Technical data
Type MiG-31
Function fighter
Year 1975
Crew 2
Engines 2*15500kg Perm D-30F6
Wing Span 13.46m
Length 22.69m
Height 6.1m
Wing Area 61.6m2
Empty Weight 21825kg
Normal Weight 41000kg
Maximum Weight 46200kg
Speed 3000km/h
g-Limit 5.0
Ceiling 20600m
Range 3000km
Armament
Guns 1*23mm GSh-6-23
260/gun
Missiles Catapult underfuselage launchers :
4*R-33 long range;
Underwing pylons :
4*R-60M close range; or 2*R-40TD mid range;

MiG-31, MiG-25MP, A.I.Mikoyan/M.I.Gurevich 'Foxhound'

Photo (26k) by Ian Woodrow ([email protected]) was found among his Planes and Things

Interceptor developed from the Mig-25. Project under designation MiG-25MP initiated in 1972, and first flight (test-pilot A.Fedotov) took place on September 19, 1975. In mass production since 1979, more than 500 MiG-31 and MiG-31B built. Two-seat aircraft has a re-designed lighter airframe (see table). Missile armament was almost doubled with 4 catapult launchable missiles and powerful cannon added.

Steel Titanium alloys Aluminum alloys
MiG-25 80% 8% 11%
MiG-31 50% 16% 33%
(31k) at Monino AF Museum, by

The first (and the only at the 1996) mass production interceptor in the world equipped with fixed Pulse-Doppler radar, allowing simultaneous tracking of 10 targets and firing against four of them. An unit of four MiG-31 can link their radars together, to establish a search pattern - covering a width of 800-900km with four aircraft, spaced at 200km. MiG-31 may also serve as an airborne command center to guide fighters with less powerful radar equipment (MiG-23, MiG-29, MiG-21-93).

Landing gear allows to use MiG-31 from unpaved airstrips (is there any other Mach 3 aircraft with such a capability?).


Modifications :

Modified December 9, 1996 Back to
Main Gate