none reached them. According to the same sources, at least one F-111 was also forced to abort its mission by a MiG-25 on the first 24 hours of hostilities, during an air raid over Tikrit.

After the war, on 27 December 1992, a U.S. F-16D downed a MiG-25 that violated the no-fly zone in southern Iraq with an AIM-120 AMRAAM missile. It was the first USAF F-16 air-to-air victory and the first AMRAAM kill.

On 23 December 2002, an Iraqi MiG-25 shot down a U.S. Air Force unmanned MQ-1 Predator drone, which was performing armed reconnaissance over Iraq. This was the first time in history that an aircraft and an unmanned drone had engaged in combat. Predators had been armed with AIM-92 Stinger air-to-air missiles, and were being used to "bait" Iraqi fighter aircraft, then run. In this incident, the Predator did not run, but instead fired one of the Stingers, which missed, while the MiG's missile did not.

No Iraqi aircraft were deployed in the U.S. invasion of Iraq in 2003, with most Iraqi aircraft being hidden or destroyed on the ground. In August 2003, several dozen Iraqi aircraft were discovered buried in the sand.

The MiG-25 was kept a guarded secret in India, and was nicknamed "Garuda", after the large mythical bird-like creature from Hindu and Buddhist mythology. It was used extensively in the Kargil War and Operation Parakram, conducting aerial reconnaissance sorties over Pakistan.

In May 1997, an Indian Air Force Mikoyan MiG-25RB reconnaissance aircraft created a furor when the pilot flew faster than Mach 2 over Pakistani territory following a reconnaissance mission into Pakistan airspace. The MiG-25 broke the sound barrier while flying at an altitude of around 65,000 feet (20,000 m), otherwise the mission would have remained covert, at least to the general public. The Pakistan Government considered the breaking of the sound barrier was deliberate to make the point that the Pakistan Air Force (PAF) had no aircraft in its inventory which can come close to the MiG-25's cruising altitude (up to 74,000 feet (23,000 m)). India denied the incident but Pakistan's Foreign Minister, Gohar Ayub Khan, believed that the Foxbat photographed strategic installations near the capital, Islamabad.

Lack of spare parts and India's acquiring of unmanned aerial vehicles and satellite imagery eventually led to its retirement in 2006.




 
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