MFI (512, 1.42)

Multifunctional Frontline Fighter

Foxhound air defence heavy interceptor. Since the mid eighties, along with the Sukhoi Su-27 Flanker, the above aircraft have formed the bulk of the Soviet Armed Forces fighter aviation. Developed in response to the adoption of the F-16 Fighting Falcon, F/A-18 Hornet, F-14 Tomcat and F-15 Eagle aircraft by the United States Air Force, they were called upon to ensure a high combat effectiveness and combat readiness level of the Soviet Air Force and Air Defence fighter fleet till the mid-nineties, with their further derivatives and upgrading programmes providing their further operability for even a longer period of time. However, life goes on, and by the mid-nineties, the USSR had planned to develop, test and put into service fifth-generation fighters which could in the early 21st century replace the fourth-generation aircraft currently operated.Mockup of competitors - MFI & S-37
It should be noted that the fifth-generation fighter development was commenced nearly at the same time both in the United States and Soviet Union. In 1981, under a governmental resolution, the USSR launched its programme of developing fighters for 1990s. The necessity for such a programme arose because of the scale of tasks assigned. It was supposed to develop not only new-generation fighters proper but the whole complex of equipment for them as well, including prospective engines, radar and optoelectronic surveillance and sighting systems, flight/navigation and communications equipment as well as the ECM system and missiles. Like the aircraft proper, all the systems were to be of a new generation with their characteristics differing radically from those of the systems operated by the present-day aircraft. The programme was to streamline efforts by various organisations and companies responsible for the development of certain aircraft systems with the costs and labour input increasing and tight schedule pressing.
The whole series of research dealing with the aircraft concept and aerodynamic configuration development, as well as with engines, weapons, avionics, materials and technologies applicable to the fifth-generation fighter, was conducted in two years.
Cockpit mockup of MFI
The research showed the requirements a future fighter must meet. They included:

  • Supermanoeuvrability, i.e. the aircraft capability to fly at high and extreme angles of attack with a high G-loading, perform tight power turns as well as to maintain controllability within the whole speed range varying from the maximal speed to the minimal speed permissible (including zero speed);
  • Supersonic non-afterburner cruising flight;
  • Low radar signature;
  • High surface and aerial target destruction effectiveness;
  • Advanced maintenance characteristics.

Mikoyan specialists had finished the preliminary design by 1985. It had two parts: the first part dealt with a heavy multirole and AD fighter (MFI) while the second one concerned a light tactical fighter (LFI). It implied a high degree of unification of the two aircraft. At the preliminary design stage, taking into account the results of the TsAGI wind-tunnel testing, research on the coatings reducing the plane’s radar signature and preliminary engine and equipment characteristics, rational MFI and LFI dimensions were determined, canard-type aerodynamic configuration was chosen, major design and lay-out solutions were adopted (airframe arrangement, air intakes’ form and arrangement, tail assembly scheme) and characteristics of the main fighter systems were set. Soon, the Mikoyan plant, along with other participants in the programme, presented successfully the design proposals for the MFI and LFI aircraft.Roll-out of 1.44

Following the MFI and LFI preliminary design presentation the Mikoyan plant launched the development of the MFI sketch design code-named 1.42. In parallel, there was a decision taken to prepare design documentation for building an experimental aircraft (project 1.44) intended for assessing and trying out its aerodynamics in flight tests as well as for studying its flight, stability and controllability characteristics. It was also supposed to be used to evaluate airframe strength, test and hone the integrated control system, powerplant and equipment and, later on, the whole system as well.

A lot of work was done by the Lyulka-Saturn association headed by Designer General Victor Chepkin. It managed to build more than twenty fifth-generation AL-41F TVC engines tested both at the plant and TsIAM Institute test-benches as well as at the LII institute flying laboratories, i.e. the subsonic on based on the Tu-16 bomber and the supersonic one derived from the MiG-25PD interceptor.MFI presentation

In 1991, the fighter’s sketch design was adopted. Unfortunately, the MFI programme funding has been considerably cut since 1992. Nonetheless, the MiG ANPK managed to build the mock-up and airframe components for static tests. In cooperation with series production plants, it made a technological advance for making prototypes. In early 1994, Mikoyan completed the construction of the first MFI flying prototype – the 1.44. In summer 1994, it was delivered to the Zhukovsky-based LII airfield where the ground testing of the 1.44 prototype systems was continued and preparation for flight testing was launched. In December 1994, the aircraft controlled by test pilot Roman Taskayev made its first high-speed taxiing on the LII runway. However, due to dramatic cuts in the MFI funding ensued by the economic situation in Russia, the fighter did not reach the flight test stage. In 1995, the funding of the programme dried up.

Late in 1998, the management of several companies concerned succeeded in persuading the decision-makers to give a green light to unveil the aircraft to the public. Such a demonstration was aimed at drawing attention to the programme, which could prompt the government to allocate additional funding for the testing to begin. Besides, unveiling the new sophisticated warplane was expected to draw potential foreign partners interested in joint development of prospective fighters in cooperation with the MiG company.First fly of 1.44

The MFI fighter was demonstrated on 12 January, 1999 when the prospective fighter, alongside other MiG’s aircraft, was officially presented to the Russian military leaders, military attaches of several countries and media. The fighter taxied down the LII Flight Test Institute runway to the demonstration site powered by its two AL-41F.

The MFI’s development, productionising and fielding with the Russian Air Force could both further bolster the national defence capabilities and increase exports, thus creating favourable environment for international cooperation in the field of aircraft building in the XXI century.1.44
The first flight the 1.44 was held February, 29, 2000 on aerodrome LII of a name of M.M.Gromov in a Joukovski. 18 minute flight passed 500-600 km/hour for speed. The airplane was piloted by the test pilot the Hero of Russia V.Gorbunov. The second flight proceeded 22 minutes.
In 2002, the MFI program was closed and flight tests of the aircraft were terminated due to a change in approaches to the creation of a front-line fighter in general. Instead of the MFI, the concept of the “Perspective Aviation Complex of Frontline Aviation” (PAK FA) was formed, on the basis of which the T-50 – Su-57 aircraft was created.
In 2015, the aircraft “1.44” was first publicly demonstrated at the MAKS-2015 air show.

1.44 at the MAKS air show

1.44Design and configuration The 1.44 aircraft is a heavy single-seat multirole fighter boasting the mid-wing canard-type airframe configuration with all-moving foreplanes, delta wings, two heavily outward-canted wide-spaced vertical stabilisers and large ventral fins. The airframe is intended to minimise the aircraft mid-section, to which end the air intakes are placed under the airframe forward section and put as close as possible, thus producing a single engine nacelle. The engines have been placed as close as possible too. Mounted on the series-built fighters, it is going to house the radar. The front side of the nosecone features the booms of the primary and backup (for the duration of testing) pitot static tubes.
The cockpit is fitted with a canopy with the moving section opened upward-backward, which is supposed to reduce the canopy’s sail area during parking and taxiing. The canopy turns into the fuselage spine fairing ending in the tail cone. The mid-fuselage section houses main fuel tanks, S-shaped air ducts as well as the landing gear wells. The belly-mounted air intakes are supersonic and adjustable with a special well for retracting the nose gear.
The all-moving foreplanes
Large delta wings have a wing-body extensionless straight leading edges fitted with two-section adaptive flap. The high-lift devices of the straight trailing edges feature two-section elevons. Every wing panel has a trailing edge dogtooth extension with additional multipurpose control surface and tail boom housing the avionics. Vertical stabilisers and ventral fins are attached to the tail boom. Every wing panel’s lower surface is equipped with hardpoints for mounting weapon pylons.
The all-moving foreplanes are mounted above the wing chord plane. Their leading edge has a distinctive “tooth” intended for generating vortices that increase the fighter’s aerodynamic characteristics. The MFI’s empennage comprise two wide-spaced trapezoid vertical stabilisers featuring forward-swept trailing edges and fitted with rudders, as well as ventral fins fitted with rudders too. The canted vertical stabilisers are supposed to reduce the radar cross-section (RCS) when illuminated laterally. The fighter boasts 16 control surfaces in total operated by multiple-redundant fly-by-wire system.
The MFI has retractable tricycle landing gear with the nose gear featuring two 620×180 mm wheels and the main gear having one 1,030×350 mm wheel each. The nose gear is retracted backwards into the two side door well within the air intake nacelle. The main struts are retracted forward into the mid-fuselage wells while turning the wheels. Each well is closed by a pair of doors.TVC engine nozzles
The powerplant consists of two AL-41F TVC turbofans ensuring the fighter’s combat super-manoeuvrability at all speeds and supersonic cruising flight in the non-afterburning mode. The TVC engine nozzles are axisymmentric with their inner surface laid out by high-temperature ceramics.
Avionics. The MFI combat version’s avionics is supposed to include a fire control, navigation, communications, ECM and fly-by-wire systems. The latter is used to manage control surfaces (elevons, leading edge flaps, foreplanes, rudders, flaps) and the engines (thrust vector value and direction). The main target detection means is to become a new-generation integral phased-array radar (FAR) capable of simultaneously acquiring and tracking multiple aerial targets and engaging several of them with missiles. Besides, the fire control system is going to incorporate optoelectronic detection and tracking systems and the helmet-mounted sight like those used by MiG-29 and Su-27 pilots but featuring better characteristics. The navigation system will include inertial and satellite navigation systems, short-range radio navigation/landing system, radio altimeter and other equipment mounted on the aircraft of such type.

Armament. The MFI prototype has no armament. However, the combat version will be able to employ all types of guided and unguided weapons now in use with the Russian Air Force as well as prospective high-precision weapons being developed for fifth-generation aircraft. It looks like the MFI’s primary weapons-load is to include RVV-AE medium-range active homing missiles and R-73 short-range infrared homing missiles as well as with their follow-on derivatives. There is a possibility of arming the MFI with long- and superlong-range air-to-air missiles (AAM) which could be derived from those carried by the MiG-31 interceptor as well as with prospective short-range missiles. The MFI’s weapons are to be housed by the internal weapons-bay and could be beefed up with external wing-mounted missiles, rocket pods and free-fall bombs. The fighter is to retain the integral 30 mm cannon.

Design RSK MiG
Type MFI (1.42)
Function Multifunctional Frontline Fighter
First flight February, 29, 2000
Crew 1
Dimensions & Weight
Length, m 21,7
Overall height, m 6,0
Wing Span, m 16,3
Take-off weight, kg max 35000
normal 28000
Warload, kg 6000-7000
Engines 2 Turbofan Al-14F
Thrust, kgf (kN) max 2 х 11200 ()
in afterburner 2 х 17700 ()
Range, km supersonic 2500
subsonic 4000
Speed, km/h (M=)
max at altitude (2,6)
cruise 1200 ()
Max g-load 9
Cannon Gsh-30-1
Missiles AA R-37
R-73, R-74
Missiles AS
unguided rockets, bomb

Схема окраски 1.44

1.44Вертикальное оперение и хвостовые балки1.44

References and Credits:

  1. Warplanes of Russia of XXI century / V.E.Il’in, «Astrel», «AST», 2000 /
  2. History and aircraft of Mikoyan design bureau / «Wings of Russia», 1999, CD-ROM /
  3. Warplanes of VVS of Russia / Aviatsia i Kosmonavtika №8. 1999 /
  4. «MiG» of fifth generation / V.E.Il’in, «Aerospace herald» 1-2 1999 /
  5. 1.44 – MFI – beginf MiG. The Russian fighter of the fifth generation / L.Berne, Wings of native land № 6 1999 /
  6. MFI / Angle of the sky /