Variants |
first serial version, produced in 450 copies,
some of which modernized to the MiG-31BS standard |
two aircraft were designated as Type 31D and were manufactured
as dedicated anti-satellite models with ballast in the nose instead
of radars, flat fuselage undersurface (i.e. no recessed weapon system
bays) and had large winglets above and below the wing-tips. Equipped
with Vympel ASAT missiles. Two prototypes were built. |
Special modification used as a flying laboratory for
testing of ejection seats during flight. |
two-seat all weather, all altitude interceptor. Designated
as MiG-31 01DZ when fitted with air-to-air refueling probe. One hundred
produced of DZ variant. |
markedly improved version, with Zaslon-A radar, R-33
missiles and in-flight refueling pole; the MiG-31BS standard corresponds
to first generation devices modernized to this standard |
intended for export, with degraded capacities; no sales |
designation applied to type 01DZ when converted to MiG-31B
standard. |
appeared in 1991, but in development since the mid-1980s.
New Zaslon-M radar (capable to engage six targets at once), modernized
avionics, capable to carry up to 4 R-77 missiles (under the wings)
and 6 missiles R-37 (under the fuselage). Seven to fourteen copies
produced before 1995 |
recast realized by MAPO-MiG, modified Zaslon-AM radar
(with a maximum range of 240 km; cartographic function and terrain
tracking mode allowing air-to-ground fire, capable to track 24 targets
and engage 10 simultaneously) , new GLONASS cockpit and navigation
system, improved missiles (K-37M, K-73M, K-77-1, R-33S…). |
modified MiG-31BM variant capable to carry the hypersonic
Kh-47M2 Kinzhal ALBM. Ten aircraft have been modified as of May 2018.[95]
With this modification and with removed APU for air-to-air missiles,
the aircraft gained a sole role of an attack aircraft. |
Planned fighter-bomber intended for use with TV, radar
and laser-guided ASM weapon systems. Never entered in serial production. |
Planned export version of the MiG-31F. |
Modification for air launch to orbit of small spacecraft
with a mass of 120–160 kg to Earth's orbit in altitude about
600–300 km. |