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  • Mikoyan-Gurevich MiG-25 (Foxbat) Supersonic Interceptor / Reconnaissance Bomber Aircraft

    The Mikoyan-Gurevich MiG-25 Foxbat was specifically designed to intercept the ultimately-cancelled North American XB-70 Valkyrie Mach 3 bomber.

     Updated: 2/1/2017; Authored By Staff Writer; Content ¬©www.MilitaryFactory.com

    Like the Tupolev Tu-95 "Bear" and the Mikoyan-Gurevich MiG-21 "Fishbed", the MiG-25 (NATO reporting name of "Foxbat") became symbolic of the Soviet air threat posed to the West (and her respective interests worldwide) throughout the latter half of the Cold War. The high-speed, high-altitude interceptor was a record-setter from the beginning and would serve in some quantity with air forces within the Soviet sphere of influence for decades. Their most notable actions occurred in the Iran-Iraq War with some modest successes and lesser so in the follow-up 1991 Gulf War, where many were destroyed on the ground by coalition forces. Regardless, the MiG-25 was a powerful aircraft in every sense of the word and was a deadly design if used in conjunction with proper facilities and expertly trained personnel. Designed to meet the proposed North American B-70 "Valkyrie" jet-powered bomber series that never was, the MiG-25 nevertheless went down in aviation history as a successful Soviet-era venture - one whose fruits can still be valued today, albeit in limited service numbers. The MiG-25 did well to counter the Lockheed SR-71 spy plane as well as force the pricey development (and ultimate production) of the McDonnell Douglas F-15 Eagle air superiority series. Some 1,190 MiG-25s of all types were eventually produced covering interception, reconnaissance, ELINT, training and bombing duties.

    The MiG-25 would never be confused with a "dedicated" fighter by any regard for her high-operating speed, poor out-of-the-cockpit visibility and rapid use of fuel preclude her from any long-standing aerial engagement. Instead, she became a very specialized thoroughbred designed with the single-minded lethal purpose of interception - led to her targets by way of powerful ground-based radar systems - while fielding a healthy collection of hard-hitting missiles. The MiG-25 utilized some of the largest missiles (19.5 feet in length) ever fitted to an aircraft in the AA-6 "Acrid" series, able to engage targets some 50 miles away. Foxbats were therefore stationed along both sides of the Soviet Empire, protecting its airspace from anything the West could seemingly muster. The arms race was in full swing and every move required a critical counter-move to match.

    In the late 1950s, the United States Air Force undertook development of a long-range, supersonic strategic bomber capable of Mach 3+ speeds and achieving altitudes upwards of 70,000 feet under the developmental designation of XB-70 "Valkyrie". The aviation firm of North American - designer and developer of the World War 2-era war-winning P-51 Mustang fighter - was tabbed with its creation. The idea behind such an airframe was in presenting Soviet air defenses with an untouchable target - outclassing the latest interceptors or surface-to-air missile systems then in inventory and those charged with protecting the vast airspace of the Soviet realm. The United States Air Force's Strategic Air Command envisioned a fleet of B-70 bombers in its stable, holding a distinct advantage in capabilities of reconnaissance and delivery of munitions should the Cold War ever go "hot". In response to the XB-70, the Soviets enacted a counter-program to shore up its aged and limited air defense network - a proposed Mach 3-capable manned interceptor to serve directly with the PVO - the Soviet Air Defense Force. Work on the aircraft began in the middle of 1959.

    The Valkyrie was a large aircraft design, powered by no less than six afterburning turbojet engines and fielding an impressive streamlined shape. However, missile technology began evolving at such a rapid pace even before the proposed bomber took to the skies and intercontinental ballistic missiles soon took over the role of proposed high-level, fast bombers. Couple these developments with the ballooning costs of the Valkyrie program as a whole and the need for the North American product became less appealing to American warplanners. As such, the Valkyrie program was officially halted and ultimately cancelled in 1961. Despite the cancellation, a pair of prototypes were completed under the experimental designation of XB-70A (a third was under construction but never finished) and first flight was recorded on September 21st, 1964. However, the XB-70A would never serve in an operational military role, instead relegated for use as a supersonic testbed. The series continued as such from 1964 onwards. In 1966, one of the prototypes was lost to accident during a mid-air collision with a trailing observation aircraft during a photoshoot but research flights continued on until 1969. The remaining prototype ended up as a museum showpiece at the National Museum of the USAF in Dayton, Ohio, where it resides today.

    While the Americans closed the chapter on their Valkyrie, development of the Soviet "Valkyrie Killer" had progressed far enough that cancellation was not in the stars - and perhaps Soviet authorities understood the impending long-term impact of the upcoming Lockheed SR-71 "Blackbird" Mach 3-capable strategic reconnaissance jet originating with the company's A-12 of 1962.

    As such, the Soviet design team at Mikoyan-Gurevich - a firm having made a name for itself in World War 2 - looked to tackle several key development hurdles en route to a polished end-product. Chief among these became the "heat barrier" encountered by high-performance aircraft attempting high-speed flight. The team looked through their available options and realized that they would have to incorporate several different construction technologies and a mix of materials to promote a viable sustaining airframe. Titanium, though expensive and difficult to work with, was selected for its strength and high-heat resistance and tabbed to be used along the nose and leading edges - those surfaces most exposed to heat generation at high speed. Instead of riveted aluminum along other facings, welded steel was utilized. In the end, some 80 percent of the new airframe would consist of tempered nickel steel along with 11 percent encompassing aluminum alloy and the final 9 percent made up of the valuable titanium. As with any aircraft contending with high-speed, high-altitude flight, pilots of the new Mikoyan-Gurevich aircraft would be forced to wear full-pressure suits - appearing more as space-bound cosmonauts than conventional pilots - for their own safety. The designation of "Ye-155" was assigned to the proposed interceptor design and final Soviet approval was handed down in February of 1962.

    With the design in place, development - and ultimate construction - began on the Ye-155-P1. On September 9th, 1964, the aircraft was sent aloft for the first time with a pair of the large Mikulin-brand R-15B-300 series turbojet engines delivering 22,500lbs of thrust each. Such power came at a price, however, for each engine was rated a service life of just 150 hours. The aircraft received the Smertch-A radar (NATO: "Foxfire") for the intended interception role and armament would be pairings of various air-to-air missiles tied to the powerful radar system. The Foxfire radar maintained the capability of detecting targets out to 62 miles while the aircraft's missile armament would become a mix of both semi-active and infrared-homing R-40R and R-40T series missile systems. The goal of such an aircraft was, naturally, to get aloft as quickly as possible, achieve altitude and race to a threat, detect the incoming enemy and gain initiative and ultimately engage at distance, delivering a lethal payload to the target before triggering a response. The Ye-155-P1 certainly held the qualities of such an interceptor. Subsequent evaluation of the Ye-155-P1 airframe in-flight yielded acceptable results.

    While the Ye-155 was always envisioned for its interception qualities, Mikoyan-Gurevich was not lost on its possible use as an untouchable "fast reconnaissance" platform. Even before the interceptor model was made available for its first flight, a reconnaissance prototype - the Ye-155-R1 - recorded its maiden flight on March 6th, 1964, again, proving the airframe held some multi-faceted qualities that could serve Soviet air power interests quite well. The reconnaissance model fitted one vertically-set and four obliquely-set cameras along her forward airframe and could be identified by her antennas further on up the nose assembly.

    To further drive the apparent success of Soviet ingenuity when concerning the Ye-155 prototype, the aircraft was assigned a secret designation of "Ye-266" (Ye-266M) and utilized as a record-breaking platform, these records ultimately and formally acknowledged by the Federation Aeronautique Internationale (FAI) and bringing attention of the Soviet design to Western observers for the first time. The first record breaking act occurred on March 16th, 1965 with Alexander Fedotov at the controls, reaching 2,319.12km/h and a 1,000- and 2,000kg payload. 2,982.5km/h was then achieved without a payload in 1967. Fedotov eventually claimed another record by reaching an altitude of 29,977m while carrying a payload of 1,000kg and later netted 35,230m with a 1,000kg payload - the latter record, however, resulting in an double engine flameout and forcing the pilot to glide his aircraft back down to safety. On August 31st, 1977, a Ye-266M fitted with a pair of R-15-BF2-300 engines set a speed record at 123,523.62 feet. Of the 29 records claimed by the new Soviet design, several were not broken until the early-to-mid 1990s while others remain even today. Lockheed's A-12 was quick to capture several records away from the Mikoyan-Gurevich aircraft by May of 1965. Regardless, for their efforts in the design of the Ye-155/Ye-266 and its counterparts, the design Mikoyan-Gurevich design team were given the "Lenin Prize" achievement. Incidentally, the Ye-266 record-breaking airframe would prove critical in the development and ultimate production of the upcoming MiG-31 "Foxhound" series - a long-range interceptor of 1982 created to overcome the performance limitations of the MiG-25 series once the latter entered service production with Soviet units in the 1970s.

    Production of the Soviet interceptor was enacted in 1969 under the military designation of "MiG-25". However, reliability issues pertaining to the complex engines reared up during early use, forcing full front line service to be delayed until 1973. Once in operation, the MiG-25 was the same complicated machine as found during development and her operations were more-or-less curtailed to protect her touchy engine qualities. The engines, though inherently powerful, only allowed for short spurts of top level thrust to reach the perceived maximum Mach 3 interception speed so pilots were told to limit general usage to about Mach 2.8 to help maximize optimal engine service lives and avoid flameouts.

    Once known to NATO - they believing the new Soviet aircraft to be an agile, dedicated fighter design - assigned the MiG-25 the codename of "Foxbat" to coincide with NATO practice of designating Soviet fighters with "F" names and bombers with "B" names. For much of the remaining Cold War, there stood little in the way of information or imagery concerning the elusive MiG-25. A bit stroke of luck finally formulated on September 6th, 1976, when Soviet pilot Viktor Belenko defected from the Soviet Union and landed his MiG-25P at Hakodate Airport in north Japan. His journey began at Sakharovka Air Base and, upon landing, US intelligence personnel were on hand to take ownership of his MiG-25. It was soon under evaluation to which its ultimate strengths and inherent weaknesses became well known to the American intelligence community. The MiG-25 was by no means an agile fighter but, by then, production of the McDonnell Douglas F-15 Eagle air superiority fighter - developed to contend with the MiG-25 - was well underway, the new American mount having already entered service in January of 1976. Belenko also brought word with him of the soon-to-arrive MiG-31 series - an interceptor now capable of engaging targets - aircraft and cruise missiles - at low altitudes.

    Outward design of the MiG-25 "Foxbat" was highly conventional by any standard, fitting a long slab-sided fuselage against a square-shaped airframe. The airframe design was necessitated by the installation of the large pair of engines buried deep within the design. Intakes were set to either side of the cockpit and sported sharp angles to accept airflow from the sides of the nose assembly. The nose protruded a great length ahead of the cockpit, eliminating any natural "look-down" capability for the pilot. The pilot's vantage point was further hindered by setting the cockpit between the two intake openings with the fuselage spine beginning aft of the canopy. The canopy was a simple two piece system but heat resistant. Wings were of a monoplane arrangement, high-set along the intake sides and swept sharply along their leading edges, less so along the trailing. To counter airflow from these assemblies, the horizontal stabilizers were set well below the main wings and featured similar sweep back, though increased moreso in comparison along their trailing edges. The engine exhaust rings promoted a smoother shape to the fuselage aft section, derailing the true boxy shape of the MiG-25 design to an extent. The engines were set close to one another in a side-by-side seating. As such, twin vertical tail fins were affixed outboard of each engine placement, though both maintained a rather straight - albeit rearward-swept - standing profile. In all, the MiG-25 was consistent with Soviet aircraft design of the time, particularly where speed was involved - utilitarian to the core. The MiG-25 would never win any beauty contests to be sure but its single-minded nature ensured that it was designed to win the aerial confrontations at hand. Its silver exterior was also consistent with many aircraft of this time period, particularly those originating in the 1950s and 1960s.

    Mikoyan-Gurevich MiG-25P Technical Specifications

    Service Year: 1972
    Type: Supersonic Interceptor / Reconnaissance Bomber Aircraft
    National Origin: Soviet Union
    Manufacturer(s): Mikoyan-Gurevich - Soviet Union / Russia
    Production Total: 1,190

    Structural (Crew Space, Dimensions and Weights)

    Operating Crew: 1
    Length: 78.15 feet (23.82 meters)
    Width: 45.77 feet (13.95 meters)
    Height: 20.01 feet (6.10 meters)

    Weight (Empty): 44,092 lb (20,000 kg)
    Weight (MTOW): 80,954 lb (36,720 kg)

    Installed Power and Standard Day Performance

    Engine(s): 2 x Soyuz / Tumansky R-15B-300 turbojet engines with afterburn developing 22,494 lb of thrust each.

    Maximum Speed: 2,156 mph (3,470 kph; 1,874 knots)
    Maximum Range: 1,600 miles (2,575 km)
    Service Ceiling: 80,052 feet (24,400 meters; 15.16 miles)
    Rate-of-Climb: 41,000 feet-per-minute (12,497 m/min)

    Armament / Mission Payload

    Mission-specific armament usually centered around a standard fielding of air-to-air missiles as in the following:

    4 x AA-6 (R-40) "Acrid" air-to-air missiles


    2 x AA-7 (R-23) "Apex" air-to-air missiles
    2 x AA-8 (R-60) "Aphid" air-to-air missiles


    4 x AA-11 (R-73A) "Archer" air-to-air missiles
    4 x AS-11 (Kh-58) "Kilter" anti-radiation missiles

    Global Operators / Customers

    Algeria; Armenia; Azerbaijan; Bulgaria; Georgia; Kazakhstan; Turkmenistan; Ukraine; India; Iraq; Libya; Russia; Soviet Union; Syria

    Model Variants (Including Prototypes)

    Ye-155R-1 - Reconnaissance Prototype Designation

    Ye-166P-1 - Interceptor Prototype Designation

    Ye-266 - Reconnaissance Prototype Designation

    Ye-266M - Interceptor Prototype Designation

    MiG-25P - Initial Production Interceptor Model

    MiG-25R "Foxbat-A" - Reconnaissance Production Variant.

    MiG-25RB "Foxbat-B" - Operational-Level Reconnaissance Bomber Variant.

    MiG-25PU "Foxbat-C" - Two-seat Conversion Trainer

    MiG-25 "Foxbat-D" - Improved Reconnaissance Aircraft Variant.

    MiG-25PD "Foxbat-E" - Improved radar capability; Some were converted and upgraded Foxbat-A models.

    MiG-25BM "Foxbat-F" - Air-Defense Suppression Model featuring improved radar functionality and provisions for AS-11 Kilter anti-radiation missiles.

    MiG-31 "Foxhound" - Based on MiG-25 capabilities but with improved radar systems, improved weaponry and multi-targeting capability.

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