The MiG-31 long-range supersonic interceptor aircraft entered into service in September 1975.
The MiG-31 fighter jet is fitted with four Vympel R-33E air-to-air missiles.
The MiG-31 aircraft is operated by two crew members including pilot and weapon system officer.
The maximum take-off weight of the MiG-31 aircraft is 46,200kg.

MiG-31 Foxhound is a long-range, two-seat supersonic interceptor aircraft offered by Russian Aircraft Corporation (previously Mikoyan and MiG) principally for the Russian and Kazakhstan air forces. Its maiden flight took place in September 1975.

The MiG-31 aircraft was derived from MiG-25 Foxbat interceptor and is equipped with state-of-the-art digital avionics.

MiG-31 can work efficiently in all weather conditions while fulfilling visual flight rules (VFR) and instrument flight rules (IFR), day and night. MiG-31 was the first soviet fighter aircraft to have true look-down and shoot-down capability.

More than 500 MiG-31 aircraft have been produced, out of which 370 were delivered to the Russian Air Force and 30 are in service with Kazakhstan Air Force. The remaining aircraft were upgraded to different variants under several upgrade programmes. Only some of the Russian MiG fleet have been upgraded to MiG-31BM standards under the upgrade programme.

Russia’s Defence Ministry announced its intention to invest in modernisation and life extension programme of MiG-31 Foxhound interceptors in July 2020.

Russian MiG-31 aircraft contract to Syria

In 2007, Russia’s United Aircraft Corporation (UAC) signed two contracts worth $1bn with Syria. One contract was for MiG-29M and another for MiG-31. The deliveries of MiG-29M are ongoing, but those of MiG-31 were not effective till 2009 when the UAC confirmed its plans to deliver the eight MiG-31 aircraft to Syria as part of the $1bn contract. The eight MiG-31 aircraft were ordered in a deal worth $400m signed in 2007. The order was cancelled in May 2009 due to pressure from Israel and lack of funds.

MiG-31 Foxhound development

The MiG-25 Foxbat was unable to fly at low altitudes. The installation of inefficient turbojet engines led to decrease in combat range at supersonic speeds and an increase in the speed gauge of the MiG-25 resulted in the destruction of the aircraft’s engine.

In an effort to overcome the drawbacks of the MiG-25 Foxbat, the MiG-31 was developed to fly at low altitudes with required supersonic speeds. MiG-31 is equipped with efficient low-bypass-ratio turbofan engines, which allow an increase in combat range.

Production of MiG-31 began in 1979 and the aircraft was fully operational with the Soviet Anti-Air Defence (PVO) by 1982. The economic slowdown in the USSR has made the maintenance of its complex MiG-31 aircraft difficult for many squadrons. As a result, around 20% of the MiG-31 aircraft were removed from service. About 75% of these aircraft, however, re-entered service with the Russian Air Force in 2006 when strong economic growth returned.

MiG-31 design

The MiG-31 has a highly aerodynamic and streamlined body to enable flying at high speeds at low altitude. The aircraft is specifically designed to track multiple targets simultaneously at high altitudes.

The MiG-31’s airframe contains various materials including welded nickel steel (49%), titanium (16%), aluminium alloy (33%) and 2% of composites. Four underwing pylons are also fitted in the fuselage of the aircraft.

The aircraft’s fuselage is designed to provide lateral rectangular and diagonal cut air intakes and features a bubble canopy with a long pointed nose.

The wings are sharpened and swept back with square tips and negative slant.


The variants of MiG-31 include MiG-31A, MiG-31B, MiG-31BS, MiG-31E, MiG-31F, MiG-31BM, MiG-31FE, MiG-31LL, MiG-31M, MiG-31D, MiG-31S, and MiG-31K.

Commercial satellite launch variants MiG-31A and MiG-31S have been used to train astronauts, to conduct research in the upper atmosphere and for space tourism by launching the aerospace rally system rocket-powered suborbital glider.

MiG-31E is an advanced version of the MiG-31 supersonic interceptor aircraft. It has a length of 21.6m, wingspan of 13.45m and height of 6.45m. The empty weigh of the aircraft is 21,825kg.

MiG-31E is equipped with RP-31E airborne phased array radar. It can track ten, and destroy four, targets from long distances. Under normal and adverse weather conditions, the MiG-31E has the capacity to destroy aerial targets flying at 50m to 28,000m altitude in front and rear hemispheres.

In the absence of a ground air-defence system, the MiG-31E aircraft scans airspace at width of 900km-1,000km. An infrared (IR) seeker unit installed in the variant can track targets by its heat emissions in the passive mode of a blind attack.

The MiG-31M is an upgraded version of MiG-31. The variant was developed by upgrading the cockpit of MiG-31 with a number of cathode ray tubes (CRT) and an increased number of missiles.

MiG-31BM is a high-speed multifunctional long-range fighter aircraft that can destroy both air and ground targets. The variant is equipped with upgraded avionics, hands-on-throttle-and-stick (HOTAS) controls, liquid-crystal colour multifunction displays (MFDs), a powerful on-board computer system, digital data links and a phased array radar. It has the capacity to intercept 24 targets simultaneously.

MiG-31D is an anti-satellite missile developed as part of the US ASAT (anti-satellite weapons) programme in 1987. It is fitted with single large missile beneath its fuselage and a special upward-looking radar. An associated intercept fire-control system is also equipped.

Two upgraded MiG-31BM fighter jets entered service with the Russian forces in 2019. The upgrades include new multimode radar, avionics, hands-on-throttle-and stick (HOTAS) controls, and multi-functional displays.


The MiG-31 cockpit is equipped with digital avionics such as MFDs and liquid crystal displays (LCDs), which provide updated instrument readings and radar information.

Both front and rear sides of the cockpit are equipped with zero / zero ejection seats which allow the pilot to fly at the altitude and airspeed preferred. The pilot sits in the front seat of the cockpit while the weapon system officer (WSO) sits in the rear cockpit seat, controlling the radar operations and weapon deployment thereby decreasing the work load of the pilot and increasing the efficiency.


Four long-range Vympel R-33E air-to-air missiles are installed in the MiG-31 aircraft. The R-33 can be launched in inertial navigation mode to shoot the target at extreme range. It can be guided in semi-active radar homing (SARH) mode for initial acquisition and mid course updates. It is used for attacking large and high-speed targets such as the SR-71 Blackbird, the B-1 Lancer bomber, and the B-52 Stratofortress.

The aircraft is also equipped with four short-range R-60MK missiles and two Bisnovat R-40TD1 medium-range missiles. A six-barrel 30mm internal cannon (Ghs-6-23M) is installed above the starboard main landing gear bay of the MiG-31 aircraft. The cannon contains 800 rounds of ammunitions and can fire at a rate of over 10,000 rounds a minute.

MiG-31BM can accommodate the AA-12 Adder missile and various Russian air-to-ground missiles (AGMs) such as the AS-17 Krypton anti-radiation missile (ARM).


The MiG-31 aircraft is equipped with world’s first electronically scanned N007 Zaslon phased array radar. It is also known as SBI-16 Zaslon (Flash Dance) radar and operates from the rear cockpit by WSO. It can receive signals from early warning radar (EWR) and airborne warning and control systems (AWACS).

Zaslon has the capacity to scan 200km distance. The radar can trap ten targets and engage four simultaneously flying in the surrounding radius of the aircraft (behind and below the aircraft).

The antenna of Zaslon is fixed and can be moved electronically. The electronic steering of the radar beam is much faster and accurate than mechanical steering.

The Zaslon radar has the capacity to search and attack various targets in air and ground using continuous and discontinuous fields of control and guidance commands despite target defensive manoeuvres, electronic counter measures (ECM) and adverse weather conditions.


MiG-31 is equipped with light duty (LD) / speed and direction (SD) sensor, track while scan (TWS) radar, infrared search and track (IRST) system and radar warning receiver (RWR) system.

The aircraft assigns partial power to track targets and the remaining to scan. The TWS radar system in the aircraft uses two new technologies – phased array radars and computer memory devices.

The IRST sensor detects and tracks jet aircraft and helicopters that emit infrared rays, while the RWR systems detect radar systems emitting radio waves through the ground or in the air. The RWR comprises a visual display unit (VDU) in the cockpit that monitors radars by producing audible sounds.

Engines and performance

MiG-31 supersonic aircraft is equipped with two Solovyev D-30F6 turbofan shaft engines with a take-off thrust 15,500kgf each. The dry thrust of the D-30F6 is 9,500kgf for each engine.

The engine provides a maximum speed of Mach 1.23 at low altitude and increases the aircraft’s range. The fuel consumption of the MiG-31 is very high compared to other aircraft, principally due to its multiple roles.

The MiG-31 can climb at a rate of 208m a second and has the capacity to fly at 3,000km/h. The ferry and combat ranges of the aircraft are 3,300km and 720km respectively.

The maximum take-off weight of the aircraft is 46,200kg. The cruise range and wing loading capacities are 1,620m and 665kg/m² respectively, while the maximum g-load is 5g.